N961AS

Part: TURBINE — FAILED (RIGHT) · airframe 51,851 hrs · 26,981 cycles

EN ROUTE SEA TO DEN RIGHTHAND ENGINE STARTED TO EXPERIENCE WHAT APPEARED TO BE COMPRESSOR STALLS. ENGINE WAS PURPOSELY SHUTDOWN AND THE FLIGHT WAS DIVERTED TO SLC. INSPECTION REVEALED TURBINE FAILURE. ENGINE WAS REPLACED. CAUSE OF FAILURE TO BE DETERMINED AT TEARDOWN.

Part: SKIN — DENTED (CARGO DOOR) · airframe 51,776 hrs · 26,945 cycles

RAMP REPORTS DENT IN AFT CARGO DOOR EXTERIOR SKIN JUST BELOW THE HANDLE CUTOUT. DAMAGED AREA OF SKIN FABRICATED REPAIR DOUBLERS AND INSTALLED IAW ASA EA 5230 01392.

Part: FRAME — CRACKED (BS 1418) · airframe 51,776 hrs · 26,945 cycles

AFT A C BAY FRAME 1418 CRACKED AT LONGERON 2 RIGHT REPAIRED AFT A C BAY FRAME 1418 IAW MD80 SRM 53 03 FIG 31A. STOP DRILLED CRACK, INSTALLED REPAIR ANGLES. LOCATED AND DRILLED 2 EACH 37 AND 1 EA 35. REPAIR ANGLES AND STRAP INSTALLED PER FIG 31A.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 51,776 hrs · 26,945 cycles

LONGERON 2 LEFT CRACKED AT STA 1418. REMOVED CRACKED SECTION OF LONGERON, FABRICATED AND INSTALLED REPLACEMENT SECTION ON LONGERON AND SPLICE IAW MD80 SRM 53-02 FIGURE 18.

Part: SKIN — DELAMINATED (AILERON) · airframe 51,776 hrs · 26,945 cycles

RT AILERON IS DELAMINATED AT THE O/B ATTACH POINT LOWER SURFACE PREPPED AREA. FABRICATED AND BONDED REPAIR PLIES IAW MD80 SRM 51 90 0 8N PG 72.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,776 hrs · 26,945 cycles

FUSELAGE FRAME STA 1418 FROM LONGERON 5L TO 5R FAILSAFE CHORD IS CRACKED. REMOVED CRACKED CHORD RECEIVED DRILLED AND INSTALLED NEW CHORD IAW MD80 SRM 51-10-4, 51-30-5.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 51,776 hrs · 26,945 cycles

LONGERON 2 RIGHT CRACKED AT STA 1418. REMOVED CRACKED SECTION OF LONGERON, FABRICATED AND INSTALLED REPLACEMENT SECTION OF LONGERON AND SPLICE IAW MD80 SRM 53-02 FIGURE 18.

Part: SKIN — DAMAGED (AIRSTAIR DOOR) · airframe 51,776 hrs · 26,945 cycles

A 9 INCH J-SHAPED CREASE ON EXTERIOR OF AFT STAIRWAY DOOR LEFT SIDE OF AIRPLANE JUST FORWARD OF EXTERNAL TAIL CONE ACCESS DOOR. CUT OUT DAMAGED SECTION OF SKIN, FABRICATED LOCATED AND INSTALLED A REPLACEMENT SKIN AND DOUBLER IAW MD80 SRM 52-05 FIG 56.

Part: CUSP WEB — CORRODED (BS 501-582) · airframe 47,849 hrs · 25,068 cycles

CUSP WEB CORRODED. REPLACED CUSP WEB PER SRM 51-10-4, 51-30-1, 51-30-2 AND 51-30-5.

Part: FLOOR PANEL — PUNCTURED (BS 886-927) · airframe 47,849 hrs · 25,068 cycles

CABIN FLOOR PANEL PUNCTURED. REPLACED FLOOR PANEL PER SRM 53-05 AND ASA DWG S4932106.

Part: SKIN — CRACKED (WING FLAP) · airframe 47,849 hrs · 25,068 cycles

RIGHT WING OUTBOARD FLAP TRAILING EDGE IS CRACKED. REMOVED DAMAGED AREA. APPLIED FOUR REPAIR PLIES PER SRM 51-70-1.

Part: SHEAR TIE — CORRODED (BS 1250 S29-30R) · airframe 47,849 hrs · 25,068 cycles

SHEAR TIE CORRODED. REMOVED DAMAGED SECTION OF TIE. INSTALLED REPAIR SECTION AND SPLICE PER SRM 53-03.

Part: STRINGER CLIP — CORRODED (BS 1261 S29R) · airframe 47,849 hrs · 35,068 cycles

TEE CLIP CORRODED. REPLACED TEE CLIP PER SRM 51-10-4 AND 51-30-5.

Part: FLOOR PANEL — CRACKED (BS 826-867) · airframe 47,849 hrs · 25,068 cycles

CABIN FLOOR PANEL IS CRACKED. REPLACED FLOOR PANEL PER SRM 53-05 AND ASA DWG S4932106.

Part: FLOOR PANEL — DELAMINATED (BS 886-946) · airframe 47,849 hrs · 25,068 cycles

CABIN FLOOR PANEL DELAMINATED. REPLACED PANEL PER SRM 53-05 AND ASA DWG S4932106.

Part: CUSP WEB — CORRODED (BS 1007-1010) · airframe 47,849 hrs · 25,068 cycles

CUSP WEB CORRODED. REMOVED DAMAGED CUSP SECTION. INSTALLED REPAIR DOUBLER AND FILLER PER SRM 51-70-4.

Part: VANE — CHAFED (TE FLAPS) · airframe 47,849 hrs · 25,068 cycles

RIGHT WING INBOARD FLAP INBOARD VANE IS CHAFED ON LEADING EDGE. INSTALLED EXTERNAL REPAIR DOUBLER PER SRM 57-03.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 47,849 hrs · 25,068 cycles

CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL IAW SRM 53 05 AND ASA DWG S4932106.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 47,849 hrs · 25,068 cycles

CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL IAW SRM 53 05 AND ASA DWG S4932106.

Part: SKIN — DENTED (FUSELAGE) · airframe 47,849 hrs · 25,068 cycles

FUSELAGE SKIN DENTED. REMOVED DAMAGED SECTION INCLUDING EXISTING REPAIR DOUBLER. INSTALLED EXTERNAL REPAIR DOUBLER FINGER DOUBLER LONGERON STRAP AND FILLER IAW SRM 53 04.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 47,849 hrs · 25,068 cycles

CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL IAW SRM 53 05 AND ASA DWG S4932106.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 47,849 hrs · 25,068 cycles

CUSP WEB CORRODED. REMOVED DAMAGED SECTION OF WEB. INSTALLED REPAIR DOUBLER IAW SRM 53 01.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 47,849 hrs · 25,068 cycles

CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL IAW SRM 52 05 AND ASA DWG S4932106.

Part: FLOOR PANEL — CORRODED (BS 160-200) · airframe 47,849 hrs · 25,068 cycles

CABIN FLOOR PANEL HAS CORRODED INSERTS. REPLACED FLOOR PANEL PER SRM 53-05 AND ASA DWG S4932106.

Part: FLOOR PANEL — CRACKED (BS 200-256) · airframe 47,849 hrs · 25,068 cycles

CABIN FLOOR PANEL CRACKED. REPLACED FLOOR PANEL PER SRM 53-05 AND ASA DWG S4932106.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 47,849 hrs · 25,068 cycles

CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL IAW SRM 53 05 AND ASA DWG S4932106.

Part: FLOOR PANEL — DELAMINATED (BS 196-256) · airframe 47,849 hrs · 25,068 cycles

CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-05 AND ASA DWG S4932106.

Part: FLOOR PANEL — CRACKED (BS 160-200) · airframe 47,849 hrs · 25,068 cycles

CABIN FLOOR PANEL CRACKED AT INSERTS. REPLACED FLOOR PANEL PER SRM 53-05 AND ASA DWG S4932106.

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 47,849 hrs · 25,068 cycles

CABIN FLOOR PANEL CORRODED AT INSERTS. REPLACED FLOOR PANEL IAW SRM 53 05 AND ASA DWG S4932106.

Part: WEB — CRACKED (BS 205-209) · airframe 47,849 hrs · 25,068 cycles

L1 DOOR JAMB WEB IS CRACKED. REMOVED DAMAGED AREA OF WEB. INSTALLED REPAIR FILLER AND DOUBLER PER SRM 51-70-4.

Part: FLOOR PANEL — CORRODED (BS 180-200) · airframe 47,849 hrs · 25,068 cycles

CABIN FLOOR PANEL CORRODED AT INSERTS. REPLACED FLOOR PANEL PER SRM 53-05 AND ASA DWG S4932106.

Part: SKIN — DENTED (CARGO BAY DOOR) · airframe 47,849 hrs · 25,068 cycles

MID CARGO BAY DOOR DENTED. COLD FORMED TO ORIGINAL CONTOUR. INSTALLED INTERNAL REPAIR DOUBLER PER SRM 53-04.

Part: FLOOR PANEL — DELAMINATED (BS 148-160) · airframe 47,849 hrs · 35,068 cycles

CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-05 AND ASA DWG S4932106.

Part: FLOOR PANEL — DELAMINATED (BS 148-160) · airframe 47,849 hrs · 25,068 cycles

CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-05 AND ASA DWG S4932106.

Part: SHEAR TIE — CORRODED (BS 1231) · corrosion level 2 · airframe 47,849 hrs · 25,068 cycles

AFT CARGO BAY SHEAR TIE IS CORRODED. REPLACED SHEAR TIE PER SRM 51-10-4 AND 51-30-5.

Part: INSERT — CORRODED (FLOOR PANEL) · airframe 47,849 hrs · 25,068 cycles

CABIN FLOOR PANEL HAS CORRODED INSERTS. REPLACED FLOOR PANEL IAW SRM 53 05 AND ASA DWG S4932106.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,849 hrs · 25,068 cycles

AFT CARGO BAY THRESHOLD WEB GUSSET IS CORRODED. REPLACED GUSSET IAW SRM 53 14 3 51 10 2 51 10 3. 51 30 2. AND 51 30 5.

Part: LANYARD — WORN (SLIDE) · airframe 47,504 hrs · 24,901 cycles

INADVERTENTLY DEPLOYED TAIL CONE WHICH SHOULD HAVE ALSO CAUSED AFT EMERGENCY SLIDE TO DEPLOY. LANYARD VELCRO AND SNAP PULLED LOOSE FROM THE SLIDE COVER BUT THE SLIDE DID NOT DEPLOY. RETRIGGER SLIDE ASSEMBLY WITH NEW LANYARD. ENGINEERING INVESTIGATION HAS BEEN INITIATED TO DETERMINE PROBABLE CAUSE OF SLIDE FAILURE TO DEPLOY.

Part: VANE — DENTED (TE FLAP)

OKC - FOUND HV-CHECK, RIGHT FLAP VANE DENTED ON LOWER SURFACE. REMOVED DAMAGED SECTION. INSTALLED FILLER AND DOUBLER. (M)

Part: VANE — GOUGED (RT TE FLAP)

OKC - FOUND DURING HV-CHECK, RIGHT FLAP VANE GOUGED. REPAIRED DAMAGED SECTION PER SRM 51-70. (M)

Part: SKIN — DENTED (NR 2 SLAT)

OKC - FOUND DURING HV-CHECK, LEFT NR 2 SLAT L/E DENTED. REPAIRED DAMAGED SECTION PER SRM 57-09. (M)

Part: WIRE — MISINSTALLED (EMERGENCY LIGHT)

SEA - FOUND DURING PREFLIGHT, COCKPIT OVERHEAD FLOOD LIGHT FOUND INOPERATIVE UPON TEST. REROUTED MIS-CONNECTED FLOOR LIGHT WIRE. LIGHT THEN OPERATED PROPERLY. (M)

Part: WEB — CORRODED (FUSELAGE)

OKC - DURING HV CHECK, FOUND AFT CARGO BAY DOOR CUTOUT INTERNAL WEB IS CORRODED AROUND ATTACH HARDWARE AT FS 1155-1211. REPLACED DAMAGED AREA OF WEB AND INSTALLED DOUBLER PER SRM 51-70-4. (M)

Part: SEAT TRACK — CHAFED (FUSELAGE)

OKC - DURING HV CHECK, FOUND CABIN SEAT TRACK IS CHAFED AT FS 1212-1322. REPLACED DAMAGED SECTION OF TRACK PER SRM 53-05. (M)

Part: ATTACH ANGLE — CORRODED (FUSELAGE)

OKC - DURING HV CHECK, FOUND ATTACH ANGLE IS CORRODED AT FS 1007. REPLACED ANGLE PER SRM 51-10-4. (M)

Part: FLOOR PANEL — DELAMINATED (FUSELAGE)

OKC - FOUND FORWARD CABIN FLOOR PANEL STATION 148 TO STATION 168 HAS DELAMINATION AROUND FASTENER HOLES. FABRICATED REPLACEMENT FLOOR PANEL IAW MD80 SRM 53-05. (M)

Part: FLOORBOARD — CORRODED (FUSELAGE)

OKC - FOUND CABIN FLOORBOARD STATION 200-256 HAS SEVERAL CORRODED INSERTS. FABRICATED REPLACEMENT FLOORBOARD IAW MD80 SRM 53-05. (M)

Part: FLOOR PANEL — CRACKED (FUSELAGE)

OKC - FOUND INSERTS PULLING OFF, CORRODED AND PANEL CRACKED AT LOWER SURFACE, FORWARD CABIN STATION 148-200. FABRICATED REPLACEMENT FLOOR PANEL IAW MD80 SRM 53-05. (M)

Part: FRAME — CORRODED (FUSELAGE)

OKC - DURING HV CHECK, FOUND FRAME IS CORRODED AT FS 1211. REPLACED FRAME PER SRM 51-30-2. (M)

Part: SEAT TRACK — CHAFED (FUSELAGE)

OKC - DURING HV CHECK, FOUND SEAT TRACK CHAFED AT FS 1212. REPLACED DAMAGED SECTION OF TRACK PER SRM 53-05. (M)

Part: FLOOR PANEL — CORRODED (FUSELAGE)

OKC - DURING HV CHECK, FOUND FLOORBOARD IS CORRODED AND DELAMINATED AT FS 843-886. REPLACED FLOOR PANEL PER SRM 53-05. (M)

Part: SEAT TRACK — CHAFED (FUSELAGE)

OKC - DURING HV CHECK, FOUND SEAT TRACK CHAFED AT FS 1212. REPLACED DAMAGED SECTION OF TRACK PER SRM 53-05. (M)

Part: DOOR FRAME — CORRODED (FUSELAGE)

OKC - DURING HV CHECK, FOUND AFT CARGO BAY DOOR BEAM PREVIOUS REPAIR ANGLE/SKIN IS CORRODED UNDER FORWARD AND AFT LOWER DOOR STOP MOUNTS. REPLACED DOOR BEAM PER SRM 51-30-2. (M)

Part: YOKE — DAMAGED (ENGINE MOUNT)

OKC - DURING HV CHECK, FOUND RIGHT ENGINE MOUNT YOKE UPPER ISOLATOR CAVITY CAD PLATING IS MISSING. REPLACED MOUNT YOKE PER MM 71-20-03. (M)

Part: WEB — CRACKED (FUSELAGE)

OKC - HV CHECK, FOUND AFT CARGO BAY FLOOR WEB IS CRACKED AT FS 1287-1307. REPLACED WEB PER SRM 51-30-5. (M)

Part: LONGERON — CORRODED (FUSELAGE)

OKC - DURING HV CHECK, FOUND LONGERON 28L IS CORRODED AT FS 1231. REMOVED DAMAGED SECTION AND INSTALLED SPLICE PER SRM 53-02. (M)

Part: FLOOR PANEL — GOUGED (FUSELAGE)

OKC - DURING HV CHECK, FOUND CABIN FLOOR PANEL IS GOUGED AT FS 148.5-200. REPLACED FLOOR PANEL PER SRM 53-05. (M)

Part: FLOOR PANEL — GOUGED (FUSELAGE)

OKC - DURING HV CHECK, FOUND CABIN FLOOR PANEL IS GOUGED AND DELAMINATED AT FS 1156-1250. REPLACED FLOOR PANEL PER SRM 53-05. (M)

Part: FLOOR PANEL — CRACKED (FUSELAGE)

OKC - DURING HV CHECK, FOUND CABIN FLOORBOARD IS CRACKED AND DELAMINATED AT FS 927-1003. REPLACED FLOOR PANEL PER SRM 53-05. (M)

Part: FLOOR PANEL — CORRODED (FUSELAGE)

OKC - DURING HV12 CHECK, FOUND CABIN FLOOR PANEL HAS MISSING AND CORRODED INSERTS AT FS 148-200. REPLACED FLOOR PANEL PER SRM 53-05. (M)

Part: SKIN — CRACKED (FUSELAGE)

OKC - DURING HV12 CHECK, FOUND NLG LEFT DOOR AFT HINGE CUTOUT IS CRACKED. REMOVED DAMAGED AREA AND INSTALLED DOUBLER PER SRM 53-05. (M)

Part: LONGERON — CORRODED (FUSELAGE)

OKC - DURING HV12 CHECK, FOUND LONGERON IS CORRODED ON UNDERSIDE AT FS 1219. REMOVED DAMAGED SECTION AND INSTALLED SPLICE AND STRAP PER SRM 53-02. (M)

Part: LONGERON — CORRODED (FUSELAGE)

OKC - DURING HV12 CHECK, FOUND LONGERON 29R IS CORRODED AT FS 1295. REMOVED DAMAGE AND INSTALLED REPAIR CHANNEL PER SRM 53-02. (M)

Part: DOOR FRAME — CRACKED (FUSELAGE)

OKC - DURING HV12 CHECK, FOUND NLG RIGHT DOOR JAMB IS CRACKED AT LOWER END OF FRAME. REMOVED DAMAGED AREA AND INSTALLED REPAIR ANGLE, FILLER, AND DOUBLER PER SRM 53-05. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

OKC - DURING HV12 CHECK, FOUND SHEAR TIE CORRODED AT FS 1287. REMOVED DAMAGED SECTION AND INSTALLED FILLER AND DOUBLER PER SRM 53-03. (M)

Part: WEB — CORRODED (FUSELAGE)

OKC - DURING HV12 CHECK, FOUND WEB CORRODED AT FS 294-313. REMOVED DAMAGED SECTION AND INSTALLED FILLER AND DOUBLER PER SRM 51-70-4. (M)

Part: SKIN — DENTED (CARGO DOOR)

OKC - DURING HV12 CHECK, FOUND AFT CARGO BAY DOOR SKIN IS DENTED AT FS 1199. REMOVED DAMAGED AREA AND INSTALLED FILLER AND DOUBLER PER SRM 52-05. (M)

Part: SKIN — CRACKED (FUSELAGE)

OKC - DURING HV12 CHECK, FOUND NLG DOOR AFT HINGE CUTOUT IS CRACKED. REMOVED DAMAGED AREA AND INSTALLED DOUBLER PER SRM 53-05. (M)

Part: FLOOR PANEL — DELAMINATED (FUSELAGE)

OKC - DURING HV12 CHECK, FOUND CABIN FLOOR PANEL HAS DELAMINATED AREAS AT FS 864-886. REPLACED PANEL PER SRM 53-05. (M)

Part: FLOOR PANEL — DELAMINATED (FUSELAGE)

OKC - DURING HV12 CHECK, FOUND CABIN FLOOR PANEL HAS SEVERAL DELAMINATED AREAS AT FS 200-256. REPLACED FLOOR PANEL PER SRM 53-05. (M)

Part: FLOORBOARD — GOUGED (FUSELAGE)

OKC - FOUND CABIN FLOORBOARD X=-44 STATION 1079-1155 HAS GOUGES AROUND EDGES AND IN SKIN. FABRICATED REPLACEMENT FLOORBOARDS IAW MD80 SRM 53-05. (M)

Part: FLOORBOARD — DELAMINATED (FUSELAGE)

OKC - FOUND CABIN FLOORBOARD STATION 946-1003 CENTER HAS DELAMINATION AROUND EDGES. FABRICATED REPLACEMENT FLOORBOARD IAW MD80 SRM 53-05. (M)

Part: FLOORBOARD — GOUGED (FUSELAGE)

OKC - FOUND CABIN FLOORBOARD X=22 STATION 1117-1174 HAS GOUGES AND DELAMINATED EDGES. FABRICATED REPLACEMENT FLOORBOARD IAW MD80 SRM 53-05. (M)

Part: FLOORBOARD — CRACKED (FUSELAGE)

OKC - FOUND CABIN FLOORBOARD STATION 927-1003 HAS CRACK IN SKIN AND DELAMINATION AROUND EDGES. FABRICATED REPLACEMENT FLOORBOARD IAW MD80 SRM 53-05. (M)

Part: INSERT — CORRODED (FUSELAGE)

OKC - DURING CABIN FLOORBOARD STATION 160-200 HAS SEVERAL CORRODED INSERTS. FABRICATED REPLACEMENT FLOORBOARD IAW MD80 SRM 53-05. (M)

Part: FLOORBOARD — CORRODED (FUSELAGE)

OKC - FOUND CABIN FLOORBOARD STATION 200-256 X=14-X=22 HAS SEVERAL CORRODED INSERTS. FABRICATED REPLACEMENT FLOORBOARD IAW MD80 SRM 53-05. (M)

Part: FLOORBOARD — DELAMINATED (FUSELAGE)

OKC - DURING FLOOR PANEL AT FS 617 TO 655 X = 22, DELAMINATED. FABRICATED REPLACEMENT FLOOR PANEL IAW MD80 SRM 53-05. (M)

Part: INSERT — CORRODED (FLOORBOARD)

OKC - FOUND CABIN FLOORBOARD STATION 160-200 HAS SEVERAL INSERTS CORRODED AND BENT. FABRICATED REPLACEMENT FLOORBOARD IAW MD80 SRM 53-05. (M0

Part: WEB — CORRODED (FUSELAGE)

OKC - FOUND CORROSION AT WEB LONGERON 18 BETWEEN STATION 275 AND 294. REMOVED DAMAGED, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW MD80 SRM 53-01. (M)

Part: WEB — CRACKED (FUSELAGE)

OKC - FOUND CRACKED FLOOR WEB AT STATION 218, RBL 47 FORWARD CABIN. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW MD80 SRM 51-70-4. (M)

Part: CONNECTOR — DISCONNECTED (LIGHT MODULE)

SEA PREFLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE NEAR AFT GALLEY. RECONNECTED MODULE CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M)

Part: LANYARD — DISCONNECTED (ESCAPE SLIDE)

PDX PREFLIGHT CHECK, FOUND FORWARD PAX L1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (M)

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT)

SEA - DURING LINE CHECK, EMERGENCY TRACK LIGHTING AT ROW 27-30 WAS FOUND TO BE INOPERATIVE. RECONNECTED WIRING. LIGHTS THEN OPERATED PROPERLY. (M)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

OAK - DURING C-CHECK, FOUND MID CARGO BAY LEFT FLOOR SUPPORT CRACKED AT TRACK ATTACH RIVET. REPLACED FLOOR SUPPORT AT FS 560 PER SRM 51-10-4 AND 30-2. (M)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

OAK - DURING C-CHECK, FOUND MID CARGO BAY LEFT FLOOR SUPPORT CRACKED AT TRACK ATTACH RIVET. REPLACED FLOOR SUPPORT AT FS 579 PER SRM 51-10-4 AND 30-2. (M)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

OAK - DUIRNG C-CHECK, FOUND MID CARGO BAY LEFT FLOOR SUPPORT CRACKED AT TRACK ATTACH RIVET. REPLACED FLOOR SUPPORT AT FS 712 PER SRM 51-10-4 AND 30-2. (M)

Part: SEALANT — MISSING (TE FLAP)

OAK - DURING C-CHECK, LT WING TRAILING EDGE OUTBOARD FLAP HINGE PIVOT BOLT SEALANT WAS FOUND TO BE MISSING. REPLACED SEALANT IAW ALASKA EA 57-50-10198. (M)

Part: SKIN — DENTED (FUSELAGE)

OAK - DURING C-CHECK, FUSELAGE SKIN IS CREASED & DENTED AT FS 1183 AT 6 O'CLOCK POSITION. INSTALLED DOUBLER PRE SRM 51-10-3 AND 51-103B. (M)

Part: LIGHT — MALFUNCTIONED (CABIN)

SEA - DURING LINE CHECK, FOUND PORTABLE EMERGENCY LIGHT WOULD NOT EXTINGUISH. REPLACED PORTABLE LIGHT ASSEMBLY. OP TESTED OK. (M)

Part: MODULE — DISCONNECTED (CABIN)

SFO - DURING PREFLIGHT CHECK, TRACK LIGHTS FROM FORWARD GALLEY TO MID 1ST CLASS WERE FOUND TO BE INOPERATIVE. RECONNECTED LIGHTING MODULES. LIGHTS THEN OPERATED PROPERLY. (M)

Part: LANYARD — DISCONNECTED (R1 DOOR)

SFO - DURING PREFLIGHT CHECK, R1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND TO BE DETACHED FROM DOOR. REATTACHED LANYARD BETWEEN GIRT BAR AND DOOR SLIDE COVER. (M)

Part: LIGHT — INOPERATIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE PORTABLE EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED THE PORTABLE EMERGENCY LIGHT ASSEMBLY AND THE LIGHT OPERATED NORMALLY. (M)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

SEA - DURING PREFLIGHT CHECK, OVERWING EMEREGNCY EXIT ILGHS WERE DETERMINED TO BE INOPERATIVE. REPLACED ASSOCIATED BATTERY PACK (POWER SUPPLY). LIGHTS THEN OPERATED NORMALLY. (M)

Part: DOOR — OUT OF RIG (L1 DOOR)

SEA - DURING PREFLIGHT CHECK, L1 DOOR (FORWARD LEFT CREW/PAX DOOR) WAS FOUND TO BE DIFFICULT TO OPEN AND CLOSE. RIGGED L1 DOOR. DOOR THEN OPERATED PROPERLY. (M)

Part: DOOR — INOPERATIVE (MAIN PAX)

SEA - DURING PRE-FLIGHT CHECK, L1 DOOR (FWD LT CREW/PAX DOOR) WAS FOUND TO BE DIFFICULT TO OPEN AND CLOSE. REMOVED AND REPLACED L1 DOOR. DOOR THEN OPERATED NORMALLY. (M)

Part: DOOR — OUT OF ADJ (MAIN PAX)

SEA - DURING PRE-FLIGHT CHECK, L1 DOOR INTERNAL HANDLE WAS FOUND TO BE RUBBING AGAINST THE FORWARD LAVATORY WALL. READJUSTED DOOR PER MM 52-11-0. (M)

Part: DOOR — OUT OF RIG (ENTRY DOOR)

SEA - DURING PREFLIGHT CHECK, L1 DOOR FORWARD LEFT CREW/PAX DOOR WAS DETERMINED TO BE HARD TO OPEN. RE-RIGGED DOOR. DOOR THEN OPERATED PROPERLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

PDX - DURING SERVICE CHECK, OVERWING EMERGENCY SPOTLIGHTS CAME ON WHEN SWITCHING FROM EXTERNAL POWER TO APU POWER. EMERGENCY LIGHTS SWITCH IN COCKPIT WAS IN OFF POSITION. REMOVED AND REPLACED BATTERY PACK ASSEMBLY. LIGHTS THEN OPERATED NORMALLY. (M)

Part: A/C PACK — CONTAMINATED (A/C BAY)

LAX - FLT 285 - DURING CLIMB THROUGH 3000 FEET, STRONG CHEMICAL/OIL ODOR NOTED IN PASSENGER CABIN. RETURNED TO LAX. REPLACED AIR CONDITIONING SYSTEM RIGHT COOLING TURBINE ASSEMBLY. SYSTEM THEN OP CHECKED OK. (M)

Part: DOOR — LACK OF LUBE (L1 DOOR)

LAX - AFTER ARRIVAL AT GATE, L1 DOOR (FORWARD LEFT CREW/PAX DOOR) WAS DETERMINED TO BE HARD TO OPEN. LUBRICATED DOOR HINGE. DOOR THEN OPERATED PROPERLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

SES - DURING LINE CHECK, EMERGENCY TRACK LIGHTS BETWEEN CABIN ROWS 13-21 WERE DETERMINED TO BE INOPERATIVE. REPLACED ASSOCIATED POWER SUPPLIES (BATTERY PACKS). LIGHTS THEN OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (ROW 25)

SEA - DURING MAINTENANCE CHECK, FLOOR EMERGENCY TRACK LIGHTS AT ROW 25 WERE FOUND TO BE INOPERATIVE. REPLACED EMERGENCY BATTERY ASSY. LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (AFT CABIN)

SEA - DURING MAINTENANCE CHECK, AFT EMERGENCY LIGHTS ILLUMINATED WHEN TRANSFERRING TO APU POWER. REPLACED BATTERY ASSEMBLY. OPS CHECKED NORMALLY. (M)

Part: LATCH — OUT OF ADJ (PAX DOOR) · airframe 28,621 hrs · 15,473 cycles

SEA - FLT 482 - PRIOR TO FLIGHT, THE L1 DOOR WAS REPORTED TO BE DIFFICULT TO OPEN AND CLOSE. SHIMMED THE DOOR OVER CENTER BUMPER AND REMOVED THREE SHIMS FROM THE BAYONET ROLLER. THE DOOR OPERATED NORMALLY. (X)

Part: POWER SUPPLY — DISCHARGED (AFT CABIN)

SEA - DURING MAINTENANCE CHECK, THE AFT CABIN EMERGENCY FLOOR TRACK LIGHT AND TAIL COMPARTMENT EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED THE POWER SUPPLY AND ALL LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (AFT CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY LIGHTS IN TAILCONE AREA INOPERATIVE. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M)

Part: LATCH — OUT OF ADJ (PAX DOOR)

SEA - PRIOR TO F608, THE L1 DOOR WAS DIFFICULT TO OPEN. ADJUSTED DOOR AND DOOR OPERATED NORMALLY. (M)

Part: LATCH — LACK OF LUBE (PAX DOOR)

MLAX-THE L1 DOOR HANDLE WAS FOUND TO BE STIFF DURING CLOSING.LUBRICATED DOOR AND DOOR OPERATED NORMALLY.

Part: SEAL — CONTAMINATED (PAX DOOR)

AFTER ARRIVAL OF FLIGHT 405; CREW REPORTED THE L1 DOOR WAS DIFFICULT TO OPEN. CLEANED PAINT OVERSPRAY FROM DOOR SEAL AND SEAL MATING SURFACE. ACCOMPLISHED GROUND PRESSURIZATION CHECK TO 3.0 PSID, NO LEAK NOTED. OPERATED DOOR THROUGH SEVERAL CYCLES AND OPERATED NORMALLY.

Part: SIGN — INOPERATIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE FORWARD LEFT OVERWING EMERGENCY EXIT IDENTIFIER WAS FOUND TO HAVE ONLY TWO LAMPS ILLUMINATED. REPLACED EMERGENCY EXIT IDENTIFIER AND OPERATED NORMALLY. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON SHEAR TIE, FS 1220, LONGERON 30 TO 29R. REMOVED AND REPLACED SHEAR TIE IAW DC9 SRM 51-30-05. (M)

Part: WEB — CORRODED (FUSELAGE)

PHX-DURING 30K CHECK CORROSION WAS FOUND ON CUSP WEB, FS 446 TO 465, LONGERON 18R. REMOVED DAMAGED MATERIAL AND INSTALLED DOUBLER IAW DC9 SRM 53-01. FIG 4

Part: CARGO TRACK — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON CARGO TRACK, FS 1174-1309, LONGERON 28L. REMOVED AND REPLACED CARGO TRACK SECTION IAW DC9 SRM 51-30-00. (M)

Part: CARGO TRACK — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON CARGO TRACK, FS 1113 TO 1155, LONGERON 28R. REMOVED AND REPLACED CARGO TRACK SECTION IAW DC9 SRM 51-30-00. (M)

Part: LONGERON — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON LONGERON 29L, FS 1200. REMOVED DAMAGED MATERIAL AND SPLICED IN NEW SECTION FROM FS 1200 TO 1240 IAW DC9 SRM 53-02, FIG 18. (M)

Part: WEB — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON CUSP WEB, FS 503 TO 598, LBL 52. REMOVED DAMGED MATERIAL AND INSTALLED FILLER AND DOUBLER IAW DC9 SRM 51-10-03. (M)

Part: FRAME — CORRODED (FUSELAGE)

PHX-DURING 30K CHECK CORROSION WAS FOUND ON FRAME FS 1271 LONGERON 28L TO 28R. REMOVED DAMAGED MATERIAL AND SPLICED IN NEW SECTION IAW DC9 SRM 53-03, FIG 2A.

Part: WEB — CORRODED (FUSELAGE)

PHX-DURING 30K CHECK CORROSION AND CRACKS WERE FOUND ON CUSP WEB, FS1250 TO 1309, LONGERON 18R. REMOVED AND REPLACED WEB IAW DC9 SRM 53-01.

Part: LONGERON — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON LONGERON 28L, FS 1200. REMOVED DAMAGED MATERIAL AND SPLICED IN NEW SECTION FROM FS 1200 TO 1220 IAW DC9 SRM 53-02, FIG 18. (M)

Part: LONGERON — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON LONGERON 30, FS 1241. REMOVED DAMAGED MATERIAL AND SPLICED IN NEW SECTION FROM FS 1241 TO 1275 IAW DC9 SRM 53-02, FIG 18 AND 53-14-03. (M)

Part: CARGO TRACK — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON CARGO TRACK, FS 1211 TO 1309, LONGERON 28R. REMOVED AND REPLACED CARGO TRACK SECTION IAW DC9 SRM 51-30-01. (M)

Part: FRAME — CORRODED (FUSELAGE)

PHX- DURING 30K CHECK CORROSION WAS FOUND ON FRAME, FS1231, LONGERON 28L TO 27R. REMOVED DAMAGED MATERIAL AND SPLICED IN NEW SECTION FROM LONGERON 26L TO 29R IAW DC9 SEM 53-03, PG 4A.

Part: FRAME — CORRODED (FUSELAGE)

DURING 30K CHECK CORROSION WAS FOUND ON FRAME, FS 1250, LONGERON 30.REMOVED DAMAGED MATERIAL AND SPLICED IN NEW SECTION FROM LONGERON 27L TO 28R IAW DC9 SRM 53-03, PG 4A.

Part: SHEAR TIE — CORRODED (FUSELAGE)

PHX-DURING 30K CHECK CORROSION WAS FOUND ON SHEAR TIE, FS 1211, LONGERON 30 TO 29R.REMOVED AND REPLACED SHEAR TIE IAW DC9 SRM 51-30-05.

Part: LONGERON — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON LONGERON 28R, FS 1254. REMOVED DAMAGED MATERIAL AND SPLICED IN NEW SECTION FROM FS 1254 TO 1280 IAW DC9 SRM 53-02, FIG 18. (M)

Part: SEAT TRACK — GOUGED (FUSELAGE)

DURING 30K CHECK GOUGES WERE FOUND ON SEAT TRACK, FS 1206 TO 1248, LBL 22.REMOVED AND REPLACED SEAT TRACK SECTION FROM FS 1029 TO 1306 IAW DC9 SRM 53-05.

Part: WEB — CORRODED (FUSELAGE)

PHX-DURING 30K CHECK CORROSION WAS FOUND ON CUSP WEB, FS 1211 TO 1231, LONGERON 18R. REMOVED AND REPLACED WEB FROM FS1174 TO 1250 IAW DC9 SRM 51-30-02 AND 51-30-05.

Part: WEB — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON CUSP WEB, FS 217, LBL 6. REMOVED DAMAGED MATERIAL AND INSTALLED NEW SECTION AND DOUBLER FROM FS 214-219 IAW DC9 SRM 53-01, FIG 4, SH 3. (M)

Part: WEB — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON FLOOR WEB, FS 570, LONGERON 18R. REMOVED AND REPLACED WEB FROM FS 503 TO 597 IAW DC8 SRM 51-01, PAGE 1. (M)

Part: WEB — CORRODED (FUSELAGE)

PHX-DURING 30K CHECK CORROSION WAS FOUND ON CUSP WEB, FS 427 TO 446, LONGERON 18R. REMOVED DAMAGED MATERIAL AND INSTALLED DOUBLER IAW DC9 SRM 53-01, FIG 4.

Part: SKIN — CORRODED (FUSELAGE)

DURING 30K CHECK CORROSION WAS FOUND ON INTERIOR SURFACE OF FUSELAGE SKIN, FS 1220, LONGERON 29R. REPAIRED IAW ASA EA 5330-01439.

Part: WEB — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON FLOOR WEB, FS 1184, LONGERON 18R. REMOVED AND REPLACED WEB FROM FS 1174 TO 1250 IAW DC9 SRM 51-30. (M)

Part: FRAME — CORRODED (FUSELAGE)

PHX-DURING 30K CHECK CORROSION WAS FOUND ON FRAME, FS 1231, LONGERON 27R TO 28R. REMOVED DAMAGED MATERIAL AND SPLICED IN NEW SECTION IAW DC9 SRM 53-03.

Part: SKIN — DENTED (FUSELAGE)

DURING 30K CHECK DENT WAS FOUND IN FUSELAGE SKIN, FS 240 TO 250, LONGERON 17L TO 18L. REWORKED TO CONTOUR AND INSTALLED TITANIUM DOUBLER IAW DC9 SRM 53-04, FIG. 38, SH 28 THROUGH SH 31.

Part: ANGLE — CORRODED (FUSELAGE)

PHX - DURNG 30K CHECK, FOUND CORROSION ON CUSP ANGLE, FS 1193 TO 1210, LONGERON 18R. REMOVED DAMAGED MATERIAL AND SPLICED IN CUSP ANGLE REPAIR SECTION FROM FS 1185 TO 1240 IAW DC9 SRM 53-05, FIG 25 AND INSTALLED FRAME REPAIR SECTION IAW DC9 SRM 53-03, FIG 32. (M)

Part: WEB — CORRODED (FUSELAGE)

PHX - DURING 30K CHECK, FOUND CORROSION ON CUSP WEB, FS 313 TO 389, LBL 52. REMOVED AND REPLACED WEB IAW DC9 SRM 51-30-01. (M)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

PHX - DURING 30K CHECK, THE EXTERIOR OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. REPLACED THE POWER SUPPLY AND OPERATED NORMALLY. (M)

Part: SLIDE — FAILED (SERVICE DOOR)

PHX - DURING 30K CHECK, THE L2 DOOR EMERGENCY EVACUATION SLIDE FAILED THE EMERGENCY LIGHT AMP TEST. REPLACED THE L2 DOOR EMERGENCY EVACUATION SLIDE ASSEMLBY. (M)

Part: BATTERY — DISCHARGED (POWER SUPPLY)

PDX - DURING MAINTENANCE CHECK, THE TAILCONE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED POWER SUPPLY BATTERY AND LIGHT OPERATED NORMALLY. (M)

Part: LIGHT — INOPERATIVE (PAX DOOR) · airframe 27,846 hrs · 15,098 cycles

SFO - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED LIGHT ASSEMBLY AND OPERATED NORMALLY. (X)

Part: BATTERY — DISCHARGED (ROWS 14-17)

SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS AT ROWS 14-17 WERE FOUND TO BE INOPERATIVE. REPLACED BATTERY AND LIGHTS OPERATED NORMALLY. (M)

Part: LIGHT — INOPERATIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE FORWARD F/A PORTABLE EMERGENCY LIGHT WAS FOUND TO BE BROKEN. REPLACED LIGHT ASSEMBLY AND LIGHT OPERATED NORMALLY. (M)

Part: LIGHT — INOPERATIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHT AT ROW 10 WAS FOUND TO BE INOPERATIVE. TIGHTENED LOOSE GROUND IN OVERHEAD PANEL AND LIGHT OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - PRIOR TO DEPARTURE OF FLT 119, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. REPAIRED WIRING IN FLOOR TRACK AT ROW 3 AND OPERATED NORMALLY. (X)

Part: BATTERIES — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 14 TO 17 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M)

Part: LIGHT — DEFECTIVE (L1 DOOR)

LAX - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (X)

Part: LIGHT — DEFECTIVE (CABIN)

LAX - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M)

Part: SKIN — CRACKED (RT WING)

SEA - RIGHT WING LOWER SURFACE SKIN CRACKED AT FORWARD OUTBOARD RADIUS OF FUEL PANEL DOOR CUTOUT. REPAIRED PER ASA EA 5730-01049. (M)

Part: LANYARD — DISCONNECTED (TAILCONE)

SEA - DURING REPLACEMENT OF THE TAILCONE EMERGENCY EVACUATION SLIDE THE DEPLOY LANYARD WAS FOUND DISCONNECTED FROM THE GIRT TAB. REPLACED THE TAILCONE EMERGENCY EVACUATION SLIDE AND CHECKED THE DEPLOY LANYARD FOR PROPER INSTALLATION. (M)

Part: LATCH MECHANSIM — STUCK (L2 DOOR)

SEA - PRIOR TO DEPARTURE OF FLT 226, CREW REPORTED THE L2 DOOR WARNING LIGHT WOULD NOT EXTINGUISH. FOUND DOOR LATCH MECHANISM STUCK, LUBED DOOR LATCH MECHANISM AND OPERATED NORMALLY. (M)

Part: LANYARD — BROKEN (L1 DOOR)

RNO - PRIOR TO DEPARTURE OF FLT 613, CREW REPORTED THE L1 DOOR EMERGENCY EVACUATION SLIDE DEPLOY LANYARD WAS BROKEN. REPLACED THE DEPLOY LANYARD AND INSPECTED THE SLIDE AND COVER FOR SECURITY. (M)

Part: LIGHT — INOPERATIVE (CABIN)

PDX - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M)

Part: COFFEE MAKER — MALFUNCTIONED (NR 3 GALLEY)

ANC - FLT 107 - FLIGHT ATTENDANT REPORTED ELECTRICAL SMOKE ODOR IN GALLEY NR 3 DURING CRUISE. DEACTIVATED GALLEY POWER AND ODOR DISSIPATED. OPERATED ALL AFT GALLEY APPLIANCES AND UNABLE TO DUPLICATE ODOR. REPLACED NR 3 GALLEY COFFEE MAKER AND NO EVIDENCE OF OVERHEATING FOUND. (W)