N478US

Part: ACM — ODOR (A/C BAY) · airframe 35,023 hrs · 41,755 cycles

PDX - STRONG EXHAUST ODOR COMING FROM THE NUMBER ONE AIR CYCLE MACHINE. PLACED AIR CYCLE MACHINE ON MEL 21-1, RSI 330954.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 35,005 hrs · 41,737 cycles

SEA- ALL EMERGENCY LIGHTS BATTERY POWER SUPPLIES ARE DEAD. REPLACED ALL EMERGENCY LIGHT BATTERY POWER SUPPLIES. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. THE BATTERY POWER SUPPLIES REPLACED ARE: S/N 1112 (8859,8668), S/N 1151 (8896, 8717), S/N 2357 (9228, 9092) S/N 345 (3391, 3116) S/N 476 (14091, 14926) S/N 480 (9319, 9253) S/N 877 (10127, 10541) S/N 886 (8859, 8668).

Part: SIGN — INOPERATIVE (CABIN) · airframe 34,904 hrs · 41,653 cycles

GEG-EXIT SIGN FORWARD CABIN INOPERATIVE. REMOVED AND REPLACED SIGN. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 34,808 hrs · 41,572 cycles

BOI - EVACUATION LIGHT ON SEAT 12A,B IS INOPERABLE. REPAIRED BROKEN WIRE. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: POWER SUPPLY — WEAK · airframe 34,691 hrs · 41,469 cycles

PDX - AFT LEFT CABIN EMERGENCY BATTERY PACK IS WEAK. REMOVED AND REPLACED AFT LEFT BATTERY PACK. OPERATIONAL CHECK IS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 34,585 hrs · 41,391 cycles

GEG - FORWARD, MIDDLE, AND AFT EXIT SIGNS INOPERABLE. REMOVED AND REPLACED THE FORWARD, MIDDLE, AND AFT EXIT SIGNS. OPERATIONAL CHECK IS GOOD, AIRCRAFT RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 33,926 hrs · 40,816 cycles

GEG- EMERGENCY EXIT SIGN, FORWARD SIDE OF ROW 8 INOP. REMOVED AND REPLACED SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: RELAY — FAILED (EMERG LIGHTS) · airframe 33,878 hrs · 40,768 cycles

SEA - EMERGENCY AND EVACUATION LIGHTS ILLUMINATED IN THE ARM POSITION. REMOVED AND REPLACED EMERGENCY LIGHTING CONTROL PANEL RELAY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 33,728 hrs · 40,643 cycles

BOI - EXIT SIGN AT CABIN ENTERENCE, AND AT OVER FLIGHT COMPARTMENT DOOR INOPERATIVE. REMOVED AND REPLACED EXIT SIGNS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 33,728 hrs · 40,643 cycles

BOI - MID CABIN EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SIGN — DEFECTIVE (CABIN) · airframe 33,364 hrs · 40,295 cycles

PDX - FORWARD CABIN EXIT SIGN WAS REPORTED DIM. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CIRCUIT BOARD — FAILED (CABIN) · airframe 33,245 hrs · 40,184 cycles

GEG-EXIT SIGN ABOVE COCKPIT DOOR INOPERATIVE IN 28V POSITION. REPLACED LIGHT CIRCUIT BOARD. LIGHTS CHECK GOOD IN 3V AND 28V POSITION. AIRCRAFT RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 32,642 hrs · 39,635 cycles

BOI - MID CABIN EXIT LIGHT (AFT FACING) FOUND INOPERATIVE. REMOVED AND REPLACED EXIT SIGN ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CIRCUIT BOARD — BURNED OUT (CABIN) · airframe 32,602 hrs · 39,599 cycles

SEA-EMERGENCY EXIT SIGNS ABOVE GALLEY AND COCKPIT DOOR HAVE SEVERAL INOPERATIVE BULBS. REPLACED BULB CIRCUIT BOARD ON 1 AND 2 EXIT SIGN POSITIONS. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 32,593 hrs · 39,591 cycles

PDX-CAPTAINS EMERGENCY FLASHLIGHT LED NOT FLASHING. REPLACED FLASHLIGHT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 31,300 hrs · 37,850 cycles

PDX - CHARGING INDICATOR ON EMERGENCY FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY FOR FLASHLIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: A/C PACK — VIBRATION (PACK BAY) · airframe 32,088 hrs · 39,118 cycles

BZN - VIBRATION WAS FELT DURING DESCENT. DIVERTED FROM BTM TO BZN. PLACED CABIN PACK ON DEFERRED MTX LIST. OPERATION CHECK FLIGHT GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BULB — FAILED (CABIN) · airframe 28,507 hrs · 34,880 cycles

BOI - FORWARD FACING OVERWING EXIT SIGN INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEMBLEY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SEPARATOR — CONTAMINATED (COCKPIT ACM) · airframe 31,790 hrs · 38,828 cycles

PDX - CREW REPORTED SLIGHT BURNT OIL SMELL COMING FROM THE FLIGHT COMPARTMENT ACM. REMOVED AND REPLACED FLIGHT COMPARTMENT CONDENSATION BAG. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CIRCUIT BOARD — FAILED (CABIN) · airframe 31,612 hrs · 38,666 cycles

SEA - FOUND EXIT SIGN ABOVE FLIGHT COMPARTMENT DOOR TO HAVE BURNT OUT LAMPS. REMOVED AND REPLACED EXIT SIGN CIRCUIT BOARD. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 30,644 hrs · 37,703 cycles

BOI- EMERGENCY EVACUATION LIGHTS ROW 12, 13, 14 STAY ON AFTER MAIN BATTERIES ARE TURNED OFF. REMOVED AND REPLACED ROW 14 UNDER SEAT BATTERY PACK TRAY. OPERATIONAL TEST GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 30,584 hrs · 37,638 cycles

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

Part: DOOR — OUT OF RIG (CARGO BAY) · airframe 30,576 hrs · 37,630 cycles

PDX- CENTER CARGO DOOR EXCEEDS SRM 51-50 MISMATCH LIMITATIONS WITH AIRCRAFT PRESSURIZED. PRESSURIZED AIRCRAFT ALL EDGES WITHIN LIMITS IAW FOKKER SRM 51-50-0 TABLE 5.

Part: RIVET — LOOSE (FUSELAGE) · airframe 30,576 hrs · 37,630 cycles

PDX- LOOSE RIVET AT STATION 8200 JUST OUTBOARD OF PANEL 82DH. REPAIRED IAW FOKKER SRM 51-31-01.

Part: SKIN — CRACKED (FUSELAGE) · airframe 30,576 hrs · 37,630 cycles

PDX- FUSELAGE SKIN CRACKED BETWEEN FRAMES 19975 AND 20075, STRINGERS 39 AND 40 AT TWO ATTACH RIVETS FOR V-STAB CLOSING ANGLE. REPAIRED IAW HORIZON AIR EA 4-53-1060, FOKKER SRM 51-31-01, AND FOKKER SRM 51-30-02.

Part: FLANGE — CRACKED (GALLEY) · airframe 30,576 hrs · 37,630 cycles

PDX- AFT GALLEY LOWER RIGHT HAND SUPPORT FLANGE IS CRACKED AT CENTER NUT PLATE. REPAIRED IAW FOKKER SRM 4-53-1066.

Part: SKIN — GOUGED (CARGO DOOR) · airframe 30,576 hrs · 37,630 cycles

PDX- A 2 INCH GOUGE ON AFT CARGO DOOR INNER SKIN. REPAIRED IAW FOKKER SRM 51-10-01 AND 52-02-05, PAGE 2 AND 3, FIGURE 1 AND FOKKER SRM 51-31-05.

Part: FLANGE — CRACKED (COAT CLOSET) · airframe 30,576 hrs · 37,630 cycles

PDX- AFT GALLEY COAT CLOSET, LOWER LEFT HAND SUPPORT FLANGE HAS CRACKS AROUND COAT CLOSET ATTACHMENT NUT PLATES (2 EACH). REPAIRED IAW FOKKER SRM 53-02-05 PAGE 3.

Part: FITTING — DAMAGED (TE FLAP) · airframe 30,576 hrs · 37,630 cycles

PDX- RIGHT HAND OUTBOARD FLAP INBOARD LOWER FITTING THAT SUPPORTS THE T-LEVERS RIG PIN HOLE IS DAMAGED AND T-LEVER IS SCRATCHED. REPAIRED IAW HORIZON EA 4-57-384.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 30,576 hrs · 37,630 cycles

PDX- FLOORBEAM CRACKED BELOW NR 1 GALLEY, FRAME 3820, BL 5R. REPAIRED IAW HORIZON AIR EA 4-53-930.

Part: SKIN — CORRODED (RT WING) · airframe 30,576 hrs · 37,630 cycles

RIGHT HAND WING FUEL ACCESS APERTURE 72A NUMEROUS HOLES HAVE LIGHT FRETTING CORROSION AROUND THEM. REPAIRED IAW FOKKER SRM 51-10-04 PAGE 9.

Part: ANGLE — CRACKED (RT WING) · airframe 30,576 hrs · 37,630 cycles

PDX- RIGHT HAND WING TO FUSELAGE ATTACH ANGLE CRACKED AT STATION 1700 Z STRINGER STATION 1825. REPAIRED IAW FOKKER SRM 51-31-01 AND FOKKER SRM 51-30-02.

Part: PANEL — CRACKED (RT WING) · airframe 30,576 hrs · 37,630 cycles

PDX- REBATE OF RIGHT HAND WING FUEL PANEL 74D HAS A CRACK INSIDE ONE OF THE FASTENER HOLES. REPAIRED IAW HORIZON AIR EA 4-57-373.

Part: PANEL — CRACKED (RT WING) · airframe 30,576 hrs · 37,630 cycles

REBATE OF RIGHT HAND WING FUEL PANEL 74A HAS TWO CRACKS INSIDE TWO OF THE FASTENER HOLES. REPAIRED HOLES IAW HORIZON AIR EA 4-57-373.

Part: PANEL — CRACKED (LT WING) · airframe 30,576 hrs · 37,630 cycles

PDX- REBATE OF LEFT HAND WING FUEL PANEL 73D HAS A CRACK INSIDE ONE OF THE FASTENER HOLES. REPAIRED IAW HORIZON AIR EA 4-57-373.

Part: PANEL — CRACKED (LT WING) · airframe 30,576 hrs · 37,630 cycles

PDX- REBATE OF LEFT HAND WING FUEL PANEL 73A HAS A CRACK INSIDE ONE OF THE FASTENER HOLES. REPAIRED IAW HORIZON AIR EA 4-57-373.

Part: FRAME — CRACKED (FUSELAGE) · airframe 30,576 hrs · 37,630 cycles

PDX- FRAME TO SKIN CASTELLATION CRACKED AT FRAME 20075 AND INBOARD OF STRINGER 39. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 6, FIGURE 4.

Part: LOCK — BROKEN (RUDDER) · airframe 30,576 hrs · 37,630 cycles

PDX- BROKEN LOCK - DEVICE OF RUDDER - SHANK ON RUDDER. REPAIRED IAW FOKKER SRM 55-02-07, PAGES 10-11.

Part: STRINGER — NICKED (RT WING) · airframe 30,576 hrs · 37,630 cycles

PDX- RIGHT HAND WING TOP SKIN STRINGERS BETWEEN WS 5280 AND WS 7020 HAVE NUMEROUS AREAS WITH BARE METAL LIGHT ABRASIONS AND SMALL NICKS THAT HAVE LIGHT SURFACE CORROSION DEVELOPING. REPAIRED IAW FOKKER SRM 51-10-04 PAGE 9.

Part: CHANNEL — DAMAGED (RT WING) · airframe 30,576 hrs · 37,630 cycles

PDX- RIGHT HAND WING INTERNAL RIB LOWER U-CHANNEL AT WS 7600 HAS TOOL MARKS INSIDE CHANNEL BETWEEN BOTTOM SKIN STRINGERS 2.17 AND 2.15. REPAIRED IAW FOKKER SRM 57-01-01 PAGE 4.

Part: STRINGER — CORRODED (RT WING) · airframe 30,576 hrs · 37,630 cycles

PDX- RIGHT HAND WING TOP SKIN STRINGERS BETWEEN WS 4700 AND WS 5280 HAVE NUMEROUS AREAS OF LIGHT ABRASION AND SMALL NICKS THAT HAVE LIGHT SURFACE CORROSION DEVELOPING. REPAIRED IAW FOKKER SRM 51-10-04.

Part: STRINGER — NICKED (RT WING) · airframe 30,576 hrs · 37,630 cycles

PDX- RIGHT HAND WING TOP SKIN STRINGERS BETWEEN WS 7020 AND WS 8200 HAVE NUMEROUS AREAS WITH BARE ALUMINUM LIGHT ABRASIONS AND SMALL NICKS THAT HAVE LIGHT SURFACE CORROSION DEVELOPING. REPAIRED IAW FOKKER SRM 51-10-04.

Part: RIB — DAMAGED (RT WING) · airframe 30,576 hrs · 37,630 cycles

PDX- RIGHT HAND WING FORGED RIB AT WS 2635 TOP FLANGE INBOARD EDGE HAS TOOL DAMAGE BETWEEN TOP SKIN STRINGERS 2.37 AND 2.38 AND BELOW STRINGER 2.36. REPAIRED IAW FOKKER SRM 57-01-01 PAGE 5.

Part: CHANNEL — DAMAGED (RT WING) · airframe 30,576 hrs · 37,630 cycles

PDX- RIGHT HAND WING INTERNAL RIB LOWER O CHANNEL AT WS 7600 HAS TOOL MARKS INSIDE CHANNEL BETWEEN BOTTOM SKIN AT STRINGERS 2.8 AND 2.7. REPAIRED IAW FOKKER SRM 57-01-01 PAGE 4.

Part: STRINGER — NICKED (RT WING) · airframe 30,576 hrs · 37,630 cycles

PDX- RIGHT HAND WING TOP SKIN STRINGER INSIDE 74G BETWEEN WS 9270 AND WS 9910 HAVE NUMEROUS AREAS OF BARE ALUMINUM LIGHT ABRASIONS AND SMALL NICKS THAT HAVE LIGHT SURFACE CORROSION DEVELOPING. REPAIRED IAW FOKKER SRM 51-10-04.

Part: STRINGER — NICKED (RT WING) · airframe 30,576 hrs · 37,630 cycles

PDX- RIGHT HAND WING TOP SKIN STRINGERS BETWEEN WS 10550 AND WS 11190 HAVE NUMEROUS AREAS OF BARE ALUMINUM, LIGHT ABRASIONS AND SMALL NICKS THAT HAVE LIGHT SURFACE CORROSION DEVELOPING. REPAIRED IAW FOKKER SRM 51-10-04.

Part: STRINGER CLIP — DAMAGED (RT WING) · airframe 30,576 hrs · 37,630 cycles

PDX- RIGHT HAND WING TOP SKIN STRINGERS 2.34 AND 2.36 FORWARD TIE CLIPS TO RIB 8780 HAVE UNTREATED CHAFE DAMAGE ON FORWARD EDGE. REPAIRED IAW FOKKER SRM 57-01-01 PAGE 3.

Part: STRINGER — SCRATCHED (RT WING) · airframe 30,576 hrs · 37,630 cycles

PDX- RIGHT HAND WING TOP SKIN STRINGER 2.31 FORWARD FACE HAS A SCRATCH 4 INCHES INBOARD OF WS 9270. REPAIRED IAW FOKKER SRM 57-01-01 PAGE 3 AND 5.

Part: STRINGER — NICKED (RT WING) · airframe 30,576 hrs · 37,630 cycles

PDX- RIGHT HAND WING TOP SKIN STRINGERS BETWEEN WS 9910 AND WS 10550 HAVE NUMEROUS AREAS OF BARE ALUMINUM, LIGHT ABRASIONS AND SMALL NICKS THAT HAVE LIGHT SURFACE CORROSION DEVELOPING. REPAIRED IAW FOKKER SRM 51-10-04.

Part: WEB — DENTED (ACM BAY) · airframe 30,576 hrs · 37,630 cycles

PDX- DENT IN LEFT HAND AIR CYCLING MACHINE COMPARTMENT WALL LOCATED NEAR THE FORWARD LOWER AIR CYCLING MACHINE MOUNT BRACKET. REPAIRED IAW HORIZON AIR EA 4-53-1043.

Part: STRINGER — CORRODED (RT WING) · airframe 30,576 hrs · 37,630 cycles

PDX- RIGHT HAND WING TOP SKIN STRINGER 2.31 FORWARD FLANGE HAS CORROSION 1 INCH OUTBOARD OF WS 9270. REPAIRED IAW FOKKER SRM 51-10-04.

Part: STIFFENER — CHAFED (FUSELAGE) · airframe 30,576 hrs · 37,630 cycles

PDX- STIFFENER BEAM, RIGHT SIDE AT FRAME 17565 CHAFED. REPAIRED IAW HORIZON AIR EA 4-53-1058.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 30,576 hrs · 37,630 cycles

PDX- GOUGE IN SEAT TRACK, BL 600R, BETWEEN FRAMES 5805 AND 6305. REPAIRED IAW HORIZON AIR EA 4-53-1059.

Part: STRINGER — NICKED (RT WING) · airframe 30,576 hrs · 37,630 cycles

PDX- RIGHT HAND WING TOP SKIN STRINGERS 2.34 AND 2.35 HAVE SMALL NICKS IN VICINITY OF CUTOUTS FOR OVERFLOW VALVE AND MAGNASTIC FLOAT. REPAIRED IAW FOKKER SRM 57-01-01 PAGE 3 AND 5.

Part: STRINGER — NICKED (RT WING) · airframe 30,576 hrs · 37,630 cycles

PDX- RIGHT HAND WING TOP SKIN STRINGERS BETWEEN WS 8780 AND WS 9270 HAVE NUMEROUS AREAS OF BARE ALUMINUM LIGHT ABRASIONS AND SMALL NICKS, THAT HAVE LIGHT SURFACE CORROSION DEVELOPING. REPAIRED IAW FOKKER SRM 51-10-04.

Part: STRINGER — CHAFED (RT WING) · airframe 30,576 hrs · 37,630 cycles

PDX- RIGHT HAND WING TOP SKIN STRINGERS 2.32, 2.33 AND 2.34 FORWARD TIE CLIPS TO RIB 9910 HAVE UNTREATED CHAFE DAMAGE ON FORWARD EDGE. REPAIRED IAW FOKKER SRM 57-01-01 PAGE 3 AND 5.

Part: STRINGER — NICKED (RT WING) · airframe 30,576 hrs · 37,630 cycles

PDX- RIGHT HAND WING TOP SKIN AND STRINGERS BETWEEN WS 8200 AND WS 8770 HAVE NUMEROUS AREAS OF BARE ALUMINUM LIGHT ABRASIONS AND SMALL NICKS THAT HAVE LIGHT SURFACE CORROSION DEVELOPING. REPAIRED IAW FOKKER SRM 51-10-04.

Part: PANEL — CORRODED (RT WING) · airframe 30,576 hrs · 37,630 cycles

PDX - RIGHT WING FUEL ACCESS PANEL 74B ALL SCREW HOLES HAVE FRETTING CORROSION. REPAIRED IAW FOKKER SRM 57-01-01, PAGE 5, PARAGRAPH B.

Part: SKIN — CORRODED (RT WING) · airframe 30,576 hrs · 37,630 cycles

PDX- RIGHT HAND WING FUEL ACCESS APERTURE 74G HAS NUMEROUS SCREW HOLE WITH LIGHT FRETTING AND A FEW LIGHT SCRATCHES AROUND THEM. REPAIRED IAW FOKKER SRM 51-10-04, PARAGRAPH 4B, PAGE 9.

Part: WEB — CRACKED (NLG WW) · airframe 30,576 hrs · 37,630 cycles

PDX- TYPE 1 CRACK AT RIGHT HAND SKIN PANEL AFT OF NOSE LANDING GEAR BAY. REPAIRED IAW FOKKER SRM 53-02-18, FIGURE 10 ACCORDING TO HORIZON AIR EA 4-53-1056.

Part: SKIN — CORRODED (RT WING) · airframe 30,576 hrs · 37,630 cycles

PDX - RIGHT WING FUEL ACCESS APERTURE 74F HAS LIGHT FRETTING CORROSION AND A FEW LIGHT SCRATCHES AROUND NUMEROUS SCREW HOLES. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4B.

Part: PANEL — CORRODED (WING) · airframe 30,576 hrs · 37,630 cycles

PDX- LIGHT FRETTING CORROSION GROUND SCREW HOLES ON FUEL PANEL APERTURE 73A. REPAIRED IAW FOKKER SRM 51-10-4.

Part: SKIN — CORRODED (RT WING) · airframe 30,576 hrs · 37,630 cycles

PDX - RIGHT FUEL ACCESS APERTURE 74C HAS NUMEROUS SCREW HOLES WITH FRETTING CORROSION AROUND THEM. REPAIRED IAW FOKKER SRM 57-01-01, PAGE 5, PARAGRAPH B.

Part: FLANGE — CRACKED (LAVATORY) · airframe 30,576 hrs · 37,630 cycles

PDX- VERTICAL L-FLANGE BEHIND LEFT HAND LAV SINK AREA ATTACHED TO REAR PRESSURE BULKHEAD FRAME 17065 FORWARD SIDE LEFT HAND HAS 2 INCH CRACK. REPAIRED IAW FOKKER SRM 51-31-01.

Part: WEB — CORRODED (FUEL ACCESS) · airframe 30,576 hrs · 37,630 cycles

PDX - RIGHT WING FUEL ACCESS 74D HAS NUMEROUS SCREW HOLES WITH FRETTING CORROSION AROUND THEM. REPAIRED IAW FOKKER SRM 57-01-01, PAGE 65, PARAGRAPH B.

Part: SKIN — CORRODED (RT WING) · airframe 30,576 hrs · 37,630 cycles

PDX - RIGHT WING FUEL ACCESS APERTURE 74E HAS LIGHT FRETTING CORROSION AND A FEW LIGHT SCRATCHES AROUND NUMEROUS SCREW HOLES. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4B.

Part: SKIN — CORRODED (RT WING) · airframe 30,576 hrs · 37,630 cycles

PDX- RIGHT HAND WING FUEL ACCESS APERTURE 74H HAS LIGHT FRETTING AND A FEW LIGHT SCRATCHES AROUND NUMEROUS SCREW HOLES. REPAIRED IAW FOKKER SRM 57-01-01.

Part: WEB — CRACKED (NLG WW) · airframe 30,576 hrs · 37,630 cycles

PDX- TYPE 1 CRACK AT LEFT HAND PANEL AFT SIDE OF NOSE LANDING GEAR WHEEL BAY. REPAIRED IAW FOKKER SRM 53-02-18, FIGURE 10 ACCORDING TO HORIZON AIR EA 4-53-1056.

Part: SKIN — CORRODED (RT WING) · airframe 30,576 hrs · 37,630 cycles

PDX - RIGHT WING FUEL ACCESS APERTURE 74A HAS SIX AREAS OF LIGHT FRETTING CORROSION. REPAIRED IAW FOKKER SRM 57-01-01, PAGE 5, PARAGRAPH B.

Part: SKIN — CORRODED (RT WING) · airframe 30,576 hrs · 37,630 cycles

PDX- RIGHT HAND WING FUEL ACCESS APERTURE 74J HAS LIGHT FRETTING AND A FEW LIGHT SCRATCHES AROUND NUMEROUS SCREW HOLES. REPAIRED IAW FOKKER SRM 57-01-01.

Part: RIB — CRACKED (VERTICAL STAB) · airframe 30,576 hrs · 37,630 cycles

PDX - VERTICAL STAB RIB 3.2 HAS A CRACKED LEFT LOWER FLANGE AT AFT END, SEVERAL CRACKS EXTEND THROUGH AND CONNECT APPROXIMATELY FOUR RIVET HOLES. REPAIRED IAW HORIZON AIR EA 4-55-194.

Part: SKIN — DAMAGED (WING) · airframe 30,576 hrs · 37,630 cycles

PDX- EXISTING SKIN PATCH IN AREA WHERE NEW DOUBLER WILL BE INSTALLED AT THE BOTTOM OF NR 3 WINDOW POST. REPAIRED IAW HORIZON EA 4-53-1039.

Part: BULKHEAD — GOUGED (CABIN) · airframe 30,576 hrs · 37,630 cycles

PDX -REAR PRESSURE BULKHEAD HAS DEEP GOUGE LOCATED FORWARD SIDE, 3 INCHES INBOARD OF VERTICAL BEAM 425L, 3 INCHES UP FROM HORIZONTAL BEAM IX. REPAIRED IAW HORIZON AIR EA 4-53-1037A.

Part: DOOR — CHAFED (RT MLG) · airframe 30,576 hrs · 37,630 cycles

PDX- RIGHT HAND MAIN LANDING GEAR OUTBOARD DOOR IS CHAFING ON THE AFT LUG OF THE AFT BRACKET AT STRUT ATTACH POINT. REPAIRED IAW HORIZON AIR EA 4-57-374.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 30,576 hrs · 37,630 cycles

PDX- REAR PRESSURE BULKHEAD HAS AN .25 INCH CRACK ON LOWER FLANGE OF BEAM 3 RADIUS. REPAIRED IAW HORIZON AIR EA 4-53-929.

Part: STRAP — CHAFED (WING TO BODY) · airframe 30,576 hrs · 37,630 cycles

PDX- WING TO FUSELAGE JOINT STRAP IS CHAFED UNDER PANEL 91J. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4B STEP 2 AND PARAGRAPH 3C STEPS 1 THRU 4 AND HORIZON AIR EA 4-53-376.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 30,576 hrs · 37,630 cycles

PDX- GOUGE IN SEAT TRACK BL 1127L, BETWEEN FRAMES 13815A AND 13815B. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4B AND C.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,576 hrs · 37,630 cycles

PDX- LIGHT CORROSION ON TOP OF FLOOR SUPPORT BEAM BETWEEN FRAMES 3820 AND 4900 BL 0. REPAIRED IAW FOKKER SRM 51-31-01.

Part: STRAP — CHAFED (WING TO BODY) · airframe 30,576 hrs · 37,630 cycles

PDX- WING TO FUSELAGE JOINT STRAP IS CHAFED UNDER PANEL 92J. REPAIRED IAW FOKKER SRM 51-10-04, PARAGRAPH 4B (1), PAGE 9 AND PARAGRAPH 3C (1-4) PAGE 8.

Part: ANGLE — BENT (PAX DOOR) · airframe 30,576 hrs · 37,630 cycles

PDX- ANGLE BENT ON MAIN CABIN DOOR FORWARD SIDE MIDDLE NEAR MIDDLE HANDRAIL ATTACH POINT. REPAIRED IAW FOKKER SRM 51-11-01, FOKKER SRM 51-10-04, PARAGRAPH 4, PAGE 9. FOKKER SRM 51-10-04, PAGE 3C, AND FOKKER SRM 51-31-01.

Part: ANGLE — BENT (PAX DOOR) · airframe 30,576 hrs · 37,630 cycles

PDX- MAIN CABIN DOOR INSIDE STRUCTURE CENTER BULKHEAD ANGLE IS BENT IN MIDDLE. REFERENCE FOKKER SRM 52-10-00, FIGURE 01, ITEM 100. REPAIRED IAW FOKKER SRM 51-31-01.

Part: PANEL — CORRODED (WING) · airframe 30,576 hrs · 37,630 cycles

PDX- LIGHT FRETTING CORROSION GROUND SCREW HOLES ON FUEL PANEL APERTURE 71A. REPAIRED IAW FOKKER SRM 57-01-01, PAGE 5, PARAGRAPH B2(A).

Part: FRAME — CORRODED (FUSELAGE) · airframe 30,576 hrs · 37,630 cycles

PDX- CORROSION BELOW NUT PLATE AT FRAME 3820, BL44R. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 6.

Part: SEAT TRACK — GOUGED (BS 5805 & 6305) · airframe 30,576 hrs · 37,630 cycles

PDX - TWO 6 INCH LONG GOUGES IN CENTER OF SEAT TRACK, BL600L, FRAME 5805 AND 6305. REPAIRED IAW FOKKER MM 53-40-01, FIGURE 204.

Part: ANGLE — BENT (PAX DOOR) · airframe 30,576 hrs · 37,630 cycles

PDX- MAIN CABIN DOOR INSIDE STRUCTURE UPPER BULKHEAD ANGLE IS BENT AND KINKED IN MIDDLE. REF FOKKER SRM 52-10-00 FIGURE 01, ITEM 135. REPAIRED IAW FOKKER SRM 51-31-01.

Part: FRAME — CRACKED (FUSELAGE) · airframe 30,576 hrs · 37,630 cycles

PDX- FRAME 20075 CASTELLATION CRACKED AT STRINGER 39. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 6 FIGURE 4.

Part: FLANGE — CRACKED (A/C DUCT) · airframe 30,576 hrs · 37,630 cycles

PDX- CRACK AT EDGE OF RETAINING FLANGE. INSPECTED AND FOUND THE METAL FLANGE INSIDE THE EXTERNAL AIR CONDITIONING CONNECTION DUCT TO STILL BE CRACKED. REPAIRED IAW FOKKER SRM 51-31-01.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 30,576 hrs · 37,630 cycles

PDX- CENTER CARGO DOOR INSIDE SKIN HAS DAMAGE AT INBOARD CENTER EDGE TO RIVET. REPAIRED IAW FOKKER SRM 52-02-01, PAGE 3, FIGURE 2, FOKKER SRM 51-31-02, FOKKER SRM 51-10-04 AND FOKKER SRM 52-01-00, PAGE 3, PARAGRAPH 3F.

Part: WEB — CRACKED (NLG WW) · airframe 30,576 hrs · 37,630 cycles

PDX- UPPER WEB AT NOSE LANDING GEAR BAY JUST AFT OF FRAME 2260 IS CRACKED. REPAIRED IAW HORIZON AIR EA 4-53-1042.

Part: FRAME — CHAFED (FUSELAGE) · airframe 30,576 hrs · 37,630 cycles

PDX- FRAME 18075 HAS CHAFE IN INBOARD FORWARD RADIUS BETWEEN STRINGERS 19 AND 20. REPAIRED IAW HORIZON AIR EA 4-53-1044.

Part: PANEL — CORRODED (RT WING) · airframe 30,576 hrs · 37,630 cycles

PDX - RIGHT WING FUEL PANEL 74F HAS FRETTING CORROSION AROUND SCREW HOLES. REPAIRED IAW FOKKER SRM 51-10- AND MM 28-11-06, PAGE 404, 3A.

Part: WEB — CRACKED (NLG WW) · airframe 30,576 hrs · 37,630 cycles

PDX- LEFT HAND NOSE LANDING GEAR BAY INNER SKIN TO TOP ANGLE JUST AFT OF FRAME 2650 IS CRACKED. REPAIRED IAW HORIZON AIR EA 4-53-1041.

Part: WEB — CRACKED (NLG WW) · airframe 30,576 hrs · 37,630 cycles

PDX- RIGHT HAND NOSE LANDING GEAR BAY INNER SKIN TO TOP ANGLE JUST AFT OF FRAME 2650 IS CRACKED. REPAIRED IAW HORIZON AIR EA 4-53-1041.

Part: BEAM — CRACKED (FUSELAGE) · airframe 30,576 hrs · 37,630 cycles

PDX- HORIZON BEAM NR 1 STATION 2422 OF THE NOSE LANDING GEAR TOP COVER, THERE ARE 2 CRACKS COMING OUT FROM FASTENERS. REPAIRED IAW FOKKER SRM 53-02-18, PAGE 14, SECTION A-A AND HORIZON AIR EA 4-53-1032.

Part: FITTING — CORRODED (HORIZ STAB) · airframe 30,576 hrs · 37,630 cycles

PDX- HORIZONTAL STABILIZER DRIVE FITTING LOWER LEFT HAND LUG HAS PITTING CORROSION ALONG UPPER HALF. REPAIRED IAW HORIZON AIR EA 4-55-191.

Part: FITTING — CORRODED (HORIZ STAB) · airframe 30,576 hrs · 37,630 cycles

PDX- HORIZONTAL STABILIZER DRIVE FITTING LOWER RIGHT HAND LUG INBOARD FACE HAS PITTING CORROSION 2 PLACES. REPAIRED IAW HORIZON AIR EA 4-55-191.

Part: FRAME — CRACKED (FUSELAGE) · airframe 30,576 hrs · 37,630 cycles

PDX- FRAME 20075 CASTELLATION CRACKED AT STRINGER 36. REPAIRED IAW FOKKER SRM 53-10-05, PAGE 601A, PARAGRAPH 2B.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 30,576 hrs · 37,630 cycles

PDX- FOUR SMALL SCUFFED AREAS ON FORWARD SIDE OF REAR PRESSURE BULKHEAD. REPAIRED IAW FOKKER SRM 51-10-04.

Part: PANEL — CORRODED (RT WING) · airframe 30,576 hrs · 37,630 cycles

PDX - RIGHT WING FUEL PANEL 74D HAS FRETTING CORROSION AROUND SCREW HOLES. REPAIRED IAW FOKKER SRM 51-10-4, PARAGRAPH 3.

Part: FITTING — CORRODED (HORIZ STAB) · airframe 30,576 hrs · 37,630 cycles

PDX- HORIZONTAL STABILIZER JUNCTION FITTING UPPER LEFT HAND LUG INBOARD FACE HAS PITTING CORROSION 1 PLACE AFT. REPAIRED IAW HORIZON AIR EA 4-55-190, REFERENCE 4-302 FOR RE-ASSEMBLY.

Part: FITTING — CORRODED (HORIZ STAB) · airframe 30,576 hrs · 37,630 cycles

PDX- HORIZONTAL STABILIZER JUNCTION FITTING UPPER RIGHT HAND LUG INBOARD FACE HAS PITTING CORROSION. REPAIRED IAW HORIZON AIR EA 4-55-190.

Part: FITTING — CORRODED (HORIZ STAB) · airframe 30,576 hrs · 37,630 cycles

PDX- HORIZONTAL STABILIZER JUNCTION FITTING LOWER LEFT HAND LUG INBOARD FACE HAS CORROSION PITTING ONE PLACE UPPER. REPAIRED IAW HORIZON AIR EA 4-55-190, REFERENCE 49302 FOR RE-ASSEMBLY.

Part: PANEL — CORRODED (WING) · airframe 30,576 hrs · 37,630 cycles

PDX - WING FUEL PANEL 74A SCREW HOLES HAVE FRETTING CORROSION. REPAIRED IAW FOKKER SRM 51-10-4, PARAGRAPH 3.

Part: PANEL — CORRODED (RT WING) · airframe 30,576 hrs · 37,630 cycles

PDX - RIGHT WING FUEL PANEL 74E HAS LIGHT FRETTING CORROSION AROUND SCREW HOLES. REPAIRED IAW FOKKER SRM 51-10-4, PARAGRAPAH 3.

Part: FITTING — CORRODED (HORIZ STAB) · airframe 30,576 hrs · 37,630 cycles

PDX- HORIZONTAL STABILIZER JUNCTION FITTING LOWER RIGHT HAND LUG INBOARD HAS PITTING CORROSION. REPAIRED IAW HORIZON AIR EA 4-55-190.

Part: PANEL — CORRODED (RT WING) · airframe 30,576 hrs · 37,630 cycles

PDX - RIGHT WING FUEL PANEL 74G HAS LIGHT FRETTING CORROSION AROUND SCREW HOLES. REPAIRED IAW FOKKER SRM 51-10-4, PARAGRAPH 4A-B.

Part: PANEL — CORRODED (FUSELAGE) · airframe 30,576 hrs · 37,630 cycles

PDX- MINOR SURFACE CORROSION ON PANEL 74H. REPAIRED IAW FOKKER SRM 51-10-04, PARAGRAPH 4 A, B.

Part: PANEL — CORRODED (RT WING) · airframe 30,576 hrs · 37,630 cycles

PDX - RIGHT FUEL PANEL 74C HAS FRETTING CORROSION AROUND SCREW HOLES. REPAIRED IAW FOKKER SRM 51-10-4, PARAGRAPH 4A-B.

Part: PANEL — CORRODED (FUSELAGE) · airframe 30,576 hrs · 37,630 cycles

PDX- MINOR SURFACE CORROSION ON PANEL 74J. REPAIRED IAW FOKKER SRM 51-10-4, PARAGRAPH 4 A, B.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 30,576 hrs · 37,630 cycles

PDX- THERE IS A CRACK IN THE LEFT KEEL BEAM SECTION CONNECTION ANGLE AT STRINGER 2.01. REPAIRED IAW HORIZON AIR EA 4-53-1034.

Part: PANEL — CORRODED (RT WING) · airframe 30,576 hrs · 37,630 cycles

PDX - RIGHT WING FUEL PANEL 74B HAS FRETTING CORROSION AROUND SCREW HOLES. REPAIRED IAW FOKKER SRM 51-10-4, PARAGRAPH 4A-B.

Part: PANEL — CORRODED (RT WING) · airframe 30,576 hrs · 37,630 cycles

PDX - RIGHT WING FUEL PANEL 72A HAS FRETTING CORROSION AROUND SCREW HOLES. REPAIRED IAW FOKKER SRM 51-10-4, PARAGRAPH 4A.

Part: SKIN — CORRODED (RT WING) · airframe 30,576 hrs · 37,630 cycles

PDX - RIGHT WING FUEL ACCESS 74C APERTURE HAS EIGHT SCREW HOLES WITH MATERIAL MUSHROOMED UP. REPAIRED IAW FOKKER SRM 57-01-01, PAGE 3.

Part: SKIN — TORN (LT AILERON) · airframe 30,576 hrs · 37,630 cycles

PDX - BEHIND PANEL 83D LEFT AILERON COVER PANEL IS TORN AND DENTED. REPAIRED IAW HORIZON AIR EA 4-57-371.

Part: FRAME — CORRODED (CARGO BAY) · airframe 30,576 hrs · 37,630 cycles

PDX- AFT CARGO BAY AT STRINGER 74 HAS SURFACE CORROSION ON NUT PLATES. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4A1 AND FOKKER SRM 51-10-04, PAGES 3, C4 ,B4, B2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 30,576 hrs · 37,630 cycles

PDX- FRAME 50-2 CASTELLATION HAS CRACK BEYOND STOP DRILL AT STRINGER 50. REPAIRED IAW FOKKER 53-10-05, PAGE 601A, PARAGRAPH 2B.

Part: FRAME — CRACKED (FUSELAGE) · airframe 30,576 hrs · 37,630 cycles

PDX- FRAME 19832 CASTELLATION CRACKED AT STRINGER 34. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 5, FIGURE 3.

Part: FRAME — CRACKED (FUSELAGE) · airframe 30,576 hrs · 37,630 cycles

PDX- FRAME 50-2 CASTELLATION HAS CRACK BEYOND STOP DRILL AT STRINGER 25. REPAIRED IAW FOKKER SRM 53-10-05, PAGE 601A, PARAGRAPH 2B.

Part: FRAME — CRACKED (FUSELAGE) · airframe 30,576 hrs · 37,630 cycles

PDX-FRAME 24-2 CASTELLATION HAS CRACK AT LEFT HAND V-STAB CUTOUT. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 7, FIGURE 5.

Part: FRAME — CRACKED (FUSELAGE) · airframe 30,576 hrs · 37,630 cycles

PDX- FRAME 19832 CASTELLATION CRACKED AT STRINGER 41. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 5, FIGURE 3.

Part: FRAME — CRACKED (FUSELAGE) · airframe 30,576 hrs · 37,630 cycles

PDX- FRAME 32-2 CASTELLATION HAS CRACK BEYOND STOP DRILL AT STRINGER 26. REPAIRED IAW FOKKER SRM 53-10-05, PAGE 601A, PARAGRAPH 2B. REPAIRED IAW FOKKER SRM 53-10-05, PAGE 601A, PARAGRAPH 2B.

Part: FRAME — CRACKED (FUSELAGE) · airframe 30,576 hrs · 37,630 cycles

PDX- FRAME 50-2 CASTELLATION HAS CRACK BEYOND STOP DRILL AT STRINGER 24. REPAIRED IAW FOKKER SRM 51-31-04.

Part: FRAME — CRACKED (FUSELAGE) · airframe 30,576 hrs · 37,630 cycles

PDX- FRAME 17565 HAS ONE CRACK PAST STOP DRILL IN CASTELLATION AT STRINGER 51. REPAIRED IAW FOKKER SRM 53-10-05, PAGE 601A AND FOKKER SRM 51-31-01.

Part: FRAME — CRACKED (FUSELAGE) · airframe 30,576 hrs · 37,630 cycles

PDX- FRAME 24-2 CASTELLLATION HAS CRACK AT RIGHT HAND V-STAB CUTOUT. REPAIRED IAW FOKKER 53-10-05, PAGE 601A, PARAGRAPH 2B.

Part: FRAME — CRACKED (FUSELAGE) · airframe 30,576 hrs · 37,630 cycles

PDX- FRAME 32-2 CASTELLATION HAS CRACK BEYOND STOP DRILL AT STRINGER 25. REPAIRED IAW FOKKER SRM 53-10-05, PAGES 601A, PARAGRAPH 2B.

Part: FRAME — CRACKED (FUSELAGE) · airframe 30,576 hrs · 37,630 cycles

PDX- FRAME 50-2 CASTELLATION HAS CRACK BEYOND STOP DRILL AT STRINGER 22. REPAIRED IAW FOKKER SRM 53-10-05, PAGE 601A, PARAGRAPH 2B.

Part: FRAME — CRACKED (FUSELAGE) · airframe 30,576 hrs · 37,630 cycles

PDX- FRAME 32-2 CASTELLATION HAS CRACK BEYOND STOP DRILL AT STRINGER 46. REPAIRED IAW FOKKER SRM 53-10-05, PAGE 601A, PARAGRAPH 2B.

Part: FRAME — CRACKED (FUSELAGE) · airframe 30,576 hrs · 37,630 cycles

PDX- FRAME 32-2 CASTELLATION HAS CRACK BEYOND STOP DRILL AT RIGHT HAND V-STAB CUTOUT. REPAIRED IAW FOKKER SRM 53-10-05, PAGE 601A, PARAGRAPH 2B.

Part: FRAME — CRACKED (FUSELAGE) · airframe 30,576 hrs · 37,630 cycles

PDX- FRAME 32-2 CASTELLATION HAS CRACK AT LEFT HAND V-STAB CUTOUT. REPAIRED IAW FOKKER SRM 53-10-05, PAGE 601A, PARAGRAPH 2B.

Part: FRAME — CRACKED (FUSELAGE) · airframe 30,576 hrs · 37,630 cycles

PDX- FRAME 32-2 CASTELLATION HAS CRACK BEYOND STOP DRILL AT STRINGER 29. REPAIRED IAW FOKKER SRM 53-10-05, PAGE 601A, PARAGRAPH 2B.

Part: FRAME — CRACKED (FUSELAGE) · airframe 30,576 hrs · 37,630 cycles

PDX- FRAME 32-2 CASTELLATION HAS CRACK AT STRINGER 48. REPAIRED IAW FOKKER SRM 53-10-05, PAGE 601A, PARAGRAPH 2B.

Part: FRAME — CRACKED (FUSELAGE) · airframe 30,576 hrs · 37,630 cycles

PDX- FRAME 32-2 CASTELLATION HAS CRACK AT STRINGER 31. REPAIRED IAW FOKKER 53-10-05, PAGE 601A, PARAGRAPH 2B.

Part: FRAME — CORRODED (CARGO BAY) · airframe 30,576 hrs · 37,630 cycles

PDX- AFT CARGO BAY AT STATION 16660 - 16060 HAS SURFACE CORROSION AT NUT PLATE HOLES. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9.

Part: STRINGER — CORRODED (CARGO BAY) · airframe 30,576 hrs · 37,630 cycles

PDX- AFT CARGO BAY AT STATION 16660, STRINGER 74 HAS SURFACE CORROSION ON NP HOLES. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9.

Part: WARMER — MALFUNCTIONED (GALLEY)

PDX - BURNT ELECTRICAL ODOR COMING FROM LOWER BEVERAGE WARMER. SYSTEM DEACTIVATED. ODOR DISSAPATED. SYSTEM PLACED ON DEFFERED MAINTENANCE LIST. AIRCRAFT RETURNED TO SERVICE.

Part: BULB — FAILED (CABIN)

SEVERAL BULBS OUT IN EMERGENCY EXIT SIGN ABOVE FLIGHT COMPARTMENT ENTERANCE. REMOVED AND REPLACED EXIT SIGN ASSEMBLY, OPERATIONAL CHECK GOOD.

Part: CIRCUIT BOARD — FAILED (CABIN)

GEG - OVERHEAD EXIT ANNUNCIATOR ABOVE COAT CLOSET HAS INOPERATIVE LAMPS. REPLACED CIRCUIT BOARD. CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CABLE — OUT OF ADJ (PAX DOOR)

PDX- MAIN CABIN DOOR WILL NOT WORK IN EMERGENCY MODE. CLEANED AND LUBED DOOR BACK-UP PINS AND EMERGENCY RELEASE CABLE. RERIGGED EMERGENCY CLUTCH RELEASE CABLE IAW MM 52-10-05. DOOR OPERATES NORMAL.

Part: VALVE — FAILED (NR 1 BLEED AIR)

PDX - AUXILLARY POWER UNITS TURBINE GAS TEMPERATURE WAS 660 DEGREES WITH 1 PACK ON. ALSO, NOTICED EXHAUST SMELL COMING FROM COCKPIT AIR VENTS. PLACED APU ON MEL. THE MEL WAS CLEARED AFTER REMOVING AND REPLACING THE BLEED AIR LOAD CONTROL VALVE. OPERATIONAL CHECK WAS GOOD.

Part: SIGN — MISSING (ROW 9B)

GEG- EXIT SIGN MISSING AT ROW 9. INSTALLED NEW SIGN AT SEAT 9B, OPERATIONAL CHECK GOOD.

Part: SIGN — BROKEN (ROW 8B)

BOI - EMERGENCY EXIT LIGHT AT SEAT 8B BROKEN. MAINTENANCE REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY. OPERATIONAL CHECKS NORMAL.

Part: INNITOR — INOPERATIVE (APU)

BIL - DURING LANDING ROLL, BIL TOWER REPORTED FLAMES COMING FROM APU EXHAUST. FIRST OFFICER NOTICED APU TGT 650 DEGRESS AND INCREASING. SHUT DOWN APU. MX DEFERED THE APU. THE FOLLOWING DAY GEG MX GROUND RAN, FOUND AFTER APU WARMED UP IT HAD LOW OIL PRESSURE AND WOULD NOT START. CONTINUED MEL. ON 3/10/99 IN BOI, REPLACED APU. OPS CHECK GOOD. A/C RETURNED TO SERVICE. THE APU WAS BOROSCOPED AND THE COMBUSTION LINER AND FUEL NOZZLE WERE INSPECTED WITH NO FINDINGS. THIS UNIT WAS DETERMINED TO HAVE A BAD IGNITOR PLUG WHICH WAS REPLACED. IT WAS RUN NUMEROUS TIMES WITHOUT INCIDENT AND HAS BEEN RETURNED TO SERVICE.

Part: FIRE DETECTOR — OUT OF POSITION (APU)

SEA - ON DESCENT AT 10,000 FT STARTED APU, 10 TO 15 SECONDS AFTER INITIAL START TGT HUNG AT ABOUT 400 DEG, UPON TURNING APU MAIN SWITCH OFF APU FIRE LIGHT ILLUMINATED AND EXTINGUISHER LIGHT CAME ON. WENT THROUGH APU FIRE CHECKLIST AND LANDED WITHOUT INCIDENT. MX INSPECTED AND FOUND NO SIGN OF FIRE OR HEAT DAMAGE. THE APU ENG FIRE SENSING ELEMENT WAS FOUND BENT AND NEARLY TOUCHING THE COMBUSTION SECTION CASING. STRAIGHTENED SENSE ELEMENT TO ORIGINAL CONTOUR. TESTED IN ACCORDANCE WITH MANUAL, RAN APU CHECKED FOR LEAKS, ALL FUNCTIONS NORMAL. REPLACED APU FIRE EXTINGUISHER CONTAINER, VALVE AND CARTRIDGE. ALSO REPLACED DISCHARGE INDICATOR THE DISCHARGE LINE (TO THE INDICATOR).

Part: CIRCUIT BOARD — FAILED (CABIN)

EXIT SIGN ABOVE GALLEY HAS 6 28V LAMPS OUT. MAINTENANCE REMOVED AND REPLACED THE CIRCUIT BOARD ASSEMBLY, OPERATIONAL TEST NORMAL.

Part: BULB — FAILED (ROW 9E)

EMERGENCY EXIT SIGN AT ROW 9E HAS A LIGHT OUT. MAINTENANCE RELAMPED, OPERATIONAL TESTS NORMAL.

Part: BULB — FAILED (CABIN)

EMERGENCY EXIT LIGHT OUT ON RIGHT FORWARD WINDOW EXIT. MAINTENANCE RELAMPED, OPERATIONAL TEST IS SATISFACTORY.

Part: BULB — FAILED (CABIN)

PDX - OVERHEAD EMERGENCY LIGHT AT ROW 8 HAS SEVERAL BULBS OUT. REPLACED OVERHEAD EMERGENCY LIGHTS. OPERATIONAL CHECK GOOD.

Part: SIGN — INOPERATIVE (CABIN)

THE EMERGENCY EXIT SIGN ABOVE THE COCKPIT DOOR HAS LIGHTS OUT. MAINTENANCE REMOVED AND REPLACED THE EXIT SIGN, OPERATIONALLY TESTED NORMAL.

Part: BULB — FAILED (CABIN)

OVERWING EXIT LIGHT AT ROW 9A IS INOPERATIVE. MAINTENANCE RELAMPED AND OPERATIONALLY TESTED. TESTS ARE NORMAL.

Part: BULB — FAILED (CABIN)

CEILING EMERGENCY LIGHT INOPERATIVE AT ROW 8. MAINTENANCE RELAMPED, OPERATIONALY TESTS NORMAL.

Part: BULB — FAILED (CABIN)

EMERGENCY LIGHT AT ROW 9AB INOPERATIVE. MAINTENANCE RELAMPED AND TESTED, OPERATIONAL TEST NORMAL.

Part: BULB — FAILED (CABIN)

OVERHEAD EMERGENCY EXIT SIGN AT ROW 8, FACING AFT IS INOPERATIVE. MAINTENANCE RELAMPED, OPERATIONALLY TESTED NORMAL.

Part: BULB — FAILED (CABIN)

SEA - THE EMERGENCY EXIT LIGHT IN THE GALLEY WAS OUT. MAINTENANCE RELAMPED AND OPERATIONALLY TESTED, TESTS NORMAL.

Part: BULB — FAILED (CABIN)

BOI - 3.5 VOLT EMERGENCY EXIT LIGHT INOPERATIVE AT ROW 8A. MAINTENANCE RELAMPED AND OPERATIONALLY TESTED. TESTS NORMAL.

Part: BULB — FAILED (CABIN)

EMERGENCY EXIT LIGHT AT ROW 8 OUT. MAINTENANCE RELAMPED AND OPERATIONAL TESTED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN)

FORWARD LEFT WING EVACUATION LIGHT OUT. MAINTENANCE PLACED ON MEL. LATER THAT SAME DAY IN PDX MAINTENANCE REMOVED AND REPLACED BATTERY PACK, CLEANED CORROSION FROM LEFT FOWARD EVACUATION LIGHT RECEPTACLE, AND REMOVED AND REPLACED BLOWN FUSE IN NEW BATTERY PACK. MAINTENANCE PERFORMED OPERATIONAL TEST, TEST IS NORMAL.

Part: SKIN — GOUGED (RT TE FLAP VANE)

RIGHTHAND WING OUTBOARD FLAP VANE HAS A DEEP GOUGE 2 INCHES LONG, ON LOWER SURFACE AT APPROXIMATELY STATION 7306. REPAIRED IAW HORIZON AIR EA 4-57-120.

Part: LATCH — OUT OF POSITION (COCKPIT)

ESCAPE SLIDE DOES NOT LATCH PROPERLY TO FLOOR. REPOSITIONED LATCH RECEPTICLE, OPS CHECKS GOOD.

Part: FRAME — CRACKED (FRAME 67-2)

FRAME 67-2 CRACKED AT RIGHTHAND SIDE OF VERTICAL FIN BASE RIB WHERE ATTACHES TO COMPOSITE TAIL CONE. STOP DRILLED BUT DAMAGE EXCEEDS 1.02 MAXIMUM CRACK LIMIT. REPAIRED IAW HORIZON AIR EA 4-53-430.

Part: CASTELLATION — CRACKED (FRAME 20075)

FRAME CASTELLATION CRACKED ON FRAME 20075 BETWEEN STRINGERS 39 AND 40 ADJACENT TO PREVIOUSLY STOP DRILLED CRACK. REPAIRED IAW HORIZON AIR EA 4-53-447 STEP 7 AND FOKKER SRM 51-31-01 AND 51-31-05.

Part: RIVET — CRACKED (FRAME 1890)

CRACK THROUGH RIVET APPROXIMATELY .5 INCH LONG AT FRAME 1890 WL+ 16.141 APPROXIMATELY. REPAIRED IAW FOKKER SRM 53-02-02, FIGURE 1.

Part: CASTELLATION — CRACKED (FRAME 20075)

FRAME CASTELLATION CRACKED PAST STOP DRILL ON FRAME 20075 BETWEEN STRINGER 35 AND 36. REPAIRED IAW HORIZON AIR EA 4-53-447, STEP 2.

Part: BATTERY — DISCHARGED (CABIN)

UNDER SEAT BATTERY PACKS FOR EMERGENCY LIGHT MISSING. REPLACED PACKS AND OPS CHECKED GOOD.

Part: SKIN — DAMAGED (LT AILERON)

LEFTHAND AILERON LOWER SKIN DAMAGED AT INBOARD HINGE ARM OPENING. REPAIRED IAW HORIZON AIR EA 4-27-45.

Part: SKIN — DENTED (RT SPEED BRAKE)

THE RIGHTHAND SPEED BRAKE HAS A DENT ON THE BOTTOM 18 BACK FROM THE LEADING EDGE, DENT MEASURES 3 X 1.5 X .125. REPAIRED IAW HORIZON AIR EA 4-53-31A.

Part: STRAP — MISALIGNED (BS 3310)

LEFTHAND STATION 3310 BUTTSTRAP FOURTH HOLE ABOVE TURBULATOR STRIP INBOARD SIDE IS MISALIGNED BY APPROXIMATELY HALF OF SCREW HOLE. REPAIRED IAW FOKKER SRM 57-20-01, PAGE 402 TO 410, PARAGRAPH 3C-3E AND HORIZON AIR EA 4-57-117.

Part: STRUT — REQD SERVICE (NLG)

CHECK VALVE FOR NOSE LANDING GEAR STRUT SERVICING IS LEAKING. INSTALLED CHECK VALVE IAW HORIZON AIR EA 4-32-47.

Part: BOLT — DAMAGED (GUSTLOCK)

GUSTLOCK HOUSING LEVER FORWARD MOUNT BOLT HAS HEAD SHAVED OFF AT LEAST 25 PERCENT. REPAIRED IAW HORIZON AIR EA 4-55-67.

Part: CLIP — CRACKED (FRAME 16-2)

CLIP AT OBLIQUE FRAME 16-2 AFT SIDE BETWEEN STRINGER 40 AND 41 IS CRACKED IN RADIUS. REPAIRED IAW FOKKER SRM 53-11-05, PAGE 63, FIGURE 602 AND 53-10-05, PAGE 601.

Part: ANGLE — CRACKED (VERT STAB)

RIGHT VERTICAL STAB CONNECTION ANGLE AT FRONT SPAR (16 PERCENT) IS CRACKED. REPAIRED IAW FOKKER SRM 55-31-00, PAGE 2, FIGURE 1.

Part: FLOOR — CORRODED (COCKPIT)

CORROSION ON COCKPIT FLOOR UNDER CO-PILOTS INBOARD AND OUTBOARD SEAT RAILS. REPAIRED IAW FOKKER SRM 51-10-04, PARAGRAPH 4, PAGE 9.

Part: FRAME — CRACKED (FRAME 22293)

FRAME 22293 CRACKED AT AFT END OF STRINGER 53A. REPAIRED IAW HORIZON AIR EA 4-53-415 AND INSTALLED IAW FOKKER SRM 51-31-01.

Part: LUG — CORRODED (LT MLG)

AFT GEAR LUG ON WING FOR LEFTHAND MLG STRUT IS CHAFED AND CORRODED. REPAIRED IAW HORIZON AIR EA 4-57-113.

Part: BRACKET — CRACKED (WING)

CRACK FROM UPPER BOLT HOLE ON BRACKET INSIDE PANEL 81X. REPAIRED IAW FOKKER SRM 51-31-01 AND 51-31-05.

Part: SKIN — DENTED (RT SPEED BRAKE)

THE RIGHTHAND SPEED BRAKE HAS A DENT ON THE BOTTOM 15 BACK FROM THE LEADING EDGE, DENT MEASURES 3 X 1.5 X .125. REPAIRED IAW FOKKER SRM 53-01-01 PAGE 8, PARAGRAPH 5.

Part: DOUBLER — CORRODED (CARGO DOOR)

DOUBLER FOR INNER SKIN ON AFT CARGO DOOR IS CORRODED. REPAIRED IAW FOKKER SRM 52-30-00, FIGURE 4, ITEM 290.

Part: WEB — DAMAGED (FRAME16060/16660)

CEILING WEB ATTACHMENT TO FRAMES 16060 AND 16660 IS BENT ABOVE CARGO DOOR OPENING. REPAIRED IAW HORIZON AIR EA 4-53-425.

Part: SKIN — CORRODED (CARGO DOOR)

NUMEROUS SPOTS OF CORROSION ON INSIDE OF INNER DOOR SKIN OF AFT CARGO DOOR. REPAIRED IAW FOKKER SRM 52-30-00, FIGURE 4.

Part: CASTELLATION — CRACKED (FRAME 17565)

CRACKED FRAME CASTELLATION AT FRAME 17565 ABOVE STRINGER 21A. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 5, FIGURE 3.

Part: SUPPORT — CORRODED (BS 3820)

FLOOR SUPPORT UNDER GALLEY IS CORRODED AND BENT AT STATION 3820 AFT END. REPAIRED IAW FOKKER SRM 53-02-14, FIGURE 1.

Part: RIB — CRACKED (RUDDER)

THERE IS A BROKEN/CRACKED OUT RIB (NR 5) AT THE LEADING EDGE OF THE RUDDER. REPAIRED IAW FOKKER SRM.

Part: SUPPORT — DENTED (BS 4150)

FLOOR SUPPORT BEAM IS DENTED JUST FORWARD OF FY.4150 AT BL600RT. REPAIRED IAW FOKKER SRM 53-02-14, FIGURE 1.

Part: BRACKET — CRACKED (WING)

BRACKET CRACKED AT 11:00 POSITION FROM UPPER LARGE BOLT HOLE INSIDE PANEL 82X. REPAIRED IAW FOKKER SRM 51-31-05.

Part: ANGLE — CRACKED (VERT STAB)

AFT VERTICAL STAB CONNECTION ANGLE AT FRONT SPAR IS CRACKED AND MISSING RIVET HEAD. REPAIRED IAW FOKKER SRM 55-31-00, PAGE 2, FIGURE 1.

Part: SUPPORT — BENT (GALLEY)

FLOOR SUPPORT UNDER NR 1 GALLEY IS BENT AND CORRODED AT AFT END. REPAIRED IAW FOKKER SRM 53-02-14, FIGURE 1.

Part: SKIN — DENTED (PAX DOORWAY)

THERE IS A 1 X .100 DENT 4.5 FORWARD OF THE RIGHTHAND CORNER OF THE 41A DOOR OPENING. REPAIRED IAW FOKKER SRM 53-02-02, FIGURE 1.

Part: STRUT — DAMAGED (NR 2)

NR 2 THRUST STRUT IS DAMAGED APPROXIMATELY 10 AFT OF NACELLE TO STUB WING FEED THROUGH. REPAIRED IAW FOKKER MM 54-40-03, PAGE 201 TO 203, AND HORIZON AIR EA 4-71-81.

Part: STRUT — DAMAGED (NR 1)

NR 1 THRUST STRUT IS DAMAGED IN TWO LOCATIONS APPROXIMATLEY 7 AFT IN FORWARD END AND 10 FORWARD ON AFT END. REPAIRED IAW FOKKER SRM 54-40-03, PAGE 201 TO 203 AND HORIZON AIR EA 4-71-81.

Part: ANGLE — CRACKED (VERT FIN)

LEFTHAND FUSE TO VERTICAL FIN CONNECTION ANGLE IS CRACKED AT THE 50 PERCENT SPAR LOCATION. REPAIRED IAW FOKKER SRM 55-31-01, PAGE 2 AND SRM 51-31-01.

Part: ANGLE — CRACKED (VERT STAB)

LEFT VERTICAL STAB CONNECTION ANGLE AT REAR SPAR IS CRACKED. REPAIRED IAW FOKKER SRM 55-31-00, PAGE 2, FIGURE 1.

Part: BUSHING — OUT OF POSITION (ELEVATOR)

BUSHING HITS HOUSING WHERE ACTUATING LEVER IS ATTACHED. REPAIRED IAW HORIZON AIR EA 4-27-37.

Part: SKIN — DENTED (CARGO DOOR)

SHARP DENT IN OUTER SKIN APPROXIMATELY 9 BELOW HANDLE ACCESS DOOR OF AFT CARGO DOOR. REPAIRED IAW FOKKER SRM 52-01-01, FIGURE 7, PARAGRAPH 5 AND 2.

Part: STRUCTURE — CRACKED (ACM BAY)

RIGHTHAND ACM BAY STRESS CRACK ABOUT 3.5 LONG ABOVE RIVET LINE. REPAIRED IAW FOKKER SRM 53-11-60, PAGE 3 FIGURE 2.

Part: ANGLE — CRACKED (VERT STAB)

LEFT VERTICAL STAB CONNECTION ANGLE AT INTERMEDIATE SPAR 1 (32 PERCENT) IS CRACKED. REPAIRED IAW FOKKER SRM 55-31-00, PAGE 2, FIGURE 1.

Part: SKIN — LOOSE (RT SPEED BRAKE)

THE RIGHTHAND SPEED BRAKE INNER SKIN IS COMING LOOSE AT THE T/E OF THE SPEED BRAKE. REPAIRED IAW HORIZON AIR EA 4-53-421.

Part: SKIN — CHAFED (RT SPEED BRAKE)

THERE ARE 2 DEEP CHAFE MARKS AT RIGHTHAND SPEEDBRAKE INNER SKIN APPROXIMATELY 28 DOWN FROM TOP AFT CORNER. REPAIRED IAW HORIZON AIR EA 4-53-421.

Part: SKIN — DAMAGED (FUSELAGE)

HOLE IN FUSELAGE SKIN AFT OF OBLIQUE FRAME 50-2 BETWEEN STRINGER 66 AND 70. REPAIRED IAW FOKKER SRM 53-02-02, PAGE 2, FIGURE 1.

Part: SKIN — CHAFED (RT SPEED BRAKE)

THERE IS A DEEP CHAFE MARK AT TOP AFT CORNER OF THE RIGHTHAND SPEEDBRAKE INNER SKIN. REPAIRED IAW HORIZON AIR EA 4-53-421.

Part: CLIP — CRACKED (FRAME 4610)

CLIP CRACKED FRAME 4610 STRINGER 7. REPAIRED IAW FOKKER SRM 51-31-01, 53-02-13, PAGE 4, 51-10-05 AND 51-10-04.

Part: SEAT TRACK — DAMAGED (RT COCKPIT)

CO-PILOTS OUTBOARD SEAT TRACK OUTBOARD SIDE RAIL HAS AREAS OF SMALL NICKS. REPLACED SEAT RAIL.

Part: SKIN — CRACKED (RT MLG DOOR)

RIGHTHAND INBOARD GEAR DOOR IS CRACKED THROUGH THREE RIVETS ALONG THE FORWARD RIVET LINE OUTER SKIN SURFACE. REPAIRED IAW HORIZON AIR EA 4-53-23B.

Part: SUPPORT — CORRODED (BS 4900-3820)

CORROSION ON UPPER SURFACE OF FLOOR SUPPORT BEAM FROM 4900 TO 3820 AT BL6004T. REPAIRED IAW FOKKER SRM 51-31-01, PAGE 13.

Part: SUPPORT — CORRODED (FRAME 3820-4900)

CORROSION ON FLOOR SUPPORT BEAM UPPER SURFACE FROM FRAME 4900 TO 3820 CENTERLINE BEAM. REPAIRED IAW FOKKER SRM 51-10-05 AND 51-21-01.

Part: SEAT TRACK — CORRODED (FRAME 3820)

CORROSION ON FLOOR SUPPORT BEAM FROM FORWARD OF INBOARD RIGHT SEAT TRACK TO FRAME 3820 ON UPPER SURFACE. REPAIRED IAW FOKKER SRM 51-31-01, PAGE 13.

Part: SEAT TRACK — WORN (LT COCKPIT)

INBOARD PILOT SEAT TRACK IS WORN TO LIMITS. REPLACED SEAT TRACK IAW FOKKER SRM 53-40-01, PAGE 201.

Part: SEAT TRACK — WORN (LT COCKPIT)

OUTBOARD PILOT SEAT TRACK WORN TO LIMITS. REPLACED OUTBOARD SEAT TRACK IAW FOKKER SRM 53-40-01, PAGE 201B, CODE 2.

Part: CONNECTOR — CORRODED (CABIN)

ALL EMERGENCY LIGHTS ON THE PASSENGER SEAT SIDES ARE INOP. FOUND CORRODED WIRE SPLICES AT SEAT ROWS 1, 9 AND 14. REPAIRED WIRING AND CONNECTIONS, OPERATIONAL CHECKS GOOD.

Part: BULB — FAILED (CABIN)

EMERGENCY EXIT SIGN AT ROW 9E IS OUT. RELAMPED SIGN, OPERATIONAL CHECKS GOOD.

Part: LIGHT — INOP (CABIN)

SEA - NR 1 AFT EVACUATION LIGHT FULL OF WATER. MAINTENANCE DRAINED AND CLEANED LIGHT. FOUND TWO OF THE FOUR LENS COVER NUT PLATES BROKEN. PERFORMED INTERIM REPAIR. NO PARTS REPLACED. OPERATIONAL TEST GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LAMP — FAILED (CABIN)

LEFT HAND EVACUATION EXIT LIGHT INOP. REPLACED LAMP, OPERATIONAL CHECK GOOD.

Part: POWER SUPPLY — MALFUNCTION (CABIN)

PDX - AFT EVACUATION LIGHT ON BOTTOM PANEL INOP. REPLACED EVACUATION LIGHT POWER SUPPLY. OPERATION CHECK GOOD.

Part: BULB — FAILED (CABIN)

GEG - OVERHEAD EXIT SIGN AT ROW 8 INOP. RELAMPED, OPERATIONAL CHECK GOOD.

Part: BULB — FAILED (COCKPIT)

PDX- COCKPIT ENTRANCE EMERGENCY LIGHT PANEL IS INOP. RELAMPED, OPERATIONAL CHECKS GOOD.

Part: LAMPS — FAILED (CABIN)

GEG - SEVERAL 28V EXIT BULBS INOP ON CENTER AISLE AFT FACING EXIT SIGN. RELAMPED EXIT SIGN, OPERATIONAL CHECK GOOD.

Part: BATTERY — DISCHARGED (CABIN)

SEA - BOTH AFT EXTERIOR EMERGENCY LIGHTS INOP. REPLACED EMERGENCY LIGHT POWER SUPPLY, OPERATIONAL CHECK GOOD.

Part: BULB — FAILED (CABIN)

SEA- EMERGENCY LIGHTS IN ROW 9D ARE INOP. REPLACED EMERGENCY LIGHT AT ROW 9D, OPERATIONAL CHECKS GOOD.

Part: CONNECTOR — FAILED (GALLEY)

STRONG ELECTRICAL SMELL COMING FROM THE COFFEE HEATER IN THE GALLEY. UPPER CANNON PLUG SHOWS SIGNS OF ARCING. DISCONNECTED CANNON PLUG AT UPPER COFFEE WARMER AND TURNED OFF. PLACED ON MEL. MEL CLEARED BY REPLACING THE AIRCRAFT COFFEE JUG FEMALE CONNECTOR, OPERATIONAL CHECKS GOOD.

Part: BULB — FAILED (CABIN)

GEG- EXIT LIGHT OVER COCKPIT DOOR HAS LAMPS THAT ARE INOP. RELAMPED EXIT SIGN, OPERATIONAL CHECKS GOOD.

Part: BULB — FAILED (CABIN)

GEG - SEVERAL OVERHEAD AISLE 28V EVACUATION LIGHTS INOP. RELAMPED, OPERATIONAL CHECK GOOD.

Part: BULB — FAILED (CABIN)

BOI- EXIT SIGN BETWEEN OVERWING EMERGENCY EXITS HAS 4 BULBS THAT ARE NOT WORKING IN THE EMERGENCY POSITION. RELAMPED SIGN, OPERATIONAL CHECKS GOOD.

Part: LAMP — FAILED (CABIN)

PDX - EXIT ROW LIGHT ASSEMBLY INOP AT ROW 9AB. RELAMPED EXIT LIGHT. OPERATIONAL CHECK GOOD.

Part: SWITCHES — OUT OF ADJUST (CARGO DOOR)

SEA - CARGO DOOR WARNING ILLUMINATED. RETURNED TO FIELD. ADJUSTED SWITCHES. OPERATIONAL CHECK GOOD.

Part: BULBS — FAILED (CABIN)

OVERHEAD EXIT LIGHT, AFT ROW 8, 9 HAS LAMPS INOP. RELAMPED AS REQUIRED, OPERATIONAL CHECK GOOD.

Part: BULB — FAILED (CABIN)

FORWARD AND AFT CEILING EXIT SIGNS HAVE BURNED OUT BULBS. REPLACED LAMPS, OPERATIONAL CHECKS GOOD.

Part: BULB — FAILED (CABIN)

GEG - EMERGENCY EXIT SIGNS AT ROW 8 HAVE 28V LIGHTS INOPERABLE. BULBS WERE REPLACED AND SIGNS OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CIRCUIT BOARD — INOPERATIVE (CABIN)

OVERHEAD EMERGENCY LIGHT BETWEEN CABIN AND FORWARD GALLEY IS INOP. CIRCUIT BOARD REPLACED AND LIGHT OPS CHECKED GOOD.

Part: CIRCUIT BOARDS — FAILED (CABIN)

VARIOUS LIGHT IN THE EXIT SIGNS FOR THE OVERWING EXITS AND EXIT SIGN ABOVE THE COCKPIT DOOR ARE INOP. EMERGENCY EXIT SIGN CIRCUIT BOARDS WERE REPLACED AND SIGNS OPS CHECKED GOOD.

Part: BULB — FAILED (CABIN)

NUMBER FIVE AND SIX EMERGENCY LIGHTS IN CABIN OVERHEAD ARE INOP. BULBS WERE REPLACED AND LIGHTS OPS CHECKED GOOD.

Part: ENGINE OIL — OVER SERVICED (NR 2 ENGINE)

SMOKE SMELL IN AFT AREA OF CABIN REPORTED BY A PASSENGER AND LEFT LAV SMOKE DETECTOR ALARM SOUNDED ON TAXI OUT. AIRCRAFT RETURNED TO GATE. NUMBER TWO ENGINE FOUND OVER SERVICED BY TWO QUARTS ON THE ENGINE OIL. ENGINE OIL SERVICED TO NORMAL LEVEL. ENGINE GROUND RUN PERFORMED AND BLEED AIR CHECK GOOD.

Part: BULB — FAILED (CABIN)

EMERGENCY LIGHT AT SEAT 9A IS INOP. BULBS WERE REPLACED AND LIGHT OPS CHECKED GOOD.

Part: BULB — FAILED (CABIN)

EXIT SIGN ABOVE CABIN ENTRY WAY HAS THREE 28V BULBS INOP. BULBS WERE REPLACED AND LIGHT OPS CHECKED GOOD.

Part: DOOR PIN — BROKEN (LAV SERVICE DOOR)

SEA - IN-FLIGHT, EXPERIENCED A LOUD PRESSURE BANG FOLLOWED BY ERRATIC PRESSURIZATION. LAV SERVICE PLUG MISSING AND SERVICE PORT DOOR MISSING. DOOR PANEL 29AA REPLACED, SERVICE PLUG REPLACED, AND LATCH PIN REPLACED. LAV RESERVICED AND AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN)

PDX - EMERGENCY LIGHT AT SEAT 4AB IS INOPERATIVE. BATTERY PACK REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

GEG - SEVERAL EVACUATION LIGHTS IN GALLEY AREA ARE INOPERATIVE. POWER SUPPLY REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BULB — FAILED (CABIN)

EXIT SIGN OVER COCKPIT DOOR IS DIM 28V. BULBS WERE REPLACED AND SIGN OPS CHECKED GOOD.

Part: BLKHD FISHPLATE — CRACKED (FWD PRESS BLKHD)

PIT - DURING SIP VISIT INSPECTION, ACCOMPLISHED SIP 53-10-06 AND FOUND 4 INCH AND 3.5 INCH CRACK IN FRONT PRESSURE BULKHEAD FISHPLATE BETWEEN STRINGER 72 AND 73. STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR PER SRM 53-02-18 PG 28. (M)

Part: STRIKER — OUT OF ADJUST (CARGO DOOR)

PHF - FLT NR 1297 - AFTER TAKEOFF FROM PHF, CREW RECEIVED A CARGO DOOR LIGHT. CAPTAIN ELECTED TO RETURN TO PHF. MAINTENANCE ADJUSTED THE AFT CARGO DOOR WARNING SWITCH STRIKER. OPERATIONS CHECKED GOOD. (M)

Part: EEL POWER SUPPLY — FAILED (CABIN)

CLT - THE EMERGENCY EXIT LIGHTS REMAIN ON WITH ALL POWER REMOVED FROM THE AIRCRAFT AND THE EMERGENCY EXIT LIGHT SWITCH 'OFF'. MAINTENANCE RPELACED BATTERY POWER SUPPLY. OPERATIONS CHECK GOOD. (X)

Part: BRACKET — CHAFING (RT MLG)

BGM - FLT 0746 - THE RED LANDING GEAR DOOR LIGHT REMAINED ON AFTER TAKEOFF FROM BFM. THE GEAR WAS RECYCLED BUT THE LIGHT REMAINED ILLUMINATED. FLIGHT CONTINUED TO PIT WITH GEAR DOWN. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE INSTALLED THREE RIVETS, ADJUSTED STOPS AND REPLACED THE RIGHT MAIN LANDING GEAR DOOR SADDLE BRACKET. THE DOOR WAS RIGGED AND GEAR SWING PERFORMED. ALL INDICATIONS WERE NORMAL. (W)