N480AU
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
493 reports on file, 1995-03-21 – 2002-03-06.
Part: ANGLE — CRACKED (VERTICAL STAB) · airframe 34,715 hrs · 40,975 cycles
PDX - CRACK ON VERTICAL STAB TO FUSELAGE LT CONNECTION ANGLE INTERMEDIATE SPAR II. REPAIRED IAW FOKKER SRM 55-31-00, PAGE 2 AND SRM 51-31-04.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - LT INBOARD SEAT TRACK AT STATION 481.800 THERE IS AN AREA ABOUT 5 INCHES LONG WITH MANY GOUGES ON THE LUGS. REPAIRED IAW FOKKER MM 53-40-01, PAGE 206, FIGURE 205 AND SRM 53-02-15, FIGURE 1.
Part: SEAT TRACK — CHAFED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - LT INBOARD SEAT TRACK AT STATION 488.738 HOLE FOR FLOORBOARD RECEPTACLE HAS CHAFING ON FLANGE. REPAIRED IAW FOKKER MM 53-40-01, PAGE 206, FIGURE 306 AND SRM 53-02-15, FIGURE 1.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - LT INBOARD SEAT TRACK AT STATION 488.740 THERE ARE GOUGES ON TOP LUGS AND FLANGE AT FRAME 10966. REPAIRED IAW FOKKER MM 53-40-01, PAGE 205, FIGURE 204 AND SRM 53-02-15, FIGURE 1.
Part: SEAT TRACK — CHAFED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - LT INBOARD SEAT TRACK AT STATION 443.024 ON FLANGE WHERE TRACKS BUTT UP THERE IS CHAFING. REPAIRED IAW FOKKER MM 53-40-01, PAGE 206, FIGURE 205 AND SRM 53-02-15, FIGURE 1.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - LT INBOARD SEAT TRACK AT STATION 464.328 TOP LUGS HAVE GOUGES. REPAIRED IAW FOKKER SRM 53-02-15, FIGURE 1 AND SRM 51-31-01.
Part: FRAME — CRACKED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - FOUR CRACKS IN CUTOUT OF CASTELLATION ON BACKSIDE OF FRAME 41-2 ABOVE STRINGER 29. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 8.
Part: SKIN — DENTED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - RT SIDE EXTERIOR EMPENNAGE SKIN HAS A DENT BELOW V-STAB CONNECTION ANGLE. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 3 AND HORIZON AIR EA 4-53-1572.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - CRACK IN REAR PRESSURE BULKHEAD AT BEAM 6 LOWER FLANGE. REPAIRED IAW HORIZON AIR EA 4-53-1564/A.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - CRACKED NESTING ANGLE IN FLOOR SUPPORT ON INBOARD SIDE OF OUTBOARD SEAT TRACK, JUST AFT OF FRAME 8770. REPAIRED IAW FOKKER SRM 53-02-18, PAGE 3, FIGURE 1, SRM 53-15-02, PAGE 32, FIGURE 11 AND SRM 51-31-01.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - RT CEILING AT FRAME 13815A AND 13815B, STRINGER 42 HAS SMALL CRACK GOING FROM HOLE IN STRINGER FOR INSULATION TO HOLD IN PLACE. REPAIRED IAW FOKKER SRM 51-10-4, SRM 53-02-01, PAGE 8, FIGURE 6 AND SRM 51-31-01.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - CORROSION ON RT OUTBOARD SEAT TRACK FORWARD OF FRAME 5305 ABOUT 10 INCHES TO FRAME 4610 OUTBOARD FLANGE. REPAIRED IAW FOKKER SRM 51-31-01.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - CORROSION ON RT OUTBOARD SEAT TRACK AFT OF FRAME 4610 ON INBOARD FLANGE. REPAIRED IAW FOKKER MM PAGE 206, FIGURE 205.
Part: SKIN — CRACKED (LT WING) · airframe 34,715 hrs · 40,975 cycles
PDX - CRACK IN DOUBLER SKIN BETWEEN RIVETS ABOVE LT MAIN LANDING GEAR STRUT. REPAIRED IAW HORIZON AIR EA 4-57-578.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - CORROSION ON RT INBOARD SEAT TRACK FORWARD OF FRAME 4900 ABOUT 2 X 3 INCHES LONG ON OUTBOARD FLANGE. REPAIRED IAW FOKKER MM PAGE 206, FIGURE 205 AND SRM 53-01-01, PAGE 8, PARAGRAPH 4C.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - RT INBOARD SEAT TRACK FROM FRAME 9305 FORWARD 9 X 2 INCHES LONG INSIDE CHANNEL HAS PITTING AND CORROSION. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 8, PARAGRAPH 4C AND SRM 51-31-01.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - CRACKED NESTING ANGLE IN FLOOR SUPPORT ON OUTBOARD SIDE OF INBOARD SEAT TRACK, JUST AFT OF FRAME 8770. REPAIRED IAW FOKKER SRM 53-15-05, PAGE 60, FIGURE 16, SRM 53-02-18, PAGE 3, FIGURE 1 AND SRM 51-31-01.
Part: SKIN — CHAFED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - PROFILE AND SKIN CHAFED AT RIGHT WING TO FUSELAGE FAIRING BY PANEL 92N. REPAIRED IAW FOKKER SRM 51-00-00.
Part: SEAT TRACK — CHAFED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - LT INBOARD SEAT TRACK, INBOARD FLANGE HAS CHAFE FROM FLOORBOARD JUST FORWARD OF CAMLOCK RECEPTACLE AT FRAME 14755. REPAIRED IAW FOKKER MM 53-40-01, PAGE 206, FIGURE 205 AND SRM 51-10-4, PAGE 9.
Part: FRAME — CRACKED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - CRACKED CASTELLATION BELOW STRINGER 25 ON AFT SIDE OF FRAME 50-2. REPAIRED IAW FOKKER MM 53-10-05, PAGE 601.
Part: FRAME — CRACKED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - CASTELLATION ON AFT SIDE OF FRAME 50-2 CRACKED AT BOTH ENDS IN RADIUS BETWEEN STRINGERS 25 AND 26. REPAIRED IAW FOKKER MM 53-10-05, PAGE 601 AND SRM 53-02-13, PAGE 5, FIGURE 13.
Part: FRAME — CRACKED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - CRACK IN FRAME 50-2 ATTACH FLANGE AT CUTOUT FOR STRINGER 26. REPAIRED IAW FOKKER MM 53-10-05, PAGE 601.
Part: SKIN — CHAFED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - CHAFE ON AFT CARGO DOOR APERTURE, AFT SIDE APPROXIMATELY 14 INCHES FROM LOWER CORNER. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 8, PARAGRAPH 3D AND SRM 51-10-4, PAGE 9, PARAGRAPH 4B AND 4C.
Part: FRAME — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - CORROSION ON FRAME 6805 ABOVE STRINGER 1 AT THE NUT PLATES. REPAIRED IAW FOKKER MM 53-00-2, PAGE 601, FIGURE 2, STEPS 1-4 AND MM 53-00-2, PAGES 601-603, FIGURE 2, STEPS 5 AND 6.
Part: SKIN — DENTED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - DENT IN AFT FUSELAGE SKIN AFT OF FRAME 41-2 BETWEEN STRINGER 3 AND 5. REPAIRED IAW SRM 53-02-02, PAGE 2, FIGURE 1 AND SRM 51-31-01.
Part: SKIN — GOUGED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - TWO GOUGES AFT OF RT ACM LOWER MOUNT ON WALL SKIN. REPAIRED IAW HORIZON AIR EA 4-53-157 AND FOKKER SRM 51-30-01.
Part: DOOR FRAME — CHAFED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - CHAFE ON AFT CARGO DOOR APERTURE LOWER AFT CORNER. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 3, PARAGRAPH 3D AND HORIZON AIR EA 4-53-1570.
Part: SKIN — DENTED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - DENT IN AFT FUSELAGE SKIN AFT OF FRAME 41-2 BETWEEN STRINGER 3 AND 5. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 9, PARAGRAPH 6C AND SRM 51-31-01.
Part: FRAME — CRACKED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - CRACK NEXT TO LOWER RIVET OF CASTELLATION ON FRAME 16-2 OUTBOARD OF STRINGER 5. REPAIRED IAW FOKKER SRM.
Part: FRAME — DENTED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - TWO DENTS IN CASTELLATION ON FRAME 16-2 OUTBOARD OF STRINGER 70. REPAIRED IAW FOKKER SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - CRACK AT UPPER RIVET OF FRAME 41-2 CASTELLATION ON AFT SIDE ABOVE STRINGER 44. REPAIRED IAW FOKKER MM.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - CRACK IN REAR PRESSURE BULKHEAD AT BEAM VI LOWER FLANGE RADIUS OUTBOARD OF BL 1050L. REPAIRED IAW FOKKER SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - CASTELLATION ON FRAME 50-2 AT STRINGER 9 HAS CRACK FROM LOWER RIVET. REPAIRED IAW FOKKER MM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - CASTELLATION AT STRINGER 1 ON FRAME 50-2 IS CRACKED AT RIVET. REPAIRED IAW FOKKER MM.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - RT OUTBOARD SEAT TRACK FORWARD OF FRAME 5305 ON INBOARD FLANGE THERE IS PITTING AND CORROSION. REPAIRED IAW FOKKER SRM.
Part: FRAME — DENTED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - CASTELLATION DENTED ON FRAME 16-2 OUTBOARD OF STRINGER 68. REPAIRED IAW FOKKER SRM.
Part: FRAME — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - CORROSION EVIDENT UNDER NUT PLATE ON FRAME 7305 AT FOUR WAY FLOOR SUPPORT ABOVE STRINGER 74. REPAIRED IAW FOKKER SRM 53-01-01 AND SRM 51-10-4.
Part: FRAME — CRACKED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - CRACK IN RADIUS OF CASTELLATION REPAIR CLIP ON SIDE OF FRAME 61-2 AT STRINGER 42. REPAIRED IAW FOKKER SRM.
Part: DOOR — STUCK (PAX DOOR) · airframe 34,715 hrs · 40,975 cycles
PDX - PASSENGER DOOR WILL NOT OPEN IN EMERGENCY MODE. REPAIRED IAW FOKKER SRM 52-10-05, PAGES 413-414, PARAGRAPH 6J, STEPS 1-7 AND SRM 52-10-05, PAGES 414-415.
Part: INTERCOSTAL — SCRATCHED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - INTERCOSTAL IMMEDIATELY ABOVE CUT OUT FOR PANEL 24A HAS BEEN SCRATCHED. REPAIRED IAW FOKER SRM.
Part: FRAME — DENTED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - DENT IN RADIUS OF CASTELLATION ON FRAME 16-2 OUTBOARD OF STRINGER 69. REPAIRED IAW FOKKER SRM.
Part: FRAME — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - CORROSION UNDER NUT PLATES ON FRAME 6305 ON FOUR WAY FLOOR SUPPORT ABOVE STRINGER 74. REPAIRED IAW FOKKER MM 53-00-2, PAGES 601-602 AND SRM 51-31-04.
Part: RIVET — CRACKED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - TWO RIVETS BETWEEN FRAME 10775 AND 11300 HAVE SMALL CRACKS RADIATING ALONG THE LOWER CIRCUMFERENCE OF THE RIVET HEADS. REPAIRED IAW FOKKER SRM 51-31-01 PAGE 13, PARAGRAPH 7 AND SRM 51-31-01 PAGE 13.
Part: ATTACH FITTING — CRACKED (LT WING) · airframe 34,715 hrs · 40,975 cycles
PDX - LT WING FAIRING ATTACH STRUCTURE IS CRACKED ALONG THE FORWARD CIRCUMFERENCE OF PANEL 91J.
Part: FRAME — CRACKED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - CRACK PAST SECOND STOP DRILL IN LOWER END OF CASTELLATION ON AFT SIDE OF FRAME 50-2 AT STRINGER 46. REPAIRED IAW FOKKER SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - AT STRINGER 31 ON AFT SIDE OF FRAME 61-2, CASTELLATION IS CRACKED. REPAIRED IAW FOKKER SRM AND MM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - CRACK IN RADIUS OF CASTELLATION AT STRINGER 22 ON FRAME 50-2. REPAIRED IAW FOKKER MM.
Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 34,715 hrs · 40,975 cycles
PDX - LT WING LOWER WING-TO-FUSELAGE CONNECTION ANGLE FOR WING-TO-FUSELAGE FAIRING CONNECTION ANGLE IS CRACKED. REPAIRED IAW FOKKER SRM 51-31-01, PAGE 13 AND SRM 51-31-02, PAGES 9-10, PARAGRAPHS 4B AND 4C.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - RT INBOARD SEAT TRACK AT FRAME 13815 AFT OUTBOARD FLANGE THERE IS CORROSION. REPAIRED IAW FOKKER SRM.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - RT INBOARD SEAT TRACK AFT OF FRAME 13815A INSIDE CHANNEL HAS PITTING AND CORROSION. REPAIRED IAW FOKKER SRM.
Part: RIVET — CRACKED (WING FAIRING) · airframe 34,715 hrs · 40,975 cycles
PDX - LEFT-HAND WING FAIRING -Z- PROFILE HAS FOUR RIVETS WITH SMALL CRACKS RADIATING FROM THE LOWER CIRCUMFERENCE OF THE HEAD BETWEEN FRAMES 10775 AND 10335. REPAIRED IAW FOKKER SRM 51-31-01 PAGE 13, PARAGRAPH 7.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - RT OUTBOARD SEAT TRACK AT FRAME 9035A FORWARD ALONG INBOARD FLANGE HAS PITTING AND CORROSION. REPAIRED IAW FOKKER SRM.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - LT INBOARD SEAT TRACK AT STATION 191.929 MOST FORWARD END OF TRACK HAS CORROSION ON LUGS. ALSO, IN CHANNEL AND ON FLANGES. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 8, PARAGRAPH 4C, SRM 51-10-4 AND SRM 51-31-01.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - RT INBOARD SEAT TRACK FROM FRAME 9305B TO FRAME 6805 LUGS AT SEAT TIE DOWN HAVE GOUGES. REPAIRED IAW FOKKER MM 53-40-01, PAGE 206, FIGURE 205.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - RT INBOARD SEAT TRACK FRAME 5805 FORWARD 4 INCHES INSIDE THE CHANNEL HAS CORROSION. REPAIRED IAW FOKKER SRM.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - RT INBOARD SEAT TRACK FROM FRAME 7805 FORWARD AND INSIDE THE CHANNEL HAS CORROSION. REPAIRED IAW FOKKER SRM.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - RT OUTBOARD SEAT TRACK FROM FRAME 8805 FORWARD ABOUT 12 INCHES INBOARD FLANGE HAS PITTING AND CORROSION. REPAIRED IAW HORIZON AIR EA 4-53-1569.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - RT INBOARD SEAT TRACK FRAME 5305 TOP LUG AREA HAS CORROSION. REPAIRED IAW FOKKER SRM.
Part: DOUBLER — CRACKED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - CRACKED REPAIR AT STATION 13815B AND STRINGER 2. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, SRM 51-31-01 AND SRM 51-11-04.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - RT OUTBOARD SEAT TRACK AT STATION 667.906 TO STATION 667.901 INSIDE TUNNEL HAS PITTING AND CORROSION. REPAIRED IAW FOKKER SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - THERE ARE TWO PARALLEL CRACKS IN CASTELLATION ON FORWARD SIDE OF FRAME 32-2. REPAIRED IAW FOKKER SRM.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - RT OUTBOARD SEAT TRACK AT FRAME 6305 FORWARD ABOUT 5 INCHES LONG ON INBOARD FLANGE THERE IS CORROSION. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 8, PARAGRAPH 4C, STEP 1.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - RT OUTBOARD SEAT TRACK FROM FRAME 15635 TO FRAME 12405 THE LUGS ARE GOUGED. REPAIRED IAW FOKKER MM AND SRM.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - RT OUTBOARD SEAT TRACK AT FRAME 8305 FORWARD OUTBOARD FLANGE HAS PITTING AND CORROSION. REPAIRED IAW FOKKER SRM.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - RT OUTBOARD SEAT TRACK AT STATION 667.906 TO STATION 667.901 INSIDE LUGS THERE IS CORROSION. REPAIRED IAW FOKKER MM AND SRM.
Part: FLANGE — CRACKED (VERTICAL STAB) · airframe 34,715 hrs · 40,975 cycles
PDX - NUT PLATE FLANGE IS CRACKED AT TOP AFT CORNER OF APERTURE FOR PANEL 57P. REPAIRED IAW FOKKER SRM 55-02-05, PAGE 8, FIGURE 4 AND SRM 51-31-01.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - RT INBOARD SEAT TRACK AT FRAME 4610, FORWARD END OF TRACK, INBOARD FLANGE HAS CORROSION. REPAIRED IAW FOKKER SRM 53-01-01.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - RT INBOARD SEAT TRACK AT FRAME 9305B FORWARD TO FRAME 6805 INBOARD FLANGE HAS PITTING AND LIGHT CORROSION. REPAIRED IAW FOKKER SRM AND MM.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - RT OUTBOARD SEAT TRACK FRAME 9305B INSIDE CHANNEL THERE IS CORROSION. REPAIRED IAW FOKKER MM AND SRM.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - RT OUTBOARD SEAT TRACK AFT OF FRAME 14755 INSIDE TUNNEL THERE IS PITTING AND CORROSION. REPAIRED IAW FOKKER SRM AND MM.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - CORROSION ON RT OUTBOARD SEAT TRACK AT FRAME 5805 FORWARD ABOUT 5.5 X 3 INCHES LONG ON INBOARD FLANGE. REPAIRED IAW FOKKER SRM 51-10-04.
Part: ATTACH ANGLE — CRACKED (VERTICAL STAB) · airframe 34,715 hrs · 40,975 cycles
PDX - LT AND RT SIDES OF THE LOWER FLANGE AT THE VERTICAL STAB FROM SPAR TO FUSELAGE CONNECTION ANGLE HAS CRACKS. REPAIRED IAW FOKKER SRM 51-31-01.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - RT OUTBOARD SEAT TRACK FROM FRAME 8805 ALONG OUTBOARD FLANGE HAS PITTING AND CORROSION. REPAIRED IAW FOKKER SRM.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - RT INBOARD SEAT TRACK AFT OF FRAME 4900 ON OUTBOARD FLANGE THERE IS CORROSION. REPAIRED IAW FOKKER SRM.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - RT INBOARD SEAT TRACK AT FRAME 9305B FORWARD INSIDE CHANNEL HAS PITTING AND CORROSION. REPAIRED IAW FOKKER SRM.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - RT INBOARD SEAT TRACK FROM FRAME 6305 TO FRAME 4610 LUGS AT SEAT ATTACH POINTS HAVE GOUGES. REPAIRED IAW FOKKER MM.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - RT OUTBOARD SEAT TRACK FORWARD OF FRAME 13815B INSIDE THE TUNNEL HAS PITTING AND CORROSION. REPAIRED IAW FOKKER SRM.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - RT OUTBOARD SEAT TRACK FROM FRAME 9305B TO FRAME 6805 LUGS HAVE GOUGES AT SEAT TIE DOWN. REPAIRED IAW FOKKER MM 53-40-01, PAGE 206, FIGURE 205 AND SRM 51-10-04.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - RT INBOARD SEAT TRACK FROM FRAME 12405 TO FRAME 9305B WHERE SEAT ATTACHES TO TRACK LUGS HAVE GOUGES. REPAIRED IAW FOKKER MM AND SRM.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - RT OUTBOARD SEAT TRACK AT FRAME 9035A INBOARD FLANGE HAS CORROSION. REPAIRED IAW FOKKER SRM.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - RT OUTBOARD SEAT TRACK AT FRAME 13815 AFT INSIDE TUNNEL HAS PITTING AND CORROSION. REPAIRED IAW FOKKER SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - TWO PARALLEL CRACKS IN FRAME 32-2 CASTELLATION ON FORWARD SIDE AT STRINGER 52. REPAIRED IAW FOKKER MM AND SRM.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - LT INBOARD SEAT TRACK AT STATION 506.028 TOP LUGS HAVE GOUGES. REPAIRED IAW FOKKER MM 53-40-01, PAGE 205, FIGURE 204.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - STRINGER 64 CORRODED AT FORWARD END, AFT OF FRAME 3820. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 5, SRM 53-01-01, PAGE 6, PARAGRAPH 3 (A) AND SRM 51-10-4.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - RT INBOARD SEAT TRACK FRAME 6805 AFT INSIDE CHANNEL THERE IS CORROSION. REPAIRED IAW FOKKER SRM.
Part: FRAME — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - CORROSION UNDER NUT PLATES ON FRAME 9305B AT FOUR WAY FLOOR SUPPORT INBOARD OF STRINGER 74. REPAIRED IAW FOKKER SRM 51-31-01, PAGE 13, CHAPTER 7.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - RT INBOARD SEAT TRACK FROM FRAME 8805 FORWARD ABOUT 7 X 6 INCHES LONG INSIDE CHANNEL THERE IS CORROSION. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 8, PARAGRAPH 4C, STEP1.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - LT INBOARD SEAT TRACK AT STATION 525-709 TOP LUGS HAVE GOUGES. REPAIRED IAW FOKKER MM 53-40-01, PAGE 205, FIGURE 204.
Part: FRAME — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - CORROSION UNDER NUT PLATES ON FRAME 9305 AT FOUR WAY FLOOR SUPPORT BETWEEN STRINGER 74 AND CENTER LINE. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 6, PARA 4B, SRM 51-31-01, PAGE 13, CHAPTER 7 AND SRM 51-30-02, PAGE 9-10.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - RT OUTBOARD SEAT TRACK FROM FRAME 12405 INSIDE TUNNEL THERE IS PITTING AND CORROSION. REPAIRED IAW FOKKER SRM.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - RT INBOARD SEAT TRACK FROM FRAME 7805 INSIDE THE CHANNEL HAS PITTING AND CORROSION. REPAIRED IAW FOKKER SRM.
Part: CLIP — CRACKED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - CRACK IN CLIP ON AFT SIDE OF FRAME 14175 10 INCHES LEFT OF CENTER LINE. REPAIRED IAW FOKKER SRM 51-11-4, PAGE 2, PARAGRAPH E, SRM 51-10-4 AND SRM 51-31-01.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - RT OUTBOARD SEAT TRACK INBOARD FLANGE AROUND RECEPTACLE HOLE JUST FORWARD OF FRAME 9305B HAS CORROSION. REPAIRED IAW FOKKER SRM.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - RT OUTBOARD SEAT TRACK FORWARD OF FRAME 15635 CORROSION ON INSIDE LUGS. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 8, PARAGRAPH 4C, STEP 1 AND SRM 51-10-04, PAGE 8.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - RT INBOARD SEAT TRACK AT FRAME 4610 FORWARD OF TRACK AFT ABOUT 4 INCHES ON INBOARD FLANGE HAS CORROSION. REPAIRED IAW FOKKER SRM 53-40-01.
Part: FRAME — CRACKED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - FRAME 32-2 HAS CRACKED CASTELLATION AT BOTTOM RIVET AT STRINGER 70. REPAIRED IAW FOKKER MM AND SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - TWO CRACKS AT RIVETS IN CASTELLATION ON FRAME 32-2 BETWEEN STRINGERS 3 AND 5. REPAIRED IAW FOKKER MM AND SRM.
Part: ATTACH ANGLE — CRACKED (VERTICAL STAB) · airframe 34,715 hrs · 40,975 cycles
PDX - RT SIDE OF THE VERTICAL STAB TO FUSELAGE CONNECTION ANGLE ON THE FORWARD FACE OF THE FRONT SPAR IS CRACKED IN THE RADIUS. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 51-30-02.
Part: CONTROL CABLE — BROKEN (ELEVATOR) · airframe 34,715 hrs · 40,975 cycles
PDX - LT INBOARD ELEVATOR CABLE AT PULLEY CLUSTER BELOW HORIZONTAL STABILIZER ACTUATOR HAS BROKEN WIRES. REPAIRED IAW FOKKER SRM 27-31-00, PAGES 201 AND 502, STEPS 1-3 A (1)-(8).
Part: FRAME — DENTED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - DENT ON LT FRAME 3050 BELOW WINDOW FRAME BASE. REPAIRED IAW FOKKER SRM 53-02-05.
Part: FRAME — CRACKED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - CRACKED CASTELLATION AT LOWER RIVET ON FRAME 17565 AT STRINGER 24. REPAIRED IAW FOKKER SRM.
Part: PANEL — CHAFED (RT WING) · airframe 34,715 hrs · 40,975 cycles
PDX - RIGHT WING STATION 5280, PANEL 82CE AFT ATTACH POINTS ON PANEL HAVE MOUNT BRACKET CHAFE ON ONE SIDE AND THE OTHER SIDE IS ELONGATED. REPAIRED IAW FOKKER SRM 57-61-04 AND SRM 51-31-01.
Part: FRAME — CRACKED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - FRAME 32-2 FORWARD SIDE CASTELLATION CRACKED AT STRINGER 61. REPAIRED IAW FOKKER MM AND SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - CASTELLATION ON FORWARD SIDE OF FRAME 17565 AT STRINGER 20 IS CRACKED ADJACENT TO DIMPLE. REPAIRED IAW FOKKER MM AND SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - CRACKED CASTELLATION ON FRAME 32-2 AT STRINGER 12. REPAIRED IAW FOKKER MM AND SRM.
Part: FLOORBEAM — DENTED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - CABIN FLOORBEAM ON LT SIDE IS DENTED ON LOWER FLANGE BETWEEN FRAMES 13815 AND 13815A. REPAIRED IAW FOKKER SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - CASTELLATION ON FRAME 32-2 CRACKED AT STRINGER 11. REPAIRED IAW FOKKER MM AND SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - CRACKED CASTELLATION ALONG TWO DIMPLES ON FORWARD SIDE OF FRAME 17565 AT STRINGER 54. REPAIRED IAW FOKKER MM AND SRM.
Part: SKIN — DENTED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - DENT .020 INCH DEEP BY 2 INCHES IN LENGTH, 14.5 INCHES AFT OF LEFT HAND FRAME 3050 AND 11 INCHES BELOW WINDOW FRAME BASE. REPAIRED IAW FOKKER SRM 53-02-05, FIGURE 1, SRM 51-10-4 AND SRM 53-02-02.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - RT OUTBOARD SEAT TRACK FROM FRAME 12875 AFT ABOUT 8 INCHES, INSIDE TUNNEL THERE IS PITTING AND CORROSION. REPAIRED IAW FOKKER MM AND SRM.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - RT OUTBOARD SEAT TRACK AT FRAME 12875 FORWARD LUGS HAVE CORROSION. REPAIRED IAW FOKKER MM AND SRM.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - RT OUTBOARD SEAT TRACK GOUGES 9 INCHES FORWARD OF FRAME 11905. REPAIRED IAW FOKKER MM AND SRM.
Part: ATTACH ANGLE — CRACKED (VERTICAL STAB) · airframe 34,715 hrs · 40,975 cycles
PDX - RT VERTICAL STAB TO FUSELAGE CONNECTION ANGLE AT INTERMEDIATE SPAR II, AFT HI-LOK FORWARD SIDE CRACKED. REPAIRED IAW FOKKER SRM.
Part: SKIN PANEL — CRACKED (VERTICAL STAB) · airframe 34,715 hrs · 40,975 cycles
PDX - THREE CRACKS IN SKIN PANEL BENEATH THE LEADING EDGE OF THE RUDDER ON THE LT SIDE AT THE STIFFENER. REPAIRED IAW FOKKER SRM 53-02-05, PAGE 10, FIGURE 5 AND SRM 51-31-01.
Part: FRAME — DENTED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - DENT AFT OF LT FRAME 3050 AND 12 INCHES BELOW D-WINDOW FRAME BASE. REPAIRED IAW FOKKER SRM 53-02-05, FIGURE 1, SRM 53-02-02 AND SRM 51-10-4.
Part: SKIN — DENTED (WINDOW BELT) · airframe 34,715 hrs · 40,975 cycles
PDX - DENT BELOW LT WINDOW FRAME BASE. REPAIRED IAW FOKKER SRM 53-02-05, FIGURE 1, SRM 51-10-4, 53-02-03 AND SRM 53-02-02.
Part: ATTACH ANGLE — CRACKED (VERTICAL STAB) · airframe 34,715 hrs · 40,975 cycles
PDX - VERTICAL STAB TO FUSELAGE LT CONNECTION ANGLE INTERMEDIATE SPAR I, TWO INDICATIONS OF CRACKS AT FORWARD HI-LOK AND ONE INDICATION OF A CRACK AT AFT SIDE OF AFT HI-LOK. REPAIRED IAW FOKKER SRM 55-31-00, PAGE 2.
Part: ATTACH ANGLE — CRACKED (VERTICAL STAB) · airframe 34,715 hrs · 40,975 cycles
PDX - VISUAL CRACK INDICATION ON RT VERTICAL STAB TO FUSELAGE CONNECTION ANGLE AT INTERMEDIATE SPAR I AFT HI-LOK FORWARD SIDE. REPAIRED IAW FOKKER SRM 55-31-00, PAGE 2, FIGURE 1.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - RT OUTBOARD SEAT TRACK FROM FRAME 12405 TO FRAME 9305B ON ATTACH POINTS, LUGS HAVE GOUGES. REPAIRED IAW FOKKER SRM.
Part: STIFFENER — DEBONDED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - BONDED STIFFENER ON AFT SIDE OF REAR PRESSURE BULKHEAD, BETWEEN BEAM V AND VI, OUTBOARD OF BL425L IS DISBONDED FROM BULKHEAD WEB. REPAIRED IAW HORIZON AIR EA 4-53-1559.
Part: SKIN — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - REAR FUSELAGE SKIN CORRODED ON INSIDE OF FRAME 18075 BETWEEN STRINGERS 67 AND 69. REPAIRED IAW FOKKER SRM.
Part: BOSS — WORN (VERTICAL STAB) · airframe 34,715 hrs · 40,975 cycles
PDX - PIP PIN BOSS HAS STEP WEAR AT THE RT SIDE OF THE UPPER REMOVABLE FALSE RIB FOR PANEL 55F. REPAIRED IAW HORIZON AIR EA 4-55-301.
Part: FRAME — SCRATCHED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - SCRATCH ON BACK SIDE OF FRAME 16.2 TO LEFT SIDE OF CENTER LINE, NEAR TOP OF FRAME WEB. REPAIRED IAW FOKKER SRM 53-01-01 AND SRM 51-10-4.
Part: SKIN — GOUGED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - GOUGE IN AFT CARGO DOOR APERTURE OF FORWARD SIDE. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 51-31-02, PAGES 8 AND 9.
Part: FLANGE — CRACKED (RUDDER) · airframe 34,715 hrs · 40,975 cycles
PDX - THE FORWARD AND AFT FLANGES ON THE APERTURE FOR PANEL 57Y ON THE RUDDER ARE CRACKED OUT. REPAIRED IAW SRM 51-31-01.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - RT INBOARD SEAT TRACK FROM FRAME 6305 FORWARD ALONG INSIDE CHANNEL HAS CORROSION. REPAIRED IAW FOKKER SRM 53-40-01.
Part: SKIN — CHAFED (LT WING) · airframe 34,715 hrs · 40,975 cycles
PDX - LT WING UPPER SURFACE AT STATION 9890, MINOR CHAFED AREA. REPAIRED IAW FOKKER SRM 53-01-01, SRM 51-10-4 AND SRM 51-30-03.
Part: SKIN — CORRODED (WING) · airframe 34,715 hrs · 40,975 cycles
PDX - PANEL 72A APERTURE HAS FRETTING CORROSION AROUND SCREW HOLES. REPAIRED IAW F-28 SRM 51-10-04, PARAGRAPH 4, 57-12-01, PAGE 9 AND SRM 51-10-4.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX- RT INBOARD SEAT TRACK AT FRAME 13345 FORWARD INBOARD FLANGE HAS PITTING CORROSION. REPAIRED IAW FOKKER SRM 53-40-01 PAGE 206 AND 51-10-04 PAGE 9.
Part: SKIN — DENTED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - THREE DENTS, RT SIDE FUSELAGE, AFT OF RADOME OPENING, APPROXIMATELY WL 30.0 AND FRAME 1385.
Part: BEAM — DENTED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - HORIZONTAL BOX BEAM BETWEEN VERTICAL BEAMS BL425L AND BL425R, DENTED IN TOP SIDE, RT END ABOVE APU, FORWARD OF BLEED AIR DUCT. REPAIRED IAW HORIZON AIR EA 4-53-1562.
Part: DOUBLER — CRACKED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX- CRACKED REPAIR DOUBLER AT FRAME 13815B AND STRINGER 73. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4 FIGURE 2, 51-10-04 PAGE 9, 51-10-5 PAGES 1-7, 51-20-00, 51-31-01 AND 51-11-04.
Part: DOUBLER — CRACKED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - CRACKED REPAIR DOUBLER AT FRAME 13815B ON RT SIDE OF STRINGER 73. REPAIRED IAW FOKKER SRM 51-10-05, PAGES 1-7, SRM 51-10-04 AND SRM 51-11-04, PAGE 5, TABLE 2.
Part: DOUBLER — CRACKED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX- CRACKED REPAIR DOUBLER AT FRAME 13815B AND STRINGER 2. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4 FIGURE 2, 51-10-04 PAGE 9, 51-20-00, 51-31-01, AND 51-11-04 PAGE 5.
Part: FLANGE — CORRODED (LT WING) · airframe 34,715 hrs · 40,975 cycles
PDX - LT WING FLANGE FOR PANEL 71A HAS FRETTING CORROSION. REPAIRED IAW FOKKER SRM 57-01-01 AND SRM 51-10-4.
Part: STRINGER — CORRODED (LT WING) · airframe 34,715 hrs · 40,975 cycles
PDX - LT WING STRINGER 2.222 IS CORRODED AT STATION 2350. REPAIRED IAW FOKKER SRM 57-01-01, PAGE 4-5 AND SRM 51-10-04, PAGE 9.
Part: STRINGER — GOUGED (LT WING) · airframe 34,715 hrs · 40,975 cycles
PDX - LT WING STRINGER 2.9 GOUGED AT STATION 11130. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 6, PARAGRAPH 5B(A).
Part: PANEL — DAMAGED (WING) · airframe 34,715 hrs · 40,975 cycles
PDX - PANEL 75E HAS TWO HOLES WITH MINOR DAMAGE WHERE SCREWS WERE REMOVED.
Part: FITTING — GOUGED (LT WING) · airframe 34,715 hrs · 40,975 cycles
PDX - LT WING LOWER STRINGER 2.9 END FITTING IS GOUGED AT STATION 11130. REPAIRED IAW FOKKER SRM 57-01-01, PAGE 6, PARAGRAPH 5B(A).
Part: SKIN — DENTED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - DENT ON RT FUSELAGE, APPROXIMATELY FRAME 6802 AND WL 38.
Part: FLANGE — CORRODED (WING) · airframe 34,715 hrs · 40,975 cycles
PDX - LIGHT FRETTING CORROSION ON FLANGE OF WING FOR PANEL 73J. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4B.
Part: FLANGE — CORRODED (LT WING) · airframe 34,715 hrs · 40,975 cycles
PDX - LT WING FLANGE FOR PANEL 73A HAS FRETTING CORROSION. REPAIRED IAW FOKKER SRM 57-01-01, PAGE 5, PARAGRAPH 4C, SRM 57-12-01, PAGE 32 AND SRM 51-10-4.
Part: FLANGE — CORRODED (WING) · airframe 34,715 hrs · 40,975 cycles
PDX - LIGHT FRETTING CORROSION AROUND ATTACH HOLES, AT WING FLANGE FOR PANEL 73G. REPAIRED IAW FOKKER SRM 57-01-01 AND SRM 51-10-4, PAGE 9, PARAGRAPH 4B.
Part: ATTACH FITTING — CHAFED (LT WING) · airframe 34,715 hrs · 40,975 cycles
PDX - LT WING STATION 8200 FLAP BEAM ATTACH FITTING ON REAR SPAR HAS TWO CHAFE MARKS ON BOTH LUGS OF FITTING. REPAIRED IAW HORIZON AIR EA 4-57-577 AND FOKKER SRM 51-10-04.
Part: FLANGE — CORRODED (WING) · airframe 34,715 hrs · 40,975 cycles
PDX - LIGHT FRETTING CORROSION AROUND ATTACH HOLES AT WING FLANGE FOR PANEL 73H. REPAIRED IAW FOKKER SRM 87-01-01 AND SRM 51-10-4, PAGE 9, PARAGRAPH 4B.
Part: SKIN — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX- NAV/COMM UPPER ANTENNA MOUNT SURFACE ON FUSELAGE SKIN HAS CORROSION ON IT. REPAIRED IAW FOKKER SRM 51-10-4.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - LT INBOARD SEAT TRACK AT STATION 386.029 TOP LUGS HAVE GOUGES.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX- RT INBOARD SEAT TRACK AT FRAME 13815B JUST FORWARD ABOUT 2.5 INCHES IN TUNNEL THERE IS CORROSION. REPAIRED IAW FOKKER SRM 53-01-01 PAGE 8, 53-40-01 PAGE 206 AND 51-10-4 PAGE 9.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - LT INBOARD SEAT TRACK AT STATION 403.661 TOP LUGS HAVE GOUGES.
Part: STRINGER — CORRODED (LT WING) · airframe 34,715 hrs · 40,975 cycles
PDX - CORROSION ON LT WING STRINGER 2.37 AT STATION 6410. REPAIRED IAW FOKKER SRM 57-01-01, PAGE 5 AND SRM 51-10-4, PAGES 8 AND 9.
Part: STRINGER — CORRODED (LT WING) · airframe 34,715 hrs · 40,975 cycles
PDX - CORROSION ON LT WING STRINGER 2.36 AT STATION 6410. REPAIRED IAW FOKKER SRM 57-01-01, PAGE 5 AND SRM 51-10-4, PAGES 8 AND 9.
Part: PANEL — CORRODED (WING) · airframe 34,715 hrs · 40,975 cycles
PDX - PANEL 73D HAS VERY LIGHT FRETTING CORROSION ON FLANGE. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - LT INBOARD SEAT TRACK AT STATION 386.017 TO STATION 366.338 MOST INBOARD FLANGE HAS PITTING AND CORROSION.
Part: FLANGE — CORRODED (WING) · airframe 34,715 hrs · 40,975 cycles
PDX - MINOR FRETTING CORROSION AROUND ATTACH HOLES AT WING FLANGE FOR PANEL 73D. REPAIRED IAW FOKKER SRM 57-01-01 AND SRM 51-10-4, PAGE 9, PARAGRAPH 4B.
Part: FLANGE — CORRODED (LT WING) · airframe 34,715 hrs · 40,975 cycles
PDX - ALODINE DETERIORATED ON LT WING FLANGE FOR PANELS 73E-73J, LIGHT CORROSION FILM FORMING. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4B.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX- RT INBOARD SEAT TRACK FROM FRAME 12405 INSIDE TUNNEL HAS PITTING CORROSION. REPAIRED IAW FOKKER SRM 53-40-01 PAGE 206 AND 51-10-04 PAGE 9.
Part: FLANGE — CORRODED (WING) · airframe 34,715 hrs · 40,975 cycles
PDX - LIGHT FRETTING CORROSION AROUND ATTACH HOLES, AT WING FLANGE FOR PANEL 73F. REPAIRED IAW FOKKER SRM 57-01-01, PAGE 5, PARAGRAPH 4C, SRM 57-01-01, PARAGRAPH B(2)(A) AND SRM 51-10-4.
Part: FLANGE — CORRODED (WING) · airframe 34,715 hrs · 40,975 cycles
PDX - LIGHT FRETTING CORROSION ON WING FLANGE FOR PANEL 73C. REPAIRED IAW FOKKER SRM 57-01-01 AND SRM 51-10-4, PAGE 9, PARAGRAPH 4B.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - LT INBOARD SEAT TRACK AT STATION 403.668 TOP LUGS HAVE GOUGES.
Part: FLANGE — CORRODED (WING) · airframe 34,715 hrs · 40,975 cycles
PDX - MINOR FRETTING CORROSION AROUND ATTACH HOLES, AT WING FLANGE FOR PANEL 73E. REPAIRED IAW FOKKER SRM 57-01-01, PAGE 5, PARAGRAPH 4C AND SRM 51-10-4, PAGE 9, PARAGRAPH 4B.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX- RT INBOARD SEAT TRACK AT FRAME 13815 AFT INSIDE LUGS HAVE CORROSION. REPAIRED IAW FOKKER SRM 53-01-01 PAGE 8, 53-40-01 PAGE 206 AND 51-10-4 PAGE 9.
Part: STRINGER — CORRODED (LT WING) · airframe 34,715 hrs · 40,975 cycles
PDX - CORROSION ON LT WING STRINGER 2.38 AND STATION 6410. REPAIRED IAW FOKKER SRM 57-01-01, PAGE 5 AND SRM 51-10-4, PAGES 8 AND 9.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - LT INBOARD SEAT TRACK AT STATION 366.338 TO STATION 346.646 MOST INBOARD FLANGE HAS PITTING AND CORROSION.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX- RT INBOARD SEAT TRACK AT FRAME 13815 FORWARD INSIDE TUNNEL HAS CORROSION. REPAIRED IAW FOKKER SRM 53-40-01 PAGE 206 AND 51-10-04 PAGE 9.
Part: PANEL — CORRODED (WING) · airframe 34,715 hrs · 40,975 cycles
PDX - PANEL 73G HAS VERY LIGHT FRETTING CORROSION ON FLANGE. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX- RT INBOARD SEAT TRACK AT STATION 649.400 IN TUNNEL IS CORRODED. REPAIRED IAW FOKKER SRM 53-01-01 PAGE 8, 53-40-01 PAGE 206 AND 51-10-4 PAGE 9.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - LT INBOARD SEAT TRACK FROM STATION 423.346 TO STATION 403.661 BOTH MATTING FLANGES ARE PITTED AND HAVE CORROSION.
Part: FLANGE — CORRODED (LT WING) · airframe 34,715 hrs · 40,975 cycles
PDX - LT WING FLANGE FOR PANEL 73B HAS FRETTING CORROSION. REPAIRED IAW FOKKER SRM 57-01-01, PAGE 5 AND SRM 51-10-4, PAGE 9, PARAGRAPH 4B.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX- RT INBOARD SEAT TRACK FROM FRAME 12875 FORWARD 8 INCHES INSIDE TUNNEL HAS CORROSION. REPAIRED IAW FOKKER SRM 53-40-01 PAGE 206 AND 51-10-04 PAGE 9.
Part: FRAME — CRACKED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX- CRACKED CASTELLATION AT FRAME 14755 AND STRINGER 58. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4, 51-04-04 PAGE 9 AND 51-31-01.
Part: PANEL — CORRODED (WING) · airframe 34,715 hrs · 40,975 cycles
PDX - PANEL 73C HAS VERY LIGHT FRETTING CORROSION ON FLANGE. REPAIRED IAW FOKKER SRM 57-01-01, PAGE 5 AND SRM 51-10-4, PAGE 9.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - LT OUTBOARD SEAT TRACK AT STATION 582.394 THERE ARE GOUGES ON LUGS.
Part: PANEL — CORRODED (WING) · airframe 34,715 hrs · 40,975 cycles
PDX - PANEL 73A HAS FRETTING CORROSION ON FLANGE. REPAIRED IAW FOKKER SRM 51-10-4.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - LT OUTBOARD SEAT TRACK AT STATION 443.024 LUGS ARE GOUGED.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - LT OUTBOARD SEAT TRACK AT STATION 563.892 TOP LUGS HAVE GOUGES.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - LT OUTBOARD SEAT TRACK AT STATION 464.329 TOP LUGS HAVE GOUGES.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - LT OUTBOARD SEAT TRACK AT STATION 287.610 TOP LUGS HAVE GOUGES.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - LT OUTBOARD SEAT TRACK AT STATION 386.016 TOP LUGS HAVE GOUGES.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - LT INBOARD SEAT TRACK AT STATION 443.021 TOP LUGS HAVE GOUGES.
Part: SKIN — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX- LOWER AIR TRAFFIC CONTROL ANTENNA MOUNT SKIN HAS CORROSION ON IT. REPAIRED IAW FOKKER SRM 51-10-4.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - LT OUTBOARD SEAT TRACK BETWEEN STATION 386.023 AND STATION 366.338 MATTING FLANGES FOR FLOOR BOARDS ARE PITTED AND HAVE LIGHT CORROSION.
Part: LINK — CHAFED (SPEED BRAKE) · airframe 34,715 hrs · 40,975 cycles
PDX - SPEED BRAKE RT SUPPORT LINK UPPER DIAGONAL IS CHAFED AT UPPER END FROM RUBBING COMPOSITE TAIL CONE. REPAIRED IAW HORIZON AIR EA 4-53-1557 AND FOKKER SRM 51-10-4.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - LT OUTBOARD SEAT TRACK FROM STATION 366.338 TO STATION 337.204 BOTH MATTING FLANGES FOR FLOOR BOARDS HAVE PITTING AND LIGHT CORROSION.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - LT OUTBOARD SEAT TRACK AT STATION 506.028 TOP LUGS HAVE GOUGES.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - LT OUTBOARD SEAT TRACK AT STATION 287.605 HAS A 3 INCH AREA IN THE CHANNEL THAT HAS CORROSION.
Part: LINK — CHAFED (SPEED BRAKE) · airframe 34,715 hrs · 40,975 cycles
PDX - LT SUPPORT LINK FOR LT SPEED BRAKE FLAP HAS CHAFE DAMAGE AT UPPER END OF DIAGONAL ARM. REPAIRED IAW HORIZON AIR EA 4-53-1556 AND FOKKER SRM 4-53-1556.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - LT OUTBOARD SEAT TRACK AT STATION 326.971 TO STATION 326.959 IN THE CHANNEL THERE IS CORROSION.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - LT OUTBOARD SEAT TRACK AT STATION 403.661 TOP LUGS HAVE GOUGES.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - LT OUTBOARD SEAT TRACK AT STATION 517.749 TOP LUGS HAVE GOUGES.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - LT OUTBOARD SEAT TRACK AT STATION 600.894 AFT OF FRAME 13345 TOP LUGS ARE GOUGED.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - LT OUTBOARD SEAT TRACK AT STATION 600.898 FORWARD OF FRAME 13815 GOUGES ON LUGS.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - LT OUTBOARD SEAT TRACK AT STATION 403.656 TOP LUGS HAVE GOUGES.
Part: SKIN — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - UPPER ATC ANTENNA MOUNT SURFACE ON FUSELAGE SKIN HAS CORROSION ON IT. REPAIRED IAW FOKKER SRM 51-10-4.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX- RIGHT HAND INBOARD SEAT TRACK FROM FRAME 10346, FORWARD ABOUT THREE INCHES ON MATTING FLANGE THERE IS CORROSION. REPAIRED IAW FOKKER SRM 53-01-01 PAGE 8, 53-40-01 PAGE 206 AND 51-10-04 PAGE 9.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - LT OUTBOARD SEAT TRACK AT STATION 619.409 AND FRAME 13815A THE LUGS ON TOP ARE GOUGED.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - LT OUTBOARD SEAT TRACK AT STATION 307.290 TOP LUGS HAVE GOUGES.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - LT OUTBOARD SEAT TRACK AT STATION 488.740 TOP LUGS HAVE GOUGES.
Part: PANEL — CORRODED (WING) · airframe 34,715 hrs · 40,975 cycles
PDX - PANEL 73E HAS VERY LIGHT FRETTING CORROSION ON FLANGE. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9 AND SRM 57-01-01, PAGE 5.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - LT OUTBOARD SEAT TRACK AT STATION 506.022 TOP LUGS HAVE GOUGES.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - LT OUTBOARD SEAT TRACK AT STATION 545.391 TOP LUGS HAVE GOUGES.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - LT OUTBOARD SEAT TRACK AT STATION 267.909 THERE IS A 3 INCH AREA OF CORROSION IN CHANNEL. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4A AND SRM 51-10-4, PAGE 9, PARAGRAPH 4C.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - LT OUTBOARD SEAT TRACK AT STATION 525.713 TOP LUGS HAVE GOUGES. REPAIRED IAW FOKKER MM 53-40-01, PGE 206, FIGURE 205 AND SRM 51-10-4, PAGE 9, PARAGRAPH 4B AND 4C.
Part: SEAT TRACK — CHAFED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - LT OUTBOARD SEAT TRACK AT STATION 248.224 LUGS ARE CHAFED TO THE POINT OF DETERIORATION. REPAIRED IAW FOKKER MM 53-40-01, PAGE 206, FIGURE 205 AND SRM 51-10-4, PAGE 9, PARAGRAPH 4 B-C.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - LT OUTBOARD SEAT TRACK AT STATION 307.277 TOP LUGS HAVE GOUGES.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - LT INBOARD SEAT TRACK AT STATION 443.026 TOP LUGS HAVE GOUGES.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - LT OUTBOARD SEAT TRACK AT STATION 366.338 TOP LUGS ARE PITTED AND GOUGED.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - LT OUTBOARD TRACK AT STATION 228.539 TOP EDGES AND LUGS HAVE CORROSION. REPAIRED IAW FOKKER MM 53-40-01, PAGE 206, FIGURE 205 AND SRM 51-10-4, PAGE 9, PARAGRAPH 4C.
Part: SKIN — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX- VHF COMM FORWARD LOWER ANTENNA MOUNT SURFACE ON FUSELAGE SKIN HAS CORROSION ON IT. REPAIRED IAW FOKKER SRM 51-10-04 PAGE 9 PARA 4A AND 4B.
Part: PANEL — CORRODED (WING) · airframe 34,715 hrs · 40,975 cycles
PDX - PANEL 73B HAS FRETTING CORROSION ON FLANGE. REPAIRED IAW FOKKER SRM 57-01-01, PAGE 5 AND SRM 51-10-4.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - LT OUTBOARD SEAT TRACK AT STATION 464.324 TOP LUGS HAVE GOUGES.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - LT OUTBOARD SEAT TRACK AT STATION 326.955 TOP LUGS HAVE GOUGES.
Part: LINK — CHAFED (SPEED BRAKE) · airframe 34,715 hrs · 40,975 cycles
PDX - RT SUPPORT LINK FOR SPEED BRAKE IS CHAFED AT BOTTOM END OF LOWER DIAGONAL FROM CONTACT WITH COMPOSITE TAIL CONE. REPAIRED IAW HORIZON AIR EA 4-53-1558 AND FOKKER SRM 51-10-4.
Part: PANEL — CORRODED (WING) · airframe 34,715 hrs · 40,975 cycles
PDX - PANEL 71A HAS FRETTING CORROSION ON FLANGE. REPAIRED IAW FOKKER SRM 51-10-4.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - LT OUTBOARD SEAT TRACK AT STATION 403.668 TOP LUGS HAVE GOUGES.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - LT OUTBOARD SEAT TRACK AT STATION 267.920 THERE IS A 3 INCH AREA IN THE CHANNEL HAS CORROSION. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 8, PARAGRAPH 4C, STEP 1 AND SRM 51-10-4, PAGE 9, PARAGRAPH 4C.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - LT OUTBOARD SEAT TRACK FROM STATION 423.346 TO STATION 403.681 BOTH MATTING FLANGES ARE PITTED AND HAVE CORROSION.
Part: FRAME — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX- EVIDENCE OF CORROSION UNDER NUT PLATES ON FRAME 5805 AT FOUR WAY SUPPORT BRACKET ABOVE STRINGER 74. REPAIRED IAW FOKKER SRM 51-10-04 AND 51-31-01.
Part: LINK — CHAFED (SPEED BRAKE) · airframe 34,715 hrs · 40,975 cycles
PDX - SPEED BRAKE LT SUPPORT LINK HAS CHAFE DAMAGE AT LOWER END OF LOWER DIAGONAL FROM CONTACT WITH COMPOSITE TAIL CONE. REPAIRED IAW HORIZON AIR EA 4-53-1553.
Part: WEB — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - COCKPIT FLOOR CORROSION UNDER FIRST OFFICERS INBOARD SEAT TRACK. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 5, SRM 51-10-04, PAGE 8, PARAGRAPH 9 AND HORIZON AIR EA 4-53-1554.
Part: DOUBLER — CRACKED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX- CRACK IN FRAME CLIP REPAIR DOUBLER AT FRAME 13815A AND STRINGER 2. REPAIRED IAW FOKKER SRM 51-10-05, 51-10-4 AND 51-31-01.
Part: FRAME — CRACKED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX- CRACKED CASTELLATION AT FRAME 13345 AND STRINGER 29. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4, 51-10-04 PAGE 9 AND 53-31-01.
Part: FRAME — CRACKED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX- CRACKED CASTELLATION AT FRAME 13345 AND STRINGER 28. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4, 51-10-04 PAGE 9 AND 51-31-01.
Part: FRAME — CRACKED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX- CRACKED CASTELLATION BETWEEN STRINGERS 1 AND 2 AT FRAME 13815A. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4 FIGURE 2, 53-02-13 AND 51-31-01.
Part: FRAME — CRACKED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX- CRACKED CASTELLATION AT FRAME 14755 AND STRINGER 41. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4, 51-10-04 PAGE 9 AND 51-31-01.
Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX- CRACKED GILLINER SUPPORT BRACKET AND MISSING NUT PLATE AT FRAME 15635 OVER STRINGER 70. REPAIRED IAW FOKKER SRM 51-11-4 PARA E AND 51-31-01.
Part: DOUBLER — CRACKED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX- CRACKED REPAIR DOUBLER AT FRAME 13815A AND STRINGER 73. REPAIRED IAW FOKKER SRM 51-10-05, 53-02-13, 51-10-4 AND 51-31-01.
Part: RIVET — CRACKED (RUDDER) · airframe 34,715 hrs · 40,975 cycles
PDX- RIVET HEAD CRACKED ON TOP RIGHT HAND CORNER OF THE RUDDER COVE BOTTOM SKIN PANEL. REPAIRED IAW FOKKER SRM 51-31-01.
Part: FRAME — CRACKED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX- CRACKED CASTELLATION AT FRAME 12875 AND STRINGER 33. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4, 51-10-04 AND 51-31-01.
Part: DOUBLER — CORRODED (RUDDER) · airframe 34,715 hrs · 40,975 cycles
PDX- THE TOP EDGE OF THE BOTTOM SKIN PANEL ON THE RUDDER COVE HAS A TEMPORARY REPAIR STRIP INSTALLED ON THE INTERIOR BY THE GUSTLOCK HOUSING. THE STRUCTURE IS WORKING AND PRODUCING ALUMINUM OXIDE BUILDUP. REPAIRED IAW FOKKER SRM 51-31-01.
Part: FRAME — CRACKED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX- CRACKED CASTELLATION AT FRAME 12875 AND STRINGER 46. REPAIRED IAW FOKKER SRM 51-10-04, 53-02-13 PAGE 4 AND 51-31-01.
Part: FRAME — CRACKED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX- CRACKED CASTELLATION AT FRAME 13345 AND STRINGER 33. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4, 51-10-04 PAGE 9 AND 51-31-01.
Part: SKIN — CHAFED (EMERGENCY EXIT) · airframe 34,715 hrs · 40,975 cycles
PDX - RT AFT OVERWING EMERGENCY EXIT DOOR OUTER SKIN HAS CHAFE AND STEP WEAR DAMAGE AT FORWARD LOWER CORNER. REPAIRED IAW FOKKER SRM 52-01-01, STEP E, AREA B AND FIGURE 1 ON PAGE 3.
Part: SKIN — CHAFED (EMERGENCY EXIT) · airframe 34,715 hrs · 40,975 cycles
PDX- RT AFT OVERWING EMERGENCY EXIT DOOR OUTER SKIN EDGE HAS CHAFE AND STEP WEAR AT AFT UPPER CORNER. REPAIRED IAW FOKKER SRM 52-01-01, STEP E, AREA B AND FIGURE 1 ON PAGE 3.
Part: SKIN — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - AFT DME ANTENNA MOUNT SURFACE ON FUSELAGE SKIN HAS CORROSION ON IT. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 8, PARAGRAPH 4C AND SRM 51-10-4, PAGE 9, PARAGRAPH 4B (2).
Part: SKIN — CHAFED (EMERGENCY EXIT) · airframe 34,715 hrs · 40,975 cycles
PDX - RT AFT OVERWING EMERGENCY EXIT DOOR OUTER SKIN EDGE HAS CHAFE AND STEP WEAR DAMAGE AT FORWARD UPPER CORNER. REPAIRED IAW FOKKER SRM 52-01-01, STEP E, AREA B AND FIGURE 1 ON PAGE 3.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX- RT INBOARD SEAT TRACK FROM FRAME 15635 TO FRAME 12405 HAS GOUGED LUGS. REPAIRED IAW FOKKER SRM 53-40-01 PAGE 206.
Part: WEB — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - COCKPIT FLOOR CORROSION UNDER CAPTAINS INBOARD SEAT TRACK. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 5, SRM 53-11-05, PAGE 8, ITEM 325 AND SRM 51-10-4, PAGE 8, PARAGRAPH 3C.
Part: WEB — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - COCKPIT FLOOR CORROSION UNDER FIRST OFFICERS OUTBOARD SEAT TRACK. REPAIRED IAW FOKKER SRM 53-04-01, PAGE 5, SRM 53-11-05, PAGE 8, ITEM 325 AND SRM 51-10-4, PAGE 8, PARAGRAPH 3C.
Part: STRAP — CHAFED (LT WING) · airframe 34,715 hrs · 40,975 cycles
PDX- LT WING HAS CHAFE DAMAGE TO WING JOINT STRAP AT WS 1700, LOWER WING SURFACE. REPAIRED IAW FOKKER SRM 53-01-01 PAGE 5 AND HORIZON AIR EA 4-57-575.
Part: WEB — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - COCKPIT FLOOR CORROSION BELOW CAPTAINS OUTBOARD SEAT TRACK. REPAIRED IAW FOKKER SRM 51-10-04, SRM 53-01-01, PAGE 5 AND SRM 53-11-05 PAGE 8, ITEM 325.
Part: FRAME — CRACKED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX- CRACKED CASTELLATION ON FRAME 14755 AND STRINGER 60. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4, 51-10-04 PAGE 9 AND 51-31-01.
Part: FRAME — CRACKED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - FUSELAGE CABIN FRAME 14755 CASTELLATION IS CRACKED AT STRINGER 19. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2 AND SRM 51-31-01.
Part: FRAME — CRACKED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX- CRACKED CASTELLATION AT FRAME 14755 AND STRINGER 57. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4, 51-10-04 PAGE 9 AND 51-31-01.
Part: FRAME — CRACKED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - FUSELAGE CABIN FRAME 15205 CASTELLATION IS CRACKED AT STRINGER 23. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2 AND SRM 51-31-01.
Part: FRAME — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX- CORROSION AT STRINGER 1 AND FRAME CASTELLATION FOR FRAME 15205. REPAIRED IAW FOKKER SRM 53-01-01 PAGES 5-6 AND 51-10-4.
Part: FRAME — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX- CORROSION BETWEEN STRINGER 74 AND STRINGER 1, ON FRAME CASTELLATION OF FRAME 15205. REPAIRED IAW FOKKER SRM 53-01-01 PAGES 5-6 AND 51-10-04.
Part: FRAME — CRACKED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - FUSELAGE CABIN FRAME 15205 CASTELLATION IS CRACKED AT STRINGER 19. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2 AND SRM 51-31-01.
Part: FRAME — CRACKED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - FUSELAGE CABIN FRAME 15205 CASTELLATION IS CRACKED AT STRINGER 54. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2 AND SRM 51-31-01.
Part: FRAME — CRACKED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX- CRACKED CASTELLATION ON FRAME 15205 AND STRINGER 60. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4, 51-10-04 PAGE 9 AND 51-31-01.
Part: FRAME — CRACKED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX- CRACKED CASTELLATION AT FRAME 13815B AND STRINGER 27. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4, 51-10-04 PAGE 9 AND 51-31-01.
Part: FRAME — CRACKED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - FUSELAGE CABIN FRAME 15205 CASTELLATION IS CRACKED AT STRINGER 24. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2 AND SRM 51-31-01.
Part: FRAME — CRACKED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX- CRACKED CASTELLATION ON FRAME 14755 AND STRINGER 59. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4, 51-10-04 PAGE 9 AND 51-31-01.
Part: FRAME — CRACKED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - FUSELAGE CABIN FRAME 15205 CASTELLATION IS CRACKED AT STRINGER 22. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2 AND SRM 51-31-01.
Part: FRAME — CRACKED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX- CRACKED CASTELLATION AT FRAME 13815B AND STRINGER 49. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4, 51-10-4 PAGE 9 AND 51-31-01.
Part: FRAME — CRACKED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX- CRACKED CASTELLATION AT FRAME 13815 AND STRINGER 17. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4, 51-10-04 PAGE 9 AND 51-31-01.
Part: FRAME — CRACKED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - FUSELAGE CABIN FRAME 15205 CASTELLATION IS CRACKED AT STRINGER 18. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2 AND SRM 51-31-01.
Part: SKIN — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - THE FUSELAGE SKIN FOR THE FORWARD RADIO ALTIMETER ANTENNA MATTING SURFACE HAS CORROSION. REPAIRED IAW FOKKER SRM 51-10-4, PARAGRAPH A AND B.
Part: SKIN — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - THE FUSELAGE SKIN FOR THE AFT RADIO ALTIMETER ANTENNA MATTING SURFACE HAS CORROSION. REPAIRED IAW FOKKER SRM 51-10-4, PARAGRAPHA 4A.
Part: SKIN — CORRODED (FUSELAGE) · airframe 34,715 hrs · 40,975 cycles
PDX - THE SKIN UNDER MARKER BEACON ANTENNA MATTING SURFACE HAS CORROSION. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9 PARAGRAPH 4A (1) AND 4B (1) (2).
Earlier reports · 1995–2001 · 234 reports
2001
Part: SIGN — INTERMITTENT (CABIN) · airframe 34,575 hrs · 40,853 cycles
PDX- EMERGENCY EXIT SIGN IN GALLEY AREA HAS FAULTY LIGHT, IT INTERMITTENTLY GOES DARK. REMOVED AND REPLACED EMERGENCY EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: CONNECTOR — OUT OF POSITION (COCKPIT) · airframe 34,575 hrs · 40,853 cycles
BOI- FORWARD EMERGENCY LIGHT ABOVE COCKPIT DOOR INOPERATIVE. REPOSITIONED CONNECTION. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.
Part: ACTUATOR — FAILED (PAX DOOR) · airframe 34,268 hrs · 40,588 cycles
GEG- MAIN CABIN DOOR WILL NOT OPEN OR CLOSE. ACTUATOR FAILED. REMOVED AND REPLACED MAIN CABIN DOOR ACTUATING MECHANISM. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: BATTERY PACK — INOPERATIVE · airframe 34,141 hrs · 40,484 cycles
PDX-LED LIGHT NOT ILLUMINATED ON EMERGENCY FLASHLIGHT BEHIND F/O'S SEAT. LIGHT WAS INSTALLED BACKWARDS. REMOVED AND REPLACED BATTERY PACK ON EMERGENCY FLASHLIGHT BEHIND F/O'S SEAT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: CIRCUIT BOARD — INOPERATIVE (CABIN) · airframe 34,024 hrs · 40,390 cycles
SEA - COCKPIT DOORWAY EMERGENCY EXIT SIGN HAS INOPERABLE BULBS. REMOVED AND REPLACED CIRCUIT BOARD. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: SIGN — INOPERATIVE (CABIN) · airframe 33,988 hrs · 40,360 cycles
GEG - EMERGENCY EXIT SIGN AT ROW 9 INOPERABLE. REPLACED SIGN. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: SIGN — INOPERATIVE (CABIN) · airframe 33,886 hrs · 40,282 cycles
GEG - EXIT LIGHT ROW 8 INOPERABLE. REMOVED AND REPLACED LIGHT ASSEMBLY. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: CIRCUIT BOARD — INOPERATIVE · airframe 33,795 hrs · 40,207 cycles
GEG - EMERGENCY EXIT SIGN, ROW 8, INOPERABLE. REMOVED AND REPLACED CIRCUIT BOARD. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: STRUCTURE — CRACKED (SERVICE DOOR) · airframe 33,422 hrs · 39,889 cycles
PDX - DURING INSPECTION, FOUND SERVICE DOOR CRACKED. REPAIRED VIA THE INSTALLATION OF DOUBLER AND FILLER IN ACCORDENCE WITH STRUCTURAL REPAIR MANUAL 51-31-01. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
2000
Part: SIGN — INOPERATIVE (ROW 8) · airframe 31,375 hrs · 38,065 cycles
BOI - ROW 8 EXIT SIGN FOUND TO HAVE INOPERATIVE BULB. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: BULB — FAILED (EXIT SIGN) · airframe 30,831 hrs · 37,538 cycles
SEA - EMERGENCY EXIT SIGN AT CENTER CEILING CABIN HAS INOPERATIVE BULBS. REMOVED AND REPLACED EXIT SIGN ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: CIRCUIT BOARD — FAILED (CABIN) · airframe 30,782 hrs · 37,485 cycles
GEG - EMERGENCY LIGHT ABOVE FORWARD CABIN INOPERATIVE. REMOVED AND REPLACED CIRCUIT BOARD, OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: CIRCUIT BOARD — FAILED (CABIN) · airframe 30,758 hrs · 37,460 cycles
SEA - THE FORWARD OVERHEAD EXIT LIGHT ABOVE THE FLIGHT COMPARTMENT DOOR WAS REPORTED AS INOPERATIVE. REMOVED AND REPLACED CIRCUIT BOARD. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 30,688 hrs · 37,393 cycles
SEAT EMERGENCY LIGHTS ILLUMINATED IN OFF POSITION, SEATS 8 - 11. REMOVED AND REPLACED POWER SUPPLY, ALSO REPAIRED CHAFING WIRE AND REPLACED CONNECTORS P900 AND J901. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 30,667 hrs · 37,372 cycles
CHAIR PROXIMITY LIGHTING IN EXIT ROWS STUCK IN ON POSITION. REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHTING BATTERY PACK. OPERATIONAL CHECKS GOOD. AICRAFT RETURNED TO SERVICE.
Part: PANEL — DAMAGED (LT WING) · airframe 30,528 hrs · 37,236 cycles
YYC- LEFT HAND WING COVER DOOR PANELS 81N, 81R AND 81J ARE DAMAGED AND REQUIRE COMPOSITE REPAIR. REPAIRED IAW FOKKER SRM 51-70-03 PAGE 17 AND 51-70-0 PAGE 12 AND 13.
Part: SKIN — DENTED (VERTICAL STAB) · airframe 30,528 hrs · 37,236 cycles
YYC- DENT FOUND BETWEEN RIB 3.5 AND 3.4 1/2, 2 1/2 FORWARD OF STATION 27060 (RIGHT HAND VERTICAL STABILIZER). REPAIRED IAW HORIZON AIR EA 4-55-210.
Part: SKIN — CORRODED (FUSELAGE) · airframe 30,528 hrs · 37,236 cycles
YYC- CORROSION FOUND ON FUSELAGE BELLY SKIN PANEL AND SKIN FLANGE OF FRAME 9305C CASTELLATION BETWEEN STRINGER 74. REPAIRED IAW FOKKER SRM 53-15-04, 53-02-12 FIGURE 1 AND 51-31-01.
Part: FLOORBOARD — DAMAGED (FUSELAGE) · airframe 30,528 hrs · 37,236 cycles
YYC- FLOOR PANEL 25BB HAS ONE INSERT MISSING AND ONE CORRODED WITH SEAL WORN. REPAIRED IAW FOKKER SRM 51-70-03 PAGE 23.
Part: DOOR FRAME — MISDRILLED (FUSELAGE) · airframe 30,528 hrs · 37,236 cycles
YYC- REAR CARGO DOOR FORWARD APERTURE FRAME HAS MISDRILLED HOLES FROM CARGO DOOR APERTURE ROAMING UPPER AND LOWER SPLICE PLATES. REPAIRED IAW FOKKER SRM 53-28-08 FIGURE 01, AND 51-31-01.
Part: BULKHEAD — DAMAGED (LT WING) · airframe 30,528 hrs · 37,236 cycles
YYC- LEFT HAND STUB WING LATERAL BULKHEAD HAS HOLE CHAFED THROUGH, DUE TO CONTACT WITH 7TH STAGE PNEUMATIC DUCT. REPAIRED IAW HORIZON AIR EA 4-54-103 AND FOKKER SRM 54-02-01 FIGURE 4.
Part: SKIN — DENTED (FUSELAGE) · airframe 30,528 hrs · 37,236 cycles
YYC- DENTS ON FUSELAGE PRESSURE SKIN AT STATION 5805 TO 6305 AND LEFT HAND STRINGER 15. REPAIRED IAW HORIZON AIR EA 4-53-1184, FOKKER SRM 53-02-06 FIGURE 4, AND 53-02-13 FIGURE 2 PAGE 4.
Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 30,528 hrs · 37,236 cycles
YYC- STAB JUNCTION DRIVE FITTING AND STAB JUNCTION FITTING HAS FRETTING/PITTING CORROSION. REPAIRED IAW FOKKER SRM 55-01-01, 51-10-04 AND HORIZON AIR EA 4-55-222.
Part: SKIN — DENTED (RT ELEVATOR) · airframe 30,528 hrs · 37,236 cycles
YYC- RIGHT HAND ELEVATOR HAS TWO DENTS AND SEVERAL DISBONDS. REMOVED AND REPLACED RIGHT HAND ELEVATOR.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,528 hrs · 37,236 cycles
YYC- BLEND CORROISON AND MEASURE REMAINING MATERIAL ON CABIN SEAT TRACKS. REPAIRED IAW FOKKER SRM 53-01-01 AND 53-40-01.
Part: SKIN — DENTED (FUSELAGE) · airframe 30,528 hrs · 37,236 cycles
YYC- REINSPECT DENT ON FUSELAGE SKIN BETWEEN FRAMES 5305 AND 5805 AND STRINGERS 17 AND 18 AND IS ADJACENT TO PREVIOUS REPAIR. REPAIRED IAW HORIZON AIR EA 4-53-1184.
Part: BULKHEAD — CHAFED (LT WING) · airframe 30,528 hrs · 37,236 cycles
YYC- RIGHT HAND STUB WING LATERAL BULKHEAD HAS HOLE CHAFED THROUGH DUE TO CONTACT WITH 7TH STAGE PNEUMATIC DUCT. REPAIRED IAW HORIZON AIR EA 4-54-103, FOKKER SRM 54-02-01 FIGURE 4 AND 51-31-01.
Part: DOOR FRAME — DAMAGED (FUSELAGE) · airframe 30,528 hrs · 37,236 cycles
YYC- REAR CARGO DOOR SURROUND, FORWARD SIDE HOLED. REPAIRED IAW HORIZON AIR EA 51-31-01, 51-31-05, 53-23-07, AND HORIZON AIR EA 4-53-1193.
Part: ATTACH ANGLE — CRACKED (FUSELAGE FRAME) · airframe 30,528 hrs · 37,236 cycles
YYC- CRACK FOUND AT FRAME 32-2 AND STRINGER 23 ATTACK ANGLE. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 4 PAGE 6.
Part: BRACKET — WORN (LT WING) · airframe 30,528 hrs · 37,236 cycles
YYC- LEFT HAND NR 1 LIFTDUMPER SPIGOT HOLES ARE WORN IN MOUNTING BRACKET. REPAIRED IAW HORIZON AIR EA 4-57-423.
Part: FRAME — CRACKED (FUSELAGE) · airframe 30,528 hrs · 37,236 cycles
YYC- CRACK FOUND BEYOND STOP DRILL AT FRAME 50-2 AND STRINGER 31 ATTACH ANGLE. REPAIRED IAW HORIZON AIR EA 4-53-1194.
Part: VANE — DENTED (TE FLAP) · airframe 30,528 hrs · 37,236 cycles
YYC- NUMEROUS SMALL DENTS ON BOTTOM SIDE OF RIGHT HAND INBOARD FLAP VANE ON INBOARD END OF WHEEL RASH. REPAIRED IAW FOKKER SRM 51-70-0 PAGE 13 FIGURE 7.
Part: SCREW — INCORRECT (RT WING) · airframe 30,528 hrs · 37,236 cycles
YYC- RIGHT HAND WING LOWER JOINT STRIP AT STATION 11253 HAS DAMAGE FROM INCORRECT LENGTH SCREW. REPAIRED IAW HORIZON AIR EA 4-57-417 AND FOKKER SRM 57-01-01.
Part: PANEL — CORRODED (WING) · airframe 30,528 hrs · 37,236 cycles
YYC- LEFT HAND FUEL PANEL LIDS HAVE SLIGHT FRETTING/PITTING CORROSION ON MATTING SURFACE. REPAIRED IAW HORIZON AIR EA 4-57-424.
Part: SKIN — DENTED (PAX DOOR) · airframe 30,528 hrs · 37,236 cycles
YYC- DENT IN PASSENGER DOOR SKIN 24 INCHES FROM HINGE AND 14.5 FROM AFT EDGE. REPAIRED IAW FOKKER SRM 52-02-02 FIGURE 1 PAGES 2 AND 3.
Part: SKIN — DENTED (PAX DOOR) · airframe 30,528 hrs · 37,236 cycles
YYC- DENT IN PASSENGER DOOR SKIN 13 INCHES FROM BOTTOM EDGE OF DOOR AND 17 FROM FORWARD EDGE AT DOOR. REPAIRED IAW FOKKER SRM 52-02-01 PAGE 3 FIGURE 2.
Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 30,528 hrs · 37,236 cycles
YYC- CRACK FOUND AT FRAME 32-2 AND STRINGER 24 ATTACH ANGLE. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 6 FIGURE 4.
Part: EXHAUST PIPE — CRACKED (NR 2 ENGINE) · airframe 30,528 hrs · 37,236 cycles
YYC- NR 2 ENGINE JET PIPE IS CRACKED INTERNALLY AT 2 O''CLOCK POSITION ON FORWARD END. REPAIRED IAW SPEY MM 72-50.
Part: BRACKET — CRACKED (FUSELAGE) · airframe 30,528 hrs · 37,236 cycles
YYC- FORWARD HOOKLATCH, BACKUP BRACKET IS CRACKED AT FORWARD OUTBOARD CORNER. REPAIRED IAW FOKKER SRM 51-31-01 AND 51-31-04.
Part: FRAME — CRACKED (FUSELAGE) · airframe 30,528 hrs · 37,236 cycles
YYC- CRACK FOUND BEYOND STOP DRILL AT FRAME 32-2 AND STRINGER 66 ATTACH ANGLE. REPAIRED IAW FOKKER SRM 53-10-5.
Part: RIB — CRACKED (VERTICAL STAB) · airframe 30,528 hrs · 37,236 cycles
YYC- CRACK ON VERTICAL STAB, RIB 3.2 LEFT HAND SIDE AFT END OF LOWER SIDE. REPAIRED IAW FOKKER SRM 55-02-05 PAGE 8 FIGURE 4.
Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 30,528 hrs · 37,236 cycles
YYC- CRACK FOUND BEYOND STOP DRILL AT FRAME 32-2 AND STRINGER 31 ATTACH ANGLE. REPAIRED IAW HORIZON AIR EA 4-53-1192.
Part: STRUCTURE — CRACKED (WING TO BODY) · airframe 30,528 hrs · 37,236 cycles
YYC- RIGHT HAND WING TO FUSELAGE LOWER SIDE ''2'' PROFILE UNDER PANEL 92L IS CRACKED. REPAIRED IAW FOKKER SRM 51-31-01.
Part: BRACKET — BROKEN (FUSELAGE) · airframe 30,528 hrs · 37,236 cycles
YYC- CABIN FLOOR STRUCTURE FRAME 4175, FLOORBEAM BL 600 LT HAS A BROKEN SUPPORT BRACKET. REPAIRED IAW FOKKER SRM 51-31-01.
Part: SKIN — CORRODED (FUSELAGE) · airframe 30,528 hrs · 37,236 cycles
YYC- VHF COMM FORWARD LOWER ANTENNA BASE IS CORRODED ON FUSELAGE SKIN. REPAIRED IAW FOKKER SRM 53-01-01 AND HORIZON AIR EA 4-53-1185.
Part: SKIN — DELAMINATED (LT WING) · airframe 30,528 hrs · 37,236 cycles
YYC- LEFT HAND WING OUTBOARD TRAILING EDGE IS DELAMINATED ON UPPER SURFACE AT OUTER END AND HAS A FEW SHARP DENTS ON LOWER INBOARD END. REPAIRED IAW FOKKER SRM 51-70-03 PAGE 22.
Part: BRACKET — CRACKED (FUSELAGE) · airframe 30,528 hrs · 37,236 cycles
YYC- CABIN FLOOR STRUCTURE AT FRAME 4175 FLOORBEAM BL 600 LT OUTBOARD SUPPORT BRACKET CRACKED. REPAIRED IAW FOKKER SRM 51-31-01.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,528 hrs · 37,236 cycles
YYC- CENTER FLOORBEAM AT STATION 5000 UNDER PANEL 37AB HAS A CORRODED CAMLOCK. REPAIRED IAW HORIZON AIR EA 4-53-1189.
Part: VANE — DENTED (TE FLAP) · airframe 30,528 hrs · 37,236 cycles
YYC- LEFT HAND FLAP INBOARD VANE TRAILING EDGE HAS A FEW SHARP DENTS. REPAIRED IAW FOKKER SRM 51-70-03 PAGE 22 AND HORIZON AIR EA 4-53-1195.
Part: SKIN — DENTED (TE FLAP) · airframe 30,528 hrs · 37,236 cycles
YYC- LEFT HAND OUTBOARD FLAP TRAILING EDGE HAS SMALL DENT ON BOTTOM SKIN. REPAIRED IAW FOKKER SRM 51-70-03.
Part: TAB — DEBONDED (AILERON) · airframe 30,528 hrs · 37,236 cycles
YYC- RIGHT HAND AILERON TAB HAS 1 MINOR DISBOND 1 FOOT FROM INBOARD END OF TOP SKIN AND 2 MINOR DENTS ON TOP SKIN. REPAIRED IAW FOKKER SRM 51-70-03 PAGE 22.
Part: BRACKET — CRACKED (FUSELAGE) · airframe 30,528 hrs · 37,236 cycles
YYC- AFT HOOKLATCH AND HOOKLATCH BACKUP BRACKETS HAVE SURFACE CORROSION. REPLACED AFT HOOKLATCH FITTING.
Part: SKIN — DENTED (TE FLAP) · airframe 30,528 hrs · 37,236 cycles
YYC- NUMEROUS SMALL DENTS ON BOTTOM SIDE OF RIGHT HAND INBOARD FLAP TRAILING EDGE, INBOARD END OF WHEEL RUSH. REPAIRED IAW FOKKER SRM 51-70-0 PAGE 13.
Part: VANE — DENTED (TE FLAP) · airframe 30,528 hrs · 37,236 cycles
YYC- SHARP DENT ON TOP SIDE OF RIGHT HAND INBOARD FLAP VANE, INBOARD AND AFT OF PANEL 82AH. REPAIRED IAW FOKKER SRM 51-70-03.
Part: HORN — DAMAGED (LT AILERON) · airframe 30,528 hrs · 37,236 cycles
YYC- LEFT HAND AILERON TAB ACTUATION HORN HAS WORN HOLE. REPAIRED IAW HORIZON AIR EA 4-57-420 AND FOKKER SRM 27-10-02 PAGE 201.
Part: SKIN — DENTED (TE FLAP) · airframe 30,528 hrs · 37,236 cycles
YYC- LEFT HAND WING TRAILING EDGE PANEL , FIRST PANEL OUTBOARD OF NR 5 LID HAS A FEW SMALL DENTS. REPAIRED IAW FOKKER SRM 51-70-03 PAGE 22.
Part: VANE — DENTED (TE FLAP) · airframe 30,528 hrs · 37,236 cycles
YYC- DENT ON TOP SIDE OF RIGHT HAND OUTBOARD FLAP VANE, OUTBOARD AND AFT OF PANEL 82BG. REPAIRED IAW FOKKER SRM 51-70-03 PAGE 22.
Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 30,528 hrs · 37,236 cycles
YYC- SIX CRACKS FOUND ON NOSE LANDING GEAR BAY TOP COVER. REPAIRED IAW HORIZON AIR EA 4-53-1179, FOKKER SRM 51-31-05 AND 51-31-01.
Part: FLOORBOARD — CORRODED (FUSELAGE) · airframe 30,528 hrs · 37,236 cycles
YYC- FLANGES FOR CENTER FLOORBOARDS HAVE VARIOUS SPOTS OF FRETTING CORROSION FROM FRONT ENTRANCE TO PARTIAL BULKHEAD. REPAIRED IAW FOKKER SRM 53-1-01.
Part: SKIN — CORRODED (FUSELAGE) · airframe 30,528 hrs · 37,236 cycles
YYC- CORROSION FOUND ON FUSELAGE SKIN UNDER MARKER BEACON ANTENNA. REPAIRED IAW FOKKER SRM 53-01-01 AND 51-10-04.
Part: ANTENNA — CORRODED (FUSELAGE) · airframe 30,528 hrs · 37,236 cycles
YYC- CORROSION FOUND ON FORWARD RAD ALT ANTENNA BASE. REPAIRED IAW FOKKER SRM 53-01-01 AND 51-10-04.
Part: ANTENNA — CORRODED (FUSELAGE) · airframe 30,528 hrs · 37,236 cycles
YYC- CORROSION FOUND ON AFT RAD ALT ANTENNA BASE. REPAIRED IAW FOKKER SRM 53-01-01 AND 51-10-04.
Part: BRACKET — CRACKED (DRIVE FITTING) · airframe 30,528 hrs · 37,236 cycles
YYC- STAB DRIVE FITTING HAS CRACKED BRACKET BETWEEN FORWARD LUGS ON BOTTOM SIDE. REPAIRED IAW FOKKER SRM 51-31-01.
Part: SKIN — CORRODED (FUSELAGE) · airframe 30,528 hrs · 37,236 cycles
YYC- CORROSION FOUND ON FUSELAGE SKIN UNDER LOWER AIR TRAFFIC CONTROL TRANSPONDER ANTENNA. REPAIRED IAW FOKKER SRM 53-01-01 AND 51-14-04.
Part: PLATE — CORRODED (ANTENNA) · airframe 30,528 hrs · 37,236 cycles
YYC- CORROSION FOUND ON AFT BLANKING PLATE ATTACH AREA OF RAD ALT ANTENNA. REPAIRED IAW FOKKER SRM 53-01-01 AND 51-10-04.
Part: DOOR FRAME — CORRODED (EMERGENCY EXIT) · airframe 30,528 hrs · 37,236 cycles
YYC- SERVICE EMERGENCY DOOR APERTURE, LOWER TENSION BOX UPPER SURFACE AND AUXILIARY STRUCTURE HAS CORROSION ALL AROUND. REPAIRED IAW FOKKER SRM 53-01-01.
Part: SKIN — DENTED (FUSELAGE) · airframe 30,528 hrs · 37,236 cycles
YYC- DENT IN FUSELAGE SKIN 2 INCHES FORWARD OF FRAME 16660 BETWEEN STRINGERS 35 AND 34. REPAIRED IAW FOKKER SRM 53-02-01 FIGURE 1.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,528 hrs · 37,236 cycles
YYC- AUXILIARY FLOORBEAM HAS CORROSION ON CABIN FLOOR STRUCTURE FRAME 3820 THROUGH 3870. REPAIRED IAW FOKKER SRM 53-01-01.
Part: STRUCTURE — CRACKED (APU BAY) · airframe 30,528 hrs · 37,236 cycles
YYC- APU FORWARD ENCLOSURE, RIGHT HAND TOP CORNER AREA IS CRACKED. REPAIRED IAW FOKKER SRM 49-00-01, 51-31-01 AND HORIZON AIR EA 4-49-79.
Part: SKIN — CRACKED (VERTICAL STAB) · airframe 30,528 hrs · 37,236 cycles
YYC- VERTICAL STABILIZER TRAILING EDGE SKIN HAS TWO CRACKS. REPAIRED IAW FOKKER SRM 55-31-01 FIGURE 1, 55-02-05 FIGURE 5 AND 51-31-01.
Part: RIVET — LOOSE (VERTICAL STAB) · airframe 30,528 hrs · 37,236 cycles
YYC- VERTICAL STABILIZER TRAILING EDGE HAS LOTS OF LOOSE RIVITS. REPAIRED IAW FOKKER SRM 51-31-01 AND 55-31-01 FIGURE 1.
Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 30,528 hrs · 37,236 cycles
YYC- CABIN FLOOR STRUCTURE AT FRAME 3820 - 3870, FORWARD GALLEY, FLOOR AUXILIARY STRUCTURE HAS A CRACKED SPOT AND A BROKEN ANCHOR NUT. REPAIRED IAW FOKKER SRM 53-02-14 FIGURE 1 AND 51-31-01.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 30,528 hrs · 37,236 cycles
YYC- FLOORBEAM TO REAR PRESSURE BULKHEAD ATTACH POINT HAS TWO ANGLE BRACKETS CRACKED. REPAIRED IAW FOKKER SRM 51-31-01.
Part: SKIN — DENTED (FUSELAGE) · airframe 30,528 hrs · 37,236 cycles
YYC- DENT IN FUSELAGE SKIN 2 INCHES FORWARD OF FRAME 16660 BETWEEN STRINGERS 34 AND 35. REPAIRED IAW FOKKER SRM 53-02-01 FIGURE 1.
Part: SKIN — CHAFED (APU BAY) · airframe 30,528 hrs · 37,236 cycles
YYC- APU FORWARD ENCLOSURE RIGHT HAND LOWER INTERNAL SKIN CHAFED. REPAIRED IAW FOKKER SRM 49-00-01, 51-31-01 AND HORIZON AIR EA 4-49-79.
Part: FRAME — CRACKED (NLG WW) · airframe 30,528 hrs · 37,236 cycles
YYC- NOSE LANDING GEAR BAY UPPER STRUCTURE FRAME 2650 IS CRACKED WHERE THE NOSE WHEEL SNUBBER ATTACHES. REPAIRED IAW FOKKER SRM 51-31-01 AND 53-02-11 PAGE 3.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,528 hrs · 37,236 cycles
YYC- CABIN FLOOR STRUCTURE AT FRAME 3450 TO 4175 FLOORBEAM BL 1127 RT HAS A CRACKED AND CORRODED SPOT. REPAIRED IAW FOKKER SRM 53-11-05 FIGURE 3, 51-31-01 AND 53-02-14.
Part: BRACKET — CRACKED (NLG WW) · airframe 30,528 hrs · 37,236 cycles
YYC- NOSE LANDING GEAR BAY TOP COVER BRACKET BETWEEN STATION 2475 AND 2650 IS CRACKED. REPAIRED IAW FOKKER SRM 53-11-13 PAGE 12 AND 51-31-02.
Part: FRAME — CRACKED (FUSELAGE) · airframe 30,528 hrs · 37,236 cycles
YYC- CRACK AT STATION 16660 AND STRINGER 43 INSIDE CABIN. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4, 53-01-00 ITEM 3D AND 53-24-04 FIGURE 6 PAGE 18.
Part: FRAME — CRACKED (FUSELAGE) · airframe 30,528 hrs · 37,236 cycles
YYC- CRACK AT STATION 16060 AND STRINGER 30 INSIDE CABIN. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4 FIGURE 2 AND 53-24-04 PAGE 18 FIGUER 6.
Part: FRAME — CRACKED (FUSELAGE) · airframe 30,528 hrs · 37,236 cycles
YYC- CRACK AT STATION 16060 AND STRINGER 45 INSIDE CABIN. REPAIRED IAW FOKKER SRM 53-02-15 PAGE 4 FIGURE 2 AND 53-24-04 FIGURE 5 PAGE 16.
Part: SKIN — CRACKED (FUSELAGE) · airframe 30,528 hrs · 37,236 cycles
YYC- THERE IS A CRACK AT STATION 16660 BETWEEN STRINGER 26 AND 27 INSIDE CABIN. REPAIRED IAW FOKKER SRM 53-02-01 FIGURE 5 PAGE 7.
Part: BRACKET — CRACKED (NR 2 ENGINE) · airframe 30,528 hrs · 37,236 cycles
YYC- NR 2 ENGINE STUB WING WIRE/CABLE LOOM BRACKET BELOW PANEL O2D IS CRACKED. REPAIRED IAW FOKKER SRM 4-20-11 FIGURE 2 AND 51-31-01.
Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 30,528 hrs · 37,236 cycles
YYC- CABIN FLOOR STRUCTURE AT FRAME 3820 - 3870, FLOORBEAM BL 600 RT HAS A LOOSE ANCHOR NUT AND A BROKEN SUPPORT BRACKET. REPAIRED IAW FOKKER SRM 51-31-01 AND 53-11-05.
Part: UNIVERSAL JOINT — WORN (FLAP DRIVE) · airframe 30,528 hrs · 37,236 cycles
YYC- LEFT HAND WHEEL BAY FLAP DRIVE TUBE U JOINT IS WORN. REPAIRED IAW FOKKER SRM 27-51-04.
Part: FRAME — CRACKED (FUSELAGE) · airframe 30,528 hrs · 37,236 cycles
YYC- CRACK AT STATION 16660 AND STRINGER 53 INSIDE CABIN. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4 FIGURE 2 AND 53-24-04 PAGE 18 FIGURE 6.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 30,528 hrs · 37,236 cycles
YYC- RIGHT HAND WING TO FUSELAGE LOWER SIDE OF WING AT STATION 1700, FUSELAGE STATION 11783 AND STRINGER TIE CAP IS CRACKED. REPAIRED IAW FOKKER SRM 53-52-04 PAGE 8 FIGURE 365, 51-31-01 AND 51-30-2.
Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 30,528 hrs · 37,236 cycles
YYC- CRACK FOUND BEYOND STOP DRILL AT FRAME 32-2 AND STRINGER 51 ATTACH ANGLE. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 3 PAGE 5.
Part: SKIN — CORRODED (FUSELAGE) · airframe 30,528 hrs · 37,236 cycles
YYC- DENT ON FUSELAGE BELLY SKIN AND DOUBLER BEHIND CENTER CARGO DOOR AT STATION 8305 AND STRINGER 73. REPAIRED IAW HORIZON AIR EA 4-53-1178 AND FOKKER SRM 51-31-01.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,528 hrs · 37,236 cycles
YYC- CABIN FLOOR STRUCTURE FRAME 4610 - 4650 FLOORBEAM BL 600 RT HAS SOME CORROSION. REPAIRED IAW FOKKER SRM 53-11-05 FIGURE 4 AND 51-31-01.
Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 30,528 hrs · 37,236 cycles
YYC- CRACK FOUND OUTDSIDE STOP DRILL ARM OF FRAME 32-2 AND STRINGER 7 ATTACH ANGLE. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 3 PAGE 5.
Part: SKIN — LOOSE (VERTICAL STAB) · airframe 30,528 hrs · 37,236 cycles
YYC- VERTICAL STABILIZER UPPER SECTION INTERMITTENT SPAR II AND SKIN CONNECTION, BOTH LEFT HAND AND RIGHT HAND SKIN LOOSE. REPAIRED IAW HORIZON AIR EA 4-55-209.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 30,528 hrs · 37,236 cycles
YYC- FRAME 13815 AND STRINGER 72 ANGLE CRACKED AT PREVIOUS REPAIR. REPAIRED IAW FOKKER SRM 53-02-12.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 30,528 hrs · 37,236 cycles
YYC- WEB CRACK 30MM LONG ON UPPERSIDE OF BEAM 1 BL 85L - BL 115L. REPAIRED IAW FOKKER SRM 53-02-18 FIGURE 13 AND 51-31-01.
Part: FRAME — CRACKED (FUSELAGE) · airframe 30,528 hrs · 37,236 cycles
YYC- CRACK FOUND BEYOND STOP DRILL AT FRAME 32-2 AND STRINGER 9 ATTACK ANGLE. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 3 PAGE 5.
Part: FRAME — CRACKED (FUSELAGE) · airframe 30,528 hrs · 37,236 cycles
YYC- CRACK FOUND BEYOND STOP DRILL AT FRAME 32-2 AND STRINGER 48. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 5 FIGURE 3.
Part: BEAM — MISDRILLED (FUSELAGE) · airframe 30,528 hrs · 37,236 cycles
YYC- UPPER U PROFILES ON BEAM 6 OF FORWARD REAR PRESSURE BULKHEAD, BETWEEN BL 425L AND BL 425R HAVE HOLES THAT ARE SHY OF EDGE DISTANCE. DRILLED UP NEW U PROFILES AND INSTALLED ON FORWARD REAR PRESSURE BULKHEAD BEAM 6 AS PER FOKKER SRM CHAPTER 51 GENERAL PRACTICES (P/N A23100-001).
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 30,528 hrs · 37,236 cycles
YYC- THE LEFT HAND INBOARD SEAT TRACK IS CRACKED ON THE INBOARD SIDE OF STATION 10253. REPAIRED IAW FOKKER SRM 53-15-05 PAGE 38 AND 51-31-01.
Part: STRUCTURE — CRACKED (RUDDER) · airframe 30,528 hrs · 37,236 cycles
YYC- RUDDER LEFT HAND LEADING EDGE STRUCTURE UNDER PANEL 57U IS CRACKED. REPAIRED IAW FOKKER SRM 51-31-01.
Part: SKIN — CRACKED (VERTICAL STAB) · airframe 30,528 hrs · 37,236 cycles
YYC- VERTICAL STABILIZER RIGHT HAND AFT LOWER SECTION REPAIR PATCH IS CRACKED. REPAIRED IAW FOKKER SRM 51-31-01.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 30,528 hrs · 37,236 cycles
YYC- REAR PRESSURE BULKHEAD BELOW FLOOR BEAM NR 1 CONNECTION ANGLE AT LEFT HAND SIDE IS CRACKED. REPAIRED IAW FOKKER SRM 53-31-01.
Part: SKIN — DENTED (FUSELAGE) · airframe 30,528 hrs · 37,236 cycles
YYC- DENT IN LOWER LEFT HAND FUSELAGE SIDE SKIN JUST FORWARD OF FRAME 8805. REPAIRED IAW FOKKER SRM 53-02-02 FIGURE 1 PAGE 2 AND 53-00-00.
Part: SKIN — DENTED (FUSELAGE) · airframe 30,528 hrs · 37,236 cycles
YYC- DENT IN AFT FUSELAGE SKIN, LEFT HAND SIDE AT STATION 920. REPAIRED IAW FOKKER SRM 53-01-01 AND 53-02-02 FIGURE 1 PAGE 2.
Part: SKIN — DENTED (FUSELAGE) · airframe 30,528 hrs · 37,236 cycles
YYC- DENT IN LOWER LEFT HAND FUSELAGE SKIN JUST AFT OF FRAME 8805 BELOW THE LAP JOINT. REPAIRED IAW FOKKER SRM 53-02-02 FIGURE 1 PAGE 2.
Part: FASTENER — LOOSE (RT ELEVATOR) · airframe 30,528 hrs · 37,236 cycles
YYC- RIGHT HAND ELEVATOR OUTBOARD END HAS LOOSE FASTENERS. REPAIRED IAW FOKKER SRM 51-31-05 AND 51-70-0.
Part: SKIN — DENTED (FUSELAGE) · airframe 30,528 hrs · 37,236 cycles
YYC- DENT FROM PREVIOUS REPAIR ON FUSELAGE SKIN ON LEFT HAND SIDE BETWEEN FRAMES 4850 AND 5305 AND STRINGERS 20 AND 21. REPAIRED IAW FOKKER SRM 53-02-02 FIGURE 1 PAGE 2.
Part: ACCESS PANEL — CRACKED (RUDDER) · airframe 30,528 hrs · 37,236 cycles
YYC- ACCESS PANEL REBATE CRACKED UNDER PANEL 57V ON LEFT HAND SIDE OF RUDDER. REPAIRED IAW FOKKER SRM 51-31-01.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 30,528 hrs · 37,236 cycles
YYC- RIGHT HAND LOWER FUSELAGE SKIN PANEL ADJACENT TO RIGHT HAND STATION 1700 FLAP FAIRING REQUIRES SHEET METAL DRESS-UP. REPAIRED IAW FOKKER SRM 53-02-17 FIGURE 5.
Part: SMOKE DETECTOR — ACTIVATED (LAVATORY) · airframe 30,467 hrs · 37,177 cycles
SMF - CLIMBING THROUGH 4,000 FEET, RECEIVED REPORT THAT THE NR 2 LAV SMOKE DETECTOR WAS SOUNDING. CREW DECIDED TO RETURN TO FIELD. ON SHORT FINAL, SMOKE DETECTOR QUIT SOUNDING. REMOVED AND REPLACED APU, OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: COALESCER BAG — CONTAMINATED (AIR/CON BAY) · airframe 30,467 hrs · 37,177 cycles
SMF - CLIMBING THOUGH 2000 FEET, NOTICED OILY SMELL EMANATING FROM BLEED AIR SYSTEM. SHORTLY AFTER, BOTH NR 1 AND NR 2 LAV SMOKE DETECTORS BEGAN SOUNDING. RETURNED TO FIELD. REMOVED AND REPLACED NR 1 AND NR 2 COOLING TURBINE WATER SOCKS. PERFORMED BLEED AIR DUCTING PURGE. NO FURTHER ODOR NOTED. AIRCRAFT RETURNED TO SERVICE.
Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY) · airframe 30,467 hrs · 37,177 cycles
GEG - AFTER TAKEOFF, THE FLIGHT ATTENDENT ADVISED THE PILOT THAT LAVATORY SMOKE DETECTOR HAD ACTIVATED. AFTER RESETTING THE DETECTOR, IT ACTIVATED A SECOND TIME. UPON SECOND ACTIVATION, FLIGHT CREW DECLARED AN EMERGENCY AND RETURNED TO AIRFIELD. INSPECTION REVEALED NO EVIDENCE OF SMOKE OR FIRE. REMOVED AND REPLACED NR 1 LAVATORY SMOKE DETECTOR, OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: BATTERY — MALFUNCTIONED (CABIN) · airframe 30,223 hrs · 36,942 cycles
BOI- ROWS 12 AND 14''S CHAIR PROXIMITY LIGHTS STAY ON FOR ABOUT 4-5 MINUTES AFTER SWITCHING THEM OFF. REMOVED AND REPLACED BATTERY CARTRIDGE AT ROW 14 AND REPAIRED BROKEN WIRE AT ROW 12. OPERATIONAL CHECKS NORMAL. AIRCRAFT RETURNED TO SERVICE.
Part: SIGN — INOPERATIVE (CABIN) · airframe 30,150 hrs · 36,871 cycles
PDX- EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED EXIT SIGN ABOVE COCKPIT DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: BULB — FAILED (ROW 8) · airframe 30,076 hrs · 36,797 cycles
GEG- FORWARD EXIT SIGN AT ROW 8 HAS SEVERAL 28 VOLT LAMPS INOPERATIVE. REMOVED AND REPLACED FORWARD EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 2,995 hrs · 36,696 cycles
GEG - EXIT SIGN AT FORWARD CABIN ENTRANCE INOPERATIVE. REMOVED AND REPLACED FORWARD CABIN ENTRANCE EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: CONNECTOR — DISCONNECTED (ROW 3)
BOI - ROW 3AB EMERGENCY LIGHT INOP. RECONNECTED ELECTRICAL CONNECTION AT SEAT FRAME. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.
Part: LIGHT — INOPERATIVE (CABIN)
GEG - EMERGENCY EXIT LIGHT OVER FLIGHT COMPARTMENT DOOR WAS REPORTED INOPERATIVE. REMOVED AND REPLACED FLIGHT COMPARTMENT EXIT SIGN ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
1999
Part: POWER SUPPLY — INOPERATIVE (CABIN)
SEA- OVERHEAD EMERGENCY EXIT SIGN INOPERATIVE. REMOVED AND REPLACED BATTERY POWER SUPPLY. OPERATIONAL CHECK GOOD.
Part: CIRCUIT BOARD — INOP (CABIN)
SEVERAL LIGHTS OUT IN EMERGENCY SIGN. REMOVED AND REPLACED EMERGENCY LIGHT CIRCUIT BOARD, OPERATIONAL CHECK GOOD.
Part: CIRCUIT BOARD — FAILED (ROW 8&9)
PDX - EXIT SIGN AT ROW 8 AND 9 INOPERATIVE. REMOVED AND REPLACED EXIT SIGN CIRCUIT BOARD. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: CIRCUIT BOARD — INOP (CABIN)
GEG- FOUND EMERGENCY EXIT SIGN HAD MANY BULBS BURNED OUT. REPLACED CIRCUIT BOARD. OPERATIONAL CHECK GOOD.
Part: LIGHT — INOPERATIVE (CABIN)
SEA - CEILING EXIT SIGN AFT OF MAIN CABIN DOOR NOT ILLUMINATING. REMOVED AND REPLACED EXIT SIGN ASSEMBLY. OPERATIONAL CHECK OK.
Part: CIRCUIT BOARD — INOP (ROW 8 & 9)
CEILING EXIT SIGN AT ROW 8 AND 9 INOPERATIVE. MAINTENANCE REPLACED THE EXIT SIGN CIRCUIT BOARD, OPERATIONAL TEST NORMAL.
1998
Part: SIGN — INOP (COCKPIT DOOR)
EXIT SIGN AT COCKPIT DOOR IS OUT. MAINTENANCE REPLACED THE SIGN ASSEMBLY, OPERATIONAL TESTED NORMAL.
Part: MECHANISM — OUT OF ADJUST (PAX DOOR)
MAIN CABIN DOOR WILL NOT OPEN FROM OUTSIDE. LOCK ROLLER DOES NOT PULL OUT OF DETENTE COMPLETELY. REPAIRED IAW FOKKER MM 52-10-4, PAGE 417, PARAGRAPH B, STEP 11 AND 12.
Part: MECHANISM — OUT OF ADJUST (PAX DOOR)
MAIN CABIN DOOR FRICTION MECHANISM IS OUT OF ADJUSTMENT. REPAIRED IAW FOKKER MM 52-10-03, PAGE 583, PARAGRAPH C THROUGH F.
Part: GLASS — LOOSE (EMERGENCY EXIT)
GLASS COMING OUT OF EMERGENCY PUSH BUTTON, EXTERIOR ON SERVICE EMERGENCY DOOR. REPLACED BREAK GLASS PUSH BUTTON COVER FOR EXTERIOR SERVICE EMERGENCY DOOR.
Part: COVER — MISSING (EMER EXIT DOOR)
PDX - SERVICE EMERGENCY DOOR FORWARD TRACK SEAL IS MISSING COVER ON RIVET ATTACH STRIP. REPAIRED IAW FOKKER SRM 51-31-05.
Part: BRACKET — CRACKED (PAX DOOR)
MAIN CABIN DOOR AFT HOOK LATCH FORWARD SUPPORT BRACKET CRACKED AT TOP. REPAIRED IAW FOKKER MM 52-10-4, PAGE 501-502, PARAGRAPH 2 A AND B.
Part: MECHANISM — OUT OF ADJUST (EMER EXIT DOOR)
SERVICE EMERGENCY DOOR TOP MICROSWITCH ACTUATING ARM DOES NOT LINE UP WITH STRIKER PLATE ON DOOR. REALIGNED BRACKET AND ADJUSTED SWITCH.
Part: CLIP — CRACKED (FRAME 5305)
FRAME CLIP IS CRACKED AT FRAME 5305 AT STRINGER 43. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.
Part: SEAL — DETERIORATED (EMER EXIT DOOR)
PDX - UPPER TRACK SEAL IS DETERIORATED ON SERVICE EMERGENCY EXIT COVER. REPLACED SEAL.
Part: COVER — DETERIORATED (EMER EXIT DOOR)
PDX - GRASP HANDLE ATTACH HOLES ARE DETERIORATED ON SERVICE/EMERGENCY EXIT COVER. REPAIRED IAW FOKKER SRM 51-70-1, PAGES 1-2.
Part: COVER — DETERIORATED (EMER EXIT COVER)
PDX - SERVICE EMERGENCY EXIT DOOR COVER PLASTIC IS DETERIORATED AND CRACKING AT FORWARD UPPER CORNER. REPAIRED IAW FOKKER SRM 51-70-1, PAGES 1-2.
Part: SKIN — DENTED (PAX DOOR) · airframe 26,157 hrs · 32,999 cycles
PDX-(UPDATE FOR OPEN SDR) DENT IN PASSENGER DOOR SKIN 33 INCHES FROM BOTTOM EDGE OF DOOR, 22 INCHES BACK FROM FORWARD EDGE. PLACED DENT ON YELLOW DOT PROGRAM IAW HORIZON AIR GMM 5-5.0. REPAIRED IAW FOKKER SRM 52-02-02, FIGURE 1, PAGE 2 & 3.
Part: HANDLE — OUT OF ADJUST (PAX DOOR)
MAIN CABIN DOOR EXTERIOR EMERGENCY RELEASE HANDLE DOES NOT LOCK IN EMERGENCY POSITION. REPAIRED IAW FOKKER SRM 52-10-05, PAGE 402, PARAGRAPH B, 1 - 12.
Part: TRACKS — WORN (EMER EXIT DOOR)
PDX - SERVICE EMERGENCY DOOR TRACKS ARE ALL BEAR METAL. TREATED IAW FOKKER SRM 51-10-4.
Part: FRAME — CRACKED (FRAME 22293)
VERTICAL FRAME 22293 HAS A 1 INCH CRACK AT STRINGER 53A. REPAIRED IAW HORIZON AIR EA 4-53-572.
Part: RIVETS — LOOSE (EMER EXIT DOOR)
PDX - SERVICE EMERGENCY DOOR COVER HAS LOOSE RIVETS ON AFT DOOR TRACK SEAT. REMOVED LOOSE RIVETS. INSTALLED NEW RIVETS.
Part: ANGLE — LOOSE (VERT STAB)
HI-LOK LOOSE IN LEFT-HAND V STAB CONNECTION ANGLE 31 FORWARD OF AFT END OF CONNECTION ANGLE. REPAIRED IAW FOKKER SRM 51-31-02.
Part: CLIP — CRACKED (FRAME 50-2)
OBLIQUE FRAME 50-2 HAS A CRACKED CLIP AT STRINGER 48. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 53-10-05, PAGE 601.
Part: FRAME — CRACKED (FRAME 50-2)
FRAME 50-2 IS CRACKED TO UNKNOWN LENGTH BEHIND THE DIAGONAL BRACE MOUNT BRACKET AT STRINGER 56. REPAIRED IAW FOKKER SRM 51-10-9, PAGE 9, PARAGRAPH 4 AND SRM 53-26-04, PAGE 20, FIGURE 8, ITEM 235.
Part: MECHANISM — OUT OF ADJUST (PAX DOOR)
MAIN CABIN DOOR LATCHING SYSTEM STIFF. REPAIRED IAW FOKKER MM 52-10-01.
Part: ANGLE — LOOSE (VERT STAB)
HI-LOK LOOSE/SMOKING IN LEFT-HAND VERTICAL STAB CONNECTION ANGLE LOCATED 17 BACK FROM FORWARD END. REPAIRED IAW FOKKER SRM 51-31-02.
Part: CLIP — CRACKED (FRAME 41-2)
OBLIQUE FRAME 41-2 HAS A FRAME CLIP CRACKED BEYOND THE STOP DRILL REPAIR. REPAIRED IAW 53-02-13, PAGE 4, FIGURE 3 AND SRM 53-10-05, PAGE 601.
Part: MECHANISM — OUT OF ADJUST (PAX DOOR)
PDX - BELLVILLE WASHERS FOR FRICTION DISC ASSEMBLY FOR PASSENGER DOOR NEED ADJUSTMENT. ADJUSTED IAW FOKKER SRM 52-10-03, PAGE 502C , PARAGRAPH D, 502-503 STEP 3 E AND F.
Part: COVER — SNAGGED (PAX DOOR)
THE FORWARD AND AFT SOUND PROOFING COVERS BECAME SNAGGED IN DOOR APERTURE DURING OPENING OF MAIN CABIN DOOR. REPAIRED COMBING.
Part: CLIP — CRACKED (FRAME 50-2)
OBLIQUE FRAME 50-2 AT STRINGER 47 HAS CLIP CRACKED THROUGH A STOP DRILL HOLE. REPAIRED IAW FOKKER MM 53-10-05, PAGE 601A.
Part: CABLE — RUSTED (PAX DOOR)
EXTERIOR MAIN CABIN DOOR RELEASE HANDLE CABLE APPEARS VERY DRY AND RUSTY WHERE IT ATTACHES TO HANDLE. REPAIRED IAW FOKKER MM 20-30-09, PAGE 9.
Part: CLIP — CRACKED (FRAME 50-2)
OBLIQUE FRAME 50-2 HAS A CRACK THROUGH A CLIP THAT HAS PROGRESSED THROUGH THE STOP DRILL, NOT YET BEYOND STOP DRILL LIMITS, LOCATED AT STRINGER 50. REPAIRED IAW FOKKER MM 53-10-05, PAGE 601.
Part: HANDRAIL — CHAFED (PAX DOOR)
FORWARD EXTENDING ROD FOR PASSENGER DOOR HANDRAILS HAS CHAFE DAMAGE. REPAIRED IAW HORIZON AIR EA 4-52-162 FOR STEPS 1 AND 2 AND FOKKER SRM 51-10-04.
Part: CLIP — CRACKED (FRAME 17565)
FUSELAGE FRAME 17565 HAS A CRACK IN THE FRAME CLIP ADJACENT TO STRINGER 52. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 5 AND SRM 51-11-4 PAGE 2, PARAGRAPH E.
Part: CLIP — CRACKED (FRAME 50-2)
OBLIQUE FRAME 50-2 HAS A CLIP AT STRINGER 25 THAT IS CRACKED BEYOND LIMITS. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 3 AND SRM 51-31-01 AND 51-31-02.
Part: BRACKET — CRACKED (PAX DOOR)
MAIN CABIN DOOR HANDRAIL FORWARD INBOARD VERTICAL STANTION HAS CRACK IN BRACKET FOR QUICK RELEASE ROD. REPAIRED IAW FOKKER MM 52-10-01, PAGE 911, PARAGRAPH 4-C.
Part: CASTELLATION — CRACKED (FRAME 9305)
THERE IS A CRACKED CASTELLATION AT FRAME 9305 AND STRINGER 28. REPAIRED IAW FOKKER SRM 51-10-4.
Part: STRINGER — CRACKED (RUDDER)
STRINGER IS CRACKED AT THE NR 5 RIB INTERSECTION IN THE RUDDER. REPAIRED IAW FOKKER SRM 55-02-07, PAGE 5.
Part: RIB — CRACKED (RUDDER)
INSIDE THE RUDDER THE NR 5 RIB HAS 2 CRACKS PASSING THROUGH ATTACH CLIPS. REPAIRED IAW FOKKER SRM 51-31-05 AND SRM 51-31-01.
Part: CLIP — CRACKED (FRAME 16660)
SMALL CRACK IN FRAME CLIP AT FRAME 16660 AND STRINGER 32. ALODINE AND PRIME IAW FOKKER SRM 51-10-4.
Part: SEAL — CUT (EMER EXIT DOOR)
PDX - SERVICE EMERGENCY EXIT DOOR SEAL HAS A CUT IN BOTTOM FORWARD CORNER. INJECTED SMALL QUANTITY OF PR1422 INTO CUT AND SKINNED OVER EXTERIOR SO AS TO FUSE INNER AND OUTER PORTIONS OF SEAL.
Part: SKIN — CHAFED (EMER EXIT DOOR)
PDX - SERVICE EMERGENCY DOOR HAS CHAFE DAMAGE THAT NEEDS TO BE TREATED AND PAINTED. REPAIRED IAW FOKKER SRM 51-10-04.
Part: JAMB NUT — LOOSE (PAX DOOR)
PDX - FORWARD EXTENDING ROD FOR PASSENGER DOOR HAND RAIL ADJUSTABLE ROD END SAFETY JAM NUT NOT SECURE. SECURED AND SAFETIED JAMB NUT.
Part: TRACK — GROOVED (TE FLAP CANOE)
FLAP CANOE PANEL 82DF VERTICAL GUIDE TRACK IS GROOVED. REPAIRED IAW FOKKER MM 27-50-6, B 2-3 AND HORIZON AIR EA 4-57-180.
Part: TRACK — GROOVED (TE FLAP CANOE)
FLAP CANOE PANEL 82CH VERTICAL GUIDE TRACK HAS A GROOVE WORN INTO TRACK. REPAIRED IAW FOKKER MM 27-50-06, PAGE 802, PARAGRAPH B 2-3 AND HORIZON AIR EA 4-57-180.
Part: HANDLE — CORRODED (PAX DOOR)
MAIN CABIN DOOR EMERGENCY RELEASE HANDLE OUTSIDE FUSELAGE HAD CORROSION AND RED PAINT IS WORN OFF. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9 AND SRM 51-10-4 PAGE 8, PARAGRAPH 3 (1).
Part: SKIN — DENTED (PAX DOOR) · airframe 26,157 hrs · 32,999 cycles
PDX- (UPDATE FOR OPEN SDR) DENT IN PASSENGER DOOR SKIN 24 INCHES FROM HINGE 14 1/2 INCHES AFT OF FORWARD EDGE, PLACED DENT ON YELLOW DOT PROGRAM IAW HORIZON AIR GMM 5-5.0. REPAIRED IAW FOKKER SRM 52-02-02, FIGURE 1, PAGE 2 & 3.
Part: SKIN — DENTED (PAX DOOR) · airframe 26,157 hrs · 32,999 cycles
PDX-DENT IN PASSENGER DOOR SKIN 13 INCHES FROM BOTTOM EDGE OF DOOR. DENT PLACED ON THE YELLOW SPOT PROGRAM IAW HORIZON AIR GMM 5-5.0 REPAIRED IAW FOKKER SRM 52-02-01, PAGE 3, FIGURE 2. REPAIRED IAW FOKKER SRM 52-02-01, PAGE 3, FIGURE 2.
Part: SMOKE DETECTOR — ACTIVATED (LAVATORY)
AIRCRAFT RETURNED TO FIELD WITH BOTH SMOKE DETECTORS IN THE LAVS GOING OFF. CREW NOTED THAT THE APU WAS OFF ON TAKEOFF AND CLIMB. PURGED BLEED AIR DUCTS AND CHANGED WATER SEPARATOR FILTER SOCKS. GROUND RAN AIRCRAFT, OPERATIONAL CHECK GOOD. NO SMOKE NOTED. AIRCRAFT TEST FLIGHT SATISFACTORY.
Part: INDICATOR — FAILED (COCKPIT RADAR)
CREW REPORTED ACRID ELECTRICAL SMELL COMING FROM JUST ABOVE THE RADAR SCREEN. MAINTENANCE REMOVED AND REPLACED THE RADAR INDICATOR, OPERATION TESTED NORMAL.
Part: BULB — FAILED (CABIN)
SEVERAL LIGHTS OUT ON CENTER CABIN OVERHEAD EXIT SIGN. MAINTENANCE RELAMPED, OPERATIONALLY TESTED NORMAL.
Part: BULB — FAILED (CABIN)
LIGHTS ON EMERGENCY EXIT AT 9A INOPERATIVE. MAINTENANCE RELAMPED LIGHT ASSEMBLY, OPERATIONALLY TESTED NORMAL.
Part: BULB — FAILED (CABIN)
PDX - EXIT ROW 8 EMERGENCY EXIT LIGHT BULB OUT. MAINTENANCE RELAMPED AND OPERATIONALLY TESTED, TESTS NORMAL.
Part: BULB — FAILED (CABIN)
GEG - BOTTOM EMERGENCY EXIT LIGHT OUT BY DOOR SLIDE. MAINTENANCE RELAMPED AND OPERATIONALLY TESTED, TESTS NORMAL.
Part: BULB — FAILED (CABIN)
CEILING EMERGENCY LIGHTS INOPERATIVE AT ROWS 9 AND 14. MAINTENANCE RELAMPED, OPERATIONAL TESTED NORMAL.
Part: BULB — FAILED (CABIN)
BOTH FORWARD EXIT SIGNS HAVE LIGHTS OUT. MAINTENANCE RELAMPED BOTH FORWARD OVERHEAD 28V EXIT SIGNS. BOTH OPERATIONALLY TESTED NORMAL.
Part: BULB — FAILED (CABIN)
CENTER FORWARD EMERGENCY EXIT HAS INOPERATIVE LIGHTS. MAINTENANCE RELAMPED, OPERATIONAL TEST NORMAL.
Part: SIGN — INOPERATIVE (CABIN)
GEG - EMERGENCY EXIT LIGHT OVER COCKPIT DOOR WAS NOT ILLUMINATED WITH EMERGENCY LIGHTS IN ARM OR ON. MAINTANENCE REPLACED EXIT SIGN, CHECKS GOOD.
Part: BULB — FAILED (CABIN)
TOP EMERGENCY EXIT LIGHT AT GALLEY SERVICE DOOR INOP. RELAMPED, OPERATIONAL CHECKS GOOD.
Part: CIRCUIT CARD — INOPERATIVE (CABIN)
SEA- AFT EMERGENCY EXIT SIGN IS INOP. REPLACED CIRCUIT CARD. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: BULB — FAILED (CABIN)
RIGHT HAND FORWARD EMERGENCY LIGHT INOPERATIVE. RELAMPED, OPERATIONAL CHECKS GOOD.
Part: SLIDE — LOW PRESS (CABIN)
EMERGENCY ESCAPE SLIDE READS BELOW 2600 PSI AT 70 DEGREES F. FERRIED AIRCRAFT FROM SJC TO GEG. REPLACED ESCAPE SLIDE.
Part: BULB — FAILED (CABIN)
FORWARD EMERGENCY EXIT SIGN HAS INOP BULBS. MAINTENANCE RELAMPED, OPERATIONAL CHECK GOOD.
Part: BULB — FAILED (CABIN)
PDX - EMERGENCY LIGHT 8 A/B INOP. RELAMPED, OP CHECK GOOD.
Part: MECHANISM — LACK OF LUBE (PAX DOOR)
BIL- MAIN CABIN DOOR IS DIFFICULT TO OPEN. CLEANED AND LUBRICATED DOOR MECHANISM, OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.
Part: BULB — FAILED (CABIN)
EXIT LIGHT AT ROW 8 ON LEFT SIDE INOP. RELAMPED EXIT SIGN, OPERATIONAL CHECK GOOD.
Part: DNLOCK ACTUATOR — MALFUNCTION (RT MLG)
FLIGHT DIVERTED TO BOI, RIGHT MAIN UNSAFE LIGHT ILLUMINATED. REPLACED MAIN LANDING GEAR DOWN LOCK ACTUATOR, OPERATIONAL CHECK GOOD.
1997
Part: BATTERY — DISCHARGED (CABIN)
BOI- LEFT WING EMERGENCY EXIT SIGNS ARE WEAK. REPLACED BATTERY POWER SUPPLY FOR THE LEFT WING EMERGNECY EXIT SIGNS, OPERATIONAL CHECKS GOOD.
Part: SIGN — INOPERATIVE (CABIN)
GEG - EXIT SIGN AT FORWARD CABIN OVERHEAD NOT ILLUMINATED. INSTALLED SERVICEABLE EXIT SIGN, OPERATIONAL CHECK GOOD.
Part: BULB — FAILED (CABIN)
GEG - OVERHEAD AISLE EMERGENCY LIGHTS AT ROWS 12 AND 13 INOP. RELAMPED, OPERATIONAL CHECK GOOD.
Part: BULB — FAILED (CABIN)
GEG - EXIT SIGN ABOVE CABIN DOOR INOP. RELAMPED SIGN, OPERATIONAL CHECK GOOD.
Part: BULB — FAILED (CABIN)
EMERGENCY EXIT LIGHT FOR THE FORWARD GALLEY SERVICE DOOR IS INOP. RELAMPED EXIT SIGN, OPERATIONAL CHECKS GOOD.
Part: BULB — FAILED (CABIN)
EMERGENCY EXIT LIGHT FOR THE FORWARD GALLEY SERVICE DOOR IS INOP. RELAMPED, OPERATIONAL CHECKS GOOD.
Part: LAMP — FAILED (CABIN)
PDX - EMERGENCY EXIT LIGHT ROW 8 INOP. RELAMPED, OPERATIONAL CHECK GOOD.
Part: BULB — FAILED (CABIN)
PDX- EMERGENCY LIGHTS IN THE COCKPIT AND AT THE CABIN ENTRANCE ARE INOP. REPLACED LAMP ASSEMBLIES, OPERATIONAL CHECKS GOOD.
Part: BULB — FAILED (CABIN)
BOI - EXIT LIGHT, ROW 8 CDE OUT. RELAMPED SAME, OP'S CHECK GOOD.
Part: BULB — FAILED (CABIN)
GEG- EMERGENCY EXIT LIGHT BULB INOP. REPLACED FORWARD FACING LIGHT ASSEMBLY AT THE AISLE POSITION. OPERATIONAL CHECK GOOD.
Part: CIRCUIT BREAKER — DIRTY (APU FIRE WARN)
SEA- APU FIRE EXT WILL NOT TEST. CLEANED AND REINSTALLED THE APU FIRE WARNING CONTROL CIRCUIT BREAKER, OPERATIONAL CHECKS GOOD.
Part: CONTROLLER — MALFUNCTION (COCKPIT)
SEA - NR 2 ENGINE FIRE WARNING WILL NOT TEST. REPLACED NR 2 FIRE WARNING CONTROLLER, OPERATIONAL TEST GOOD.
Part: BULB — FAILED (CABIN)
EMERGENCY EXIT LIGHT AT ROW 8CDE IS INOPERATIVE. RELAMPED EMERGENCY EXIT LIGHT AT ROW 8CDE, OPERATIONAL CHECK GOOD.
Part: BULB — FAILED (CABIN)
EMERGENCY EXIT LIGHT 9A INOP. RELAMPED AS NECESSARY, OPERATIONAL CHECK GOOD.
Part: POWER SUPPLY — INOPERATIVE (CABIN)
BOTH OVERWING EMERGENCY 3 VOLT LIGHT BULBS INOP RIGHT HAND SIDE. REPLACED POWER SUPPLY LV55, OPERATIONAL CHECKED GOOD.
Part: PWR SUPPLY — INOPERATIVE (CABIN)
LEFT OVERWING EMERGENCY EXIT SIGN INOP. REPLACED POWER SUPPLY, OPERATIONAL CHECKS GOOD.
Part: RELAY — FAILED (COCKPIT)
COCKPIT EMERGNCY LIGHTS DO NOT ILLUMINATE WHEN BATTERIES ARE TURNED ON. REPLACED EMERGENCY LIGHTS RELAY LV3-164, OPERATIONAL CHECKS GOOD.
Part: BULB — FAILED (CABIN)
GEG - NUMEROUS 28 VOLT EMERGENCY EVACUATION LIGHTS ARE INOP IN THE CABIN OVERHEAD. REPLACED LIGHT BULBS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: BULB — FAILED (CABIN)
PDX - EMERGENCY EXIT LIGHT AT ROW 9 WINDOW EXIT HAS AN INOP BULB. REPLACED LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: BULB — FAILED (CABIN)
GEG- SEVERAL EMERGENCY LIGHT INOP. RELAMPED LIGHTS. OPERATIONAL CHECK GOOD, AIRCRAFT RETURNED TO SERVICE.
Part: BULB — FAILED (CABIN)
EMERGENCY EXIT LIGHT AT ROW 9 OUT. REPLAMPED EMERGENCY EXIT LIGHT, OPS CHECK GOOD.
Part: BULBS — FAILED (CABIN)
SEA - SEAT 8E EMERGENCY SIGN OVERHEAD 3V AND 28V LAMPS ARE INOPERATIVE. BULBS WERE REPLACED AND SIGN OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.
1996
Part: BATTERY PACK — DISCHARGED (CABIN)
CLT - THE FORWARD EMERGENCY LIGHTS STAYED ILLUMINATED WITH POWER ON. MAINTENANCE REPLACED THE FORWARD EMERGENCY LIGHT BATTERY PACK. (M)
Part: SEQ VALVE — MALFUNCTIONED (LANDING GEAR)
CLT - FLT 799 - ON GEAR EXTENSION, CREW RECEIVED RED GEAR DOOR LIGHT. CREW RECYCLED THE GEAR TWICE WITH SAME INDICATION. GEAR WAS MANUALLY EXTENDED AND TOWER FLYBY CONDUCTED. FLIGHT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND THE DOOR UP STOP LOOSE AND ADJUSTED IT. THE GEAR DOWN SEQUENCE VALVE WAS REPLACED AS A PRECAUTION. (M)
Part: SELECTOR VLV — FAILED (NLG DOORS)
CLT - FL 568 - NOSE GEAR RED DOOR LIGHT REMAINED ON AFTER GEAR RETRACTION. CREW ACCOMPLISHED ABNORMAL PROCEDURE. LIGHT WENT OUT AFTER GEAR WAS RECYCLED. MAINTENANCE REMOVED AND REPLACED THE FOLLOWING ITEMS; NOSE WHEEL STEERING SELECTOR, P/N 714540 AND NLG DOOR ACTUATOR, P/N 12500-1 AND NLG DOOR SELECTOR VALVE, P/N 71539 AND NLG SELECTOR VALVE, P/N 71538-1. REFERENCE USAAF96047.
Part: SELECTOR VLV — MALFUNCTIONED (NLG STEERING)
CLT - FL 568 - NOSE GEAR RED DOOR LIGHT REMAINED ON AFTER GEAR RETRACTION. CREW ACCOMPLISHED ABNORMAL PROCEDURE. LIGHT WENT OUT AFTER GEAR WAS RECYCLED. MAINTENANCE REMOVED AND REPLACED THE FOLLOWING ITEMS; NOSE WHEEL STEERING SELECTOR, P/N 714540 AND NLG DOOR ACTUATOR, P/N 12500-1 AND NLG DOOR SELECTOR VALVE, P/N 71539 AND NLG SELECTOR VALVE, P/N 71538-1. (M)
Part: SELECTOR VLV — FAILED (NLG DOORS)
CLT - FL 568 - NOSE GEAR RED DOOR LIGHT REMAINED ON AFTER GEAR RETRACTION. CREW ACCOMPLISHED ABNORMAL PROCEDURE. LIGHT WENT OUT AFTER GEAR WAS RECYCLED. MAINTENANCE REMOVED AND REPLACED THE FOLLOWING ITEMS; NOSE WHEEL STEERING SELECTOR, P/N 714540 AND NLG DOOR ACTUATOR, P/N 12500-1 AND NLG DOOR SELECTOR VALVE, P/N 71539 AND NLG SELECTOR VALVE, P/N 71538-1. REFERENCE USAAF96047.
Part: ACTUATOR — FAILED (NLG)
CLT - FL 568 - NOSE GEAR RED DOOR LIGHT REMAINED ON AFTER GEAR RETRACTION. CREW ACCOMPLISHED ABNORMAL PROCEDURE. LIGHT WENT OUT AFTER GEAR WAS RECYCLED. MAINTENANCE REMOVED AND REPLACED THE FOLLOWING ITEMS; NOSE WHEEL STEERING SELECTOR, P/N 714540 AND NLG DOOR ACTUATOR, P/N 12500-1 AND NLG DOOR SELECTOR VALVE, P/N 71539 AND NLG SELECTOR VALVE, P/N 71538-1. REFERENCE USAAF96047.
Part: ENG DRIVEN PUMP — FAILED (NR 1 ENG)
CLT - FL 498 - ON DESCENT INTO CLT, CREW LOST UTILITY HYDRAULIC SYSTEM. CAPTAIN EXTENDED THE LANDING GEAR AND FLAPS USING ALTERNATE PROCEDURE. NO EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY. MAINTENANCE REPLACED NR 1 ENGINE DRIVEN PUMP AND PRESSURE FILTER. THE HYDRAULIC SYSTEM WAS SERVICED, THE ENGINE WAS RUN AND LEAK TESTED AND ALL FLIGHT CONTROLS WERE OPS CHECKED AS NORMAL. (M)
Part: ACCESS DOOR — NOT SECURED (LT AIR COND SYST)
PIT - FLT 682 - AFTER TAKEOFF AND REACHING 8,000 FEET, CREW WAS UNABLE TO PRESSURIZE AIRCRAFT. FLIGHT RETURNED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPOSITIONED/SECURED LEFT AIR CONDITIONING ACCESS DOOR.
Part: SKIN — CRACKED (BS 2620/2200)
PIT - DURING SIP VISIT INSPECTION, FOUND 1.5 INCH CRACK RIGHT NOSE LANDING GEAR BAY SKIN STATION 2620 AND 2200, SIP REF 53-10-19. STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER PER SRM 53-02-07. (M)
Part: SKIN — CRACKED (BS 4850)
PIT - DURING SIP VISIT INSPECTION, FOUND .375 INCH CRACK UPPER AFT CORNER SKIN OF SERVICE DOOR FRAME AT STATION 4850, REF SIP 53-10-20. INSTALLED DOUBLER REPAIR PER SRM 53-02-16. (M)
1995
Part: ENGINE — VIBRATING (RIGHT)
CRW - FL 551 - EN ROUTE CLE-CLT, CREW EXPERIENCED VIBRATION FROM RIGHT ENGINE. UPON POWER REDUCTION, THE VIBRATION BECAME SEVERE. CREW SHUT DOWN ENGINE (SET 12 MINUTES), DECLARED AN EMERGENCY DIVERTED TO CRW. FLIGHT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT ENGINE. (M)
Part: WEB — DAMAGED (WING)
CLT - CLT INSPECTION VISUALLY FOUND WEB NR 4 CRUSHED 4 INCH BETWEEN RIB NR 2 AND NR 4 LOWER FLANGE ON TAILBOX STRUCTURE. FABRICATED NEW WEB. REPAIRED WEB NR IV AS PER SRM 57-22-03. (M)
Part: WEB — DAMAGED (WING)
CLT - CLT INSPECTION VISUALLY FOUND WEB NR 3 CRUSHED 10 INCH ALONG ITS LENGTH BETWEEN RIB NR 2 AND NR 4 OF LOWER FLANGE ON TAIL BOX STRUCTURE. REPLACED WEB NR 3 AS PER SRM 57-22-03. (M)
Part: SKIN — DAMAGED (WINGS)
CLT - CLT INSPECTION VISUALLY FOUND 4 INCH BY 6 INCH TEARS THROUGH SKIN AT WEBS 3 AND 4 BETWEEN RIBS 2 AND 4 OF LOWER SKIN TAIL BOX STRUCTURE. FABRICATED NEW SKIN. REPLACED LOWER SKIN ON TAIL BOX STRUCTURE PER SRM 51-11-42 AND 57-01-00. (M)
Part: RIB — CRACKED (NR 4)
CLT - .5 INCH CRACK AT NR 4 FORWARD CAP RIB AT LOWER FLANGE RADIUS AND TORQUE ROD CUT OUT. CRACK WAS VISUALLY FOUND BY CLT INSPECTION. REPAIRED NR 4 CAP RIB. FABRICATED NEW RIB, PER SRM 57-02-03 AND SRM 20-30-06. (M)
Part: TIRE — FAILED (LT MLG)
CAPTAIN ADVISED THAT ON TAKEOFF ROLL AND AND JUST AFTER REACHING V2, A STRONG VIBRATION WAS NOTICED. A PRECAUTIONARY FLY-BY WAS MADE BY CLT TOWER AND THE LEFT INBOARD TIRE WAS APPARENTLY BLOWN. NO EMERGENCY WAS DECLARED, HOWEVER, CFR WAS CALLED OUT BY ATC. THE FLIGHT RETURNED TO FIELD CLT AND LANDED WITHOUT INCIDENT. (M)
Part: FUEL VALVE — INOPERATIVE (APU)
BWI - FLT NR 0451 - EN ROUTE TO CLT, THE APU FAILED. THE CAPTAIN COULD NOT RESTART. THE DECISION WAS MADE TO DIVERT TO BWI. MAINTENANCE REPLACED THE APU FUEL SOLENOID VALVE AS A PRECAUTION AND THE FUEL FILTER. OPERATIONS CHECKED GOOD. (M)
Part: FUEL FILTER — INOPERATIVE (APU)
BWI - FLT NR 0451 - EN ROUTE TO CLT, THE APU FAILED. THE CAPTAIN COULD NOT RESTART. THE DECISION WAS MADE TO DIVERT TO BWI. MAINTENANCE REPLACED THE APU FUEL SOLENOID VALVE AS A PRECAUTION AND THE FUEL FILTER. OPERATIONS CHECKED GOOD.
Part: BEAM — CRACKED (FS 17065)
PIT - DURING SCHEDULED SIP VISIT, FOUND 1.5 INCH CRACK IN REAR PRESSURE BULKHEAD STATION 17065 HORIZONTAL BEAM NR 3 AT BL 425 RT HIGH FREQUENCY EDDY CURRENT INSPECTION SIP REF 53-10-03. STOP DRILLED CRACK AND INSTALLED ANGLE AND DOUBLER REPAIR PER USAIR EA 30104.
Part: SKIN — CRACKED (DOOR OPENING)
PIT - DURING SCHEDULED SIP VISIT, FOUND .5 INCH CRACK SERVICE EMERGENCY DOOR APERTURE AFT LOWER CORNER EDDY CURRENT INSPECTION REF SIP 53-10-20. ACCOMPLISHED SHEET METAL REPAIR PER SRM 53-02-16 PG 7, 8 AND 11. (M)
Part: SKIN — CRACKED (FS 347)
PIT - DURING Q-3 CHECK INSPECTION, FOUND .25 INCH SKIN CRACK AT RIVET HEAD STATION 347 BETWEEN LONGERON 23L AND 24L. INSTALLED DOUBLER REPAIR PER SRM 53-04 FIG 38. (M)
Part: FITTING — CRACKED (FS 691)
PIT - DURING Q-3 CHECK INSPECTION, FOUND .25 INCH CRACK AT BOLT HOLE AT REAR SPAR KEEP FITTING STATION 691 LEFT WHEEL WELL. INSTALLED DOUBLER REPAIR PER SRM 53-03 FIG 11. (M)
Part: TRACK — CORRODED (FS 197-237)
PIT - DURING Q-3 CHECK INSPECTION, FOUND LEVEL I CORROSION PREVIOUSLY REWORKED LEFT INBOARD SEAT TRACK STATION 197-237. SPLICED IN SECTION OF SEAT TRACK PER SRM 53-05 FIG 4F. (M)
Part: SKIN — DENT (FS 219)
PIT - DURING Q-3 CHECK INSPECTION, FOUND DENT OUT OF LIMITS JUST AFT OF NOSE JACK PAD STATION 218 LONGERON 30. INSTALLED INTERNAL DOUBLER PER SRM 53-04 FIG 38 EFG. (M)
Part: SKIN — DAMAGED (BS 229)
PIT - DURING Q-3 CHECK INSPECTION, FOUND TEMPORARY REPAIR INSTALLED STATION 229 LONGERON 17L TO LONGERON 18L. INSTALLED FLUSH REPAIR PER SRM 53-04 FIG 47. (M)
Part: SKIN — DAMAGED (AFT OF NLG DOOR)
PIT - DURING Q-3 INSPECTION, FOUND TEMPORARY REPAIR INSTALLED RT AFT NOSE GEAR DOOR HINGE. INSTALLED DOUBLER REPAIR PER USAIR TYPICAL REPAIR 53-30-09. (M)
Part: SKIN — CRACKED (NLG WW)
PIT - DURING SCHEDULED SIP VISIT, FOUND .25 INCH CRACK 2 EACH FUSELAGE SKIN JUST FORWARD OF RT CORNER NOSE WHEEL WELL CUTOUT, EDDY CURRENT INSPECTION SIP REF 53-10-24. INSTALLED REPAIR PER SRM 53-02-18 FIG 10. (M)