N964AS
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.
160 reports on file, 1995-02-14 – 2012-03-20.
Part: UNKNOWN — MALFUNCTIONED (COCKPIT) · airframe 54,362 hrs · 27,886 cycles
AIR TURNBACK LOST AUTOTHROTTLES, AUTO PILOTS, BOTH FMA AND FLIGHT DIRECTORS. PERFORMED RETURN TO SERVICE CHECK ON NR 1 AND NR 2 FMGS IAW AMM 22-01-05. NO FAULTS NOTED. BOTH SYSTEMS CHECK OK.
Part: WIRE HARNESS — CORRODED (FUEL SYSTEM) · airframe 54,226 hrs · 27,820 cycles
(AIR TURNBACK) EN ROUTE/CLIMBOUT, APPEARS CENTER FUEL TANK NOT SUPPLING FUEL. FOUND AFT/CTR BOOST PUMP C/B OPEN (ALL TESTED GOOD PRE-FLT). COULD NOT VERIFY, FWD/CTR PUMP LEVEL FLIGHT NORMAL. REMOVED AND REPLACED CENTER WING AFT BOOST PUMP HARNESS IAW SWPM 28-10-01. LEAK AND OPS CHECK NORMAL IAW 28-20-07.
Part: COMPUTER — MALFUNCTIONED (AUTOTHROTTLE SYS) · airframe 54,217 hrs · 27,815 cycles
NR 1 AUTOTHROTTLE WOULD NOT ENGAGE AT START OF TAKEOFF ROLL. RERACKED NR 1 DFGC RAN RTS CHECK. A/T CHECKS NORMAL PER MD-80 MM 22-01-09. REMOVED PLACARD.
Part: LIGHT — INTERMITTENT (CABIN) · airframe 54,114 hrs · 27,775 cycles
L1 DOOR PORTABLE EMERGENCY LIGHT ON/OFF SWITCH INTERMITTENT. REMOVED AND REPLACED L1 DOOR PORTABLE EMERGENCY LIGHT PER AMM 33-53-00. OPERATIONAL CHECK GOOD.
Part: ADC — FAILED (ZONE 100) · airframe 54,080 hrs · 27,758 cycles
FIRST OFFICER'S AIRSPEED SHOWS OVERSPEED, CAPTAIN'S AIRSPEED SHOWING 250. REPLACED NR 2 CADC IAW AMM 34-16-01. OPS CHECKED NORMAL. HIGH LEVEL PITOT STATIC SYSTEM CHECKED PER AMM 34-11-00. NO LEAKS NOTED.
Earlier reports · 1995–2011 · 155 reports
2011
Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 53,240 hrs · 27,353 cycles
EMERGENCY LIGHTS IN CABIN CEILING, ROWS 9 THRU 10 INOPERATIVE. REMOVED AND REPLACED EMERGENCY POWER SUPPLY IAW AMM 33-5001. OPERATION CHECKED GOOD.
Part: PUMP — MALFUNCTIONED (FUEL BOOST)
CENTER TANK FUEL DOES NOT BURN OUT WITH 4 MAIN WING BOOST PUMPS ON. REMOVED AND REPLACED FORWARD AND AFT CENTER TANK BOOST PUMPS PER MM 28-20-07. OPS CHECKED NORMAL.
2006
Part: DOUBLER — GOUGED (FLAP VANE)
FOUND RIGHT WING OUTBOARD FLAP INBOARD VANE SEGMENT HAS GOUGED REPAIR DOUBLER ON LEADING EDGE. REPLACED DAMAGED DOUBLER PER SRM 51 70 2 PARA 1 3 AND 13.
Part: CABLE — MISINSTALLED (R1 DOOR SLIDE) · airframe 45,871 hrs · 23,601 cycles
MANUAL INFLATION HANDLE DETACHED FROM SLIDE DEPLOYMENT LANYARD DURING DEPLOYMENT TEST. SLIDE ASSEMBLY WAS REPLACED. ENGINEERING EVALUATION, DTD 16 MAR 06, HAS DETERMINED THE CAUSE TO BE AN IMPROPERLY INSTALLED FIRING CABLE ASSEMBLY, SPECIFICALLY THE INCOMPLETE CAPTURE OF THE NYLON STRAP BY THE KEY RING.
2005
Part: INTERCOSTAL — CORRODED (FUSELAGE)
OKC - HV-CHECK, SEAT TRACK SUPPORT HAS CORRODED FASTENERS ON ATTACHING ANGLE INTERCOSTAL. REPLACED INTERCOSTAL. (M)
2004
Part: SKIN — GOUGED (FUSELAGE)
OKC - HV-CHECK, FUSELAGE GOUGED ON LEFT SIDE. REMOVED DAMAGED AREA AND INSTALLED DOUBLER. (M)
Part: DOOR FRAME — CRACKED (FUSELAGE)
OKC - HV-CHECK, FORWARD ENTRY DOOR JAMB WEB CRACKED. REMOVED DAMAGED AREA AND INSTALLED DOUBLER. (M)
Part: SKIN — DENTED (FS)
OKC - HV-CHECK, FUSELAGE DENTED BETWEEN LONGERON 16R AND 17R. RECONTOURED DENT AND INSTALLED DOUBLER. (M)
Part: SKIN — DENTED (CARGO DOOR)
OKC - HV-CHECK, AFT CARGO BAY DOOR IS DENTED. RECONTOURED DOOR SKIN AND INSTALLED DOUBLER. (M)
Part: LANYARD — DISCONNECTED (R1 DOOR SLIDE)
LAX - PREFLIGHT CHECK, AFT SERVICE L-2 DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (M)
Part: LANYARD — DISCONNECTED (L2 DOOR) · airframe 42,097 hrs · 21,769 cycles
PRE-FLIGHT CHECK- AFT SERVICE (L-2) DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD.
Part: LIGHT — INOPERATIVE (CABIN)
PDX LINE CHECK, FOUND PORTABLE EMERGENCY LIGHT, SITUATED NEAR THE FORWARD PASSENGER DOOR, IS INOPERATIVE. REPLACED LIGHT ASSEMBLY. (M)
Part: POWER SUPPLY — INOPERATIVE (COCKPIT)
SEA - PREFLIGHT CHECK, FOUND OVERHEAD EMERGENCY LIGHTS DID ILLUMINATE DURING CHECK. REPLACED ASSOCIATED POWER SUPPLY BATTERY PACK. LIGTHS THEN OPERATED NORMALLY. (M)
Part: POWER SUPPLY — NOT SEATED (COCKPIT)
SEA - DURING PREFLIGHT CHECK, FOUND COCKPIT OVERHEAD EMERGENCY FLOOD LIGHTS INOPERATIVE. RESEATED ASSOCIATED BATTERY PACK, POWER SUPPLY. LIGHTS THEN OPERATED NORMALLY. (M)
Part: ACCESS PANEL — CHAFED (LT WING)
OKC - HV-CHECK, LEFT WING FUEL PANELS 1307, 13333, AND 1379 ARE WORN AND CHAFED AT EDGE. REPLACED PANELS AT XFS 70-196, XCW58-70, AND XRS 445-447 RESECTIVELY. (M)
Part: ACCESS PANEL — CORRODED (LT WING)
OKC - HV-CHECK, LEFT WING FUEL PANELS 1363 AND 1367 ARE CORRODED ON LANDINGS. REPLACED PANELS, AT XRS 267-295 AND XRS 295-353 RESPECTIVELY. (M)
Part: ACCESS PANEL — CORRODED (RT WING)
OKC - HV-CHECK, RIGHT WING FUEL PANELS 1436 AND 1464 ARE CORRODED. REPLACED PANELS, AT XFS 58-70 AND XRS 324-353 RESPECTIVELY. (M)
Part: ACCESS PANEL — CORRODED (RT WING)
OKC - HV-CHECK, RIGHT WING FUEL PANEL AT HEAT BLANKET IS CORRODED. REPLACED PANEL. (M)
Part: FRAME — CORRODED (FUSELAGE)
OKC - HV-CHECK, FRAME LOWER FLANGE IS CORRODED. REPLACED FRAME. (M)
Part: TAB — DAMAGED (LT ELEVATOR)
OKC - HV-CHECK, LEFT ELEVATOR ANTI-FLOAT TAB MISSING COMPOUND. REPLACED MISSING COMPOUND. (M)
Part: ACCESS PANEL — CORRODED (RT WING)
OKC - HV CHECK, RIGHT WING FUEL ACCESS PANEL, FOR BOOST PUMP, IS CORRODED AROUND FASTENERS. REPLACED PANEL. (M)
Part: FLOOR PANEL — PUNCTURED (CABIN)
OKC - HV-CHECK, COCKPIT FLOOR PANEL PUNCTURED. REMOVED DAMAGED AREA. INSTALLED REPAIR DOUBLER. (M)
Part: TAB — DELAMINATED (RUDDER)
OKC - HV-CHECK, RUDDER TAB IS DELAMINATED AT BASE WEDGE. BOND REPAIRED. (M)
Part: VANE — CHAFED (TE FLAP)
RIGHT OUTBOARD FLAP INBOARD VANE CHAFED. REMOVED DAMAGE. INSTALLED REPAIR FILLER AND DOUBLER. (M)
Part: STRUCTURE — GOUGED (CARGO DOOR)
OKC - HV-CHECK, AFT CARGO BAY DOOR LOWER AFT INTERIOR GOUGED. REMOVED DAMAGED SECTIONS. REPAIRED SECTIONS PER EA 5210-01168. (M)
Part: SKIN — GOUGED (TE FLAP)
OKC - HV-CHECK, LEFT INBOARD FLAP LOWER SURFACE GOUGED. REMOVED DAMAGE. INSTALLED REPAIR DOUBLER. (M)
Part: LONGERON — CORRODED (FUSELAGE)
OKC - HV-CHECK, AFT CARGO BAY LONGERON 29R CORRODED. REMOVED DAMAGED SECTION. INSTALLED REPAIR ANGLE. (M)
Part: ACCESS PANEL — CORRODED (LT WING)
OKC - HV-CHECK, LEFT WING FUEL PANEL 1303, CORRODED ON LANDING. REPLACED PANEL. (M)
Part: TAB — DENTED (RT ELEVATOR)
OKC - HV-CHECK, RIGHT ELEVATOR GEAR TAB UPPER SURFACE IS DENTED. REMOVED DAMAGED SECTION. INSTALLED REPAIR FILLER AND DOUBLER. (M)
Part: FRAME — CORRODED (FUSELAGE)
OKC - HV-CHECK, AFT CARGO BAY FRAME CORRODED. REMOVED AND REPLACED DAMAGED SECTION. INSTALLED REPAIR SPLICE. (M)
Part: SEAT TRACK — CORRODED (FUSELAGE)
OKC - HV-CHECK, SEAT TRACK CORRODED. REPLACED SEAT TRACK. (M)
Part: VANE — CHAFED (TE FLAP)
OKC - HV-CHECK, LEFT OUTBOARD FLAP INBOARD VANE CHAFED. REMOVED DAMAGE. INSTALLED REPAIR FILLER AND DOUBLER. (M)
Part: BEARING — WORN (RUDDER)
OKC - HV-CHECK, RUDDER TORQUE TUBE BEARING IS WORN. REPLACED TORQUE TUBE ASSEMBLY. (M)
Part: VANE — CHAFED (TE FLAP)
OKC - HV-CHECK, LEFT OUTBOARD FLAP VANE CHAFED INBOARD EDGE. REMOVED DAMAGE. INSTALLED FILLER AND REPAIR DOUBLER. (M)
Part: CUSP WEB — CRACKED (FUSELAGE)
OKC - HV-CHECK, MID CARGO BAY CUSP WEB/MEMBRANE CRACKED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER. (M)
Part: INTERCOSTAL — CORRODED (FUSELAGE)
OKC - HV-CHECK, LONGERON 29L INTERCOSTAL CORRODED. REPLACED INTERCOSTAL. (M)
Part: STRUCTURE — CORRODED (CARGO DOOR)
OKC - HV-CHECK, AFT CARGO BAY DOOR CORRODED AT SEVERAL SLEEVE AND EXPANDER POINTS. REMOVED DAMAGED SECTIONS. INSTALLED REPAIR DOUBLERS. (M)
Part: FRAME — GOUGED (FUSELAGE)
OKC - HV-CHECK, RIGHT TAIL COMPARTMENT FRAME IS GOUGED. REMOVED DAMAGE. INSTALLED REPAIR PLATE AND ANGLE. (M)
Part: SKIN — DENTED (CARGO DOOR)
OKC - HV-CHECK, AFT CARGO BAY DOOR DENTED JUST BELOW TOP EDGE. RECONTOURED DOOR SKIN AND INSTALLED REPAIR DOUBLER. (M)
Part: SKIN — DENTED (AFT CARGO DOOR)
OKC - DURING HV-CHECK, AFT CARGO BAY DOOR DENTED JUST BELOW TOP EDGE. RECONTOURED DOOR SKIN AND INSTALLED REPAIR DOUBLER. (M)
Part: VANE — CHAFED (TE FLAP)
OKC - HV-CHECK, RIGHT OUTBOARD FLAP INBOARD VANE L/E IS CHAFED. REMOVED DAMAGE. INSTALLED REPAIR FILLER AND DOUBLER. (M)
Part: FLOORBOARD — DELAMINATED (FUSELAGE)
OKC - HV-CHK, CABIN FLOORBOARD PANEL WAS FOUND DELAMINATED WITH CORRODED INSERTS. REPLACED PANEL. (M)
Part: DOOR FRAME — BENT (FUSELAGE)
OKC - FOUND HV-CHECK, MID CARGO BAY DOOR FRAME LIP SEAL WAS FOUND BENT AND DENTED. REMOVED DAMAGED SECTION. INSTALLED REPAIR SPLICE AND DOUBLER. (M)
Part: FLOORBOARD — CORRODED (CABIN)
OKC - FOUND HV-CHECK, CABIN FLOORBOARD WAS FOUND TO BE DELAMINATED, WITH CRACKED 'W' CHANNEL. REPLACED PANEL. (M)
Part: FLOORBOARD — CORRODED (FUSELAGE)
OKC - HV-CHECK, CABIN FLOORBOARD PANEL HAS INSERTED PULLED THROUGH. REPLACED PANEL. (M)
Part: FLOORBOARD — CORRODED (FUSELAGE)
OKC - HV-CHECK, TWO CABIN FLOORBOARDS WERE FOUND TO HAVE CORRODED AND INSERTS FROM FS 541-617 AND BUTTOCK LINES L22 TO R22. BOTH PANELS WERE REPLACED. (M)
Part: FRAME — CORRODED (FUSELAGE)
OKC - HV-CHECK, AFT CARGO BAY FRAME LOWER FLANGE WAS FOUND CORRODED ABOVE LONGERON 30. REMOVED AND REPLACED DAMAGED SECTION. (M)
Part: ACCESS PANEL — CORRODED (LT WING)
OKC - HV-CHECK, SEVEN LEFT WING FUEL PANELS, FROM XRS 189 TO XRS 445, WERE FOUND CORRODED. ALL PANELS WERE REPLACED. (M)
Part: ACCESS PANEL — CORRODED (RT WING)
OKC - HV-CHECK, NINE RIGHT WING FUEL PANELS, FROM XRS TO XRS 477, WERE FOUND CORRODED. ALL PANELS WERE REPLACED. (M)
Part: FLOORBOARD — CORRODED (FUSELAGE)
OKC - HV-CHECK, CABIN FLOORBOARD PANEL HAS CORRODED INSERTS. REPLACED PANEL. (M)
Part: FLOORBOARD — DELAMINATED (CABIN)
OKC - HV-CHECK, FOUND CABIN FLOORBOARDS WERE FOUND DELAMINATED AT 25 DIFFERENT LOCATIONS FROM FUSELAGE STATION 148 TO 1250 AND BUTTOCK LINES L45 TO R50. DAMAGED FLOORBOARDS WERE REMOVED AND REPLACED IN ALL CASES.
2003
Part: WEB — CORRODED (FUSELAGE)
OKC - DURING C-CHECK, FOUND CUSP WEB CORRODED ON RIGHT SIDE FS 1250. REMOVED DAMAGED AREA. INSTALLED DOUBLER PER SRM 51-70-4. (M)
Part: SKIN — DENTED (FUSELAGE)
OKC - DURING C-CHECK, FOUND FUSELAGE SKIN IS DENTED AT FS 360. RECONTOURED/COLD-WORKED SKIN. INSTALLED DOUBLER PER SRM 53-04. (M)
Part: SKIN — CRACKED (FUSELAGE)
OKC - DURING C-CHECK, FOUND FUSELAGE SKIN IS CRACKED AT LEFT AFT NLG DOOR CUTOUT. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 53-05. (M)
Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)
PDX - DURING LINE CHECK, FOUND PORTABLE EMERGENCY LIGHT AT FORWARD ENTRY DOOR INOPERATIVE. REPLACED BATTERY. LIGHT THEN OPERATED PROPERLY. (M)
Part: FILLET — CORRODED (WING TO BODY)
OAK - DUIRNG C-CHECK, FOUND CORROSION ON LEFT WING-TO-BODY FAIRING FILLET PANEL 2108. INSTALLED DOUBLER AT FS 1079-1098 PER SRM 53-04. (M)
Part: FRAME — CORRODED (FUSELAGE)
OAK - DURING C-CHECK, FOUND CORROSION ON AFT SIDE OF CIRCUMFERENCE FRAME IN AFT CARGO BAY COMPARTMENT AT FS 1271 BETWEEN L28 AND R28 LONGERONS. REMOVED DAMAGED SECTION. SPLICED IN NEW SECTION PER SRM 5303, 51-10-3, 51-10-3B, 51-30-2, AND 50-30-5. (M)
Part: DRAIN — CORRODED (FUSELAGE)
OAK - DURING C-CHECK, FOUND CORROSION AROUND MID CARGO BAY BELLY DRAIN. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER PER SRM 53-04, 51-30-2, AND 51-30-5. (M)
Part: DRAIN — CORRODED (FUSELAGE)
OAK - DURING C-CHECK, FOUND CORROSION AROUND BELLY DRAINS IN AFT CARGO BAY. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER AT FS 1231 PER SRM 53-04. (M)
Part: FLOOR SUPPORT — CRACKED (FUSELAGE)
OAK - DURING C-CHECK, FOUND AFT CARGO BAY CIRCUMFERENTIAL FLOORBOARD SUPPORT CRACKED. CUTOUT DAMATED AREA AND INSTALLED DOUBLER AT FS 1079, L27L-L28L PER SRM 53-01, 51-10-4, AND 51-30-2. (M)
Part: NUT — LOOSE (COCKPIT WINDOW)
PDX - DURING PREFLIGHT CHECK, THE FIRST OFFICERS SLIDING CLEARVIEW WINDOW WAS FOUND TO BE DIFFICULT TO OPEN. AFT TRACK BLOCK SECURING NUT HAD BECOME LOOSE. RESECURED AFT TRACK BLOCK. WINDOW THEN OPERATED PROPERLY. (M)
2002
Part: WIRE — BROKEN (CABIN)
LAS - DURING PREFLIGHT CHECK, THE EMERGENCY TRACK LIGHTING IN FIRST CLASS CABIN WAS INOPERATIVE. REPAIRED BROKEN WIRE. LIGHTS THEN OPERATED PROPERLY. (M)
Part: LIGHT — INOPERATIVE (CABIN)
SEA - DURING PREFLIGHT CHECK, FOUND PORTABLE EMERGENCY LIGHT AT FORWARD ENTRY DOOR INOPERATIVE. REPLACED BATTERIES. LIGHT THEN OPERATED NORMALLY. (M)
Part: POWER SUPPLY — DISCHARGED (CABIN)
SEA - DURING LINE CHECK, EXTERIOR OVERWING EMERGENCY LIGHTS WERE FOUND TO REMAIN ON WITH SWITCH TURNED OFF. REPLACED POWER SUPPLY. EMERGENCY LIGHTS THEN OPERATED PROPERLY. (M)
Part: LIGHT — LOW (CABIN)
SEA - DURING LINE CHECK, FOUND PORTABLE EMERGENCY LIGHT TO BE VERY DIM. REPLACED PORTABLE LIGHT ASSEMBLY. OPS TESTED OK. (M)
Part: WIRE — DAMAGED (CABIN)
ANC - DURING LINE CHECK, FOUND INOPERATIVE EMERGENCY TRACK LIGHT IN CABIN. REPAIRED DAMAGED WIRE AND RECONNECTED. LIGHTS THEN OPERATED PROPERLY. (M)
Part: O-RING — LEAKING (APU)
PDX - FOUND OIL ODOR IN CABIN DURING FLIGHT. REPLACED LEAKING O-RING FOR APU OIL CLUSTER. OP CHECKED OK. (M)
2001
Part: BATTERY PACK — DISCHARGED (CABIN)
SEA - DURING LINE CHECK, EXTERIOR OVERWING EMERGENCY EXIT LIGHTS WERE DETERMINED TO BE INOPERATIVE. REPLACED ASSOCIATED BATTERY PACK (POWER SUPPLY). LIGHTS THEN OPERATED PROPERLY. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
SEA - DURING LINE CHECK, MID CABIN OVERHEAD EMERGENCY LIGHTS NEAR OVERWING EXITS WERE DETERMINED TO BE INOPERATIVE. REMOVED AND REPLACED ASSOCIATED BATTERY PACK. LIGHTS THEN OPERATED NORMALLY. (M)
Part: LIGHT — INOPERATIVE (CABIN)
SEA - DURING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS AT AFT END OF 1ST CLASS CABIN INOPERATIVE. REPLAED LIGHT JUMPER (CONNECTOR). LIGHTS THEN OPERATED PROPERLY. (M)
2000
Part: HINGE — LACK OF LUBE (PAX DOOR)
LAX PRIOR TO FLIGHT 277 THE L1 DOOR WAS FOUND TO BE DIFFICULT TO OPEN WITH NOISE IN THE HINGE AREA. LUBRICATED THE HINGE POINTS AND THE DOOR OPERATED NORMALLY.
Part: WEB — CORRODED (FUSELAGE)
PHX - DURING SCHEDULED 30K CHECK, THE CUSP WEB AT STATION 1153 TO 1174, WAS FOUND TO BE CORRODED. REPAIRED PER SRM. (M)
Part: BATTERY — DISCHARGED (COCKPIT)
LAX - PRIOR TO FLIGHT 481, THE EMERGENCY LIGHTS IN THE FLIGHT DECK WOULD NOT TEST. REPLACED BATTERY AND LIGHTS OPERATED NORMALLY. (M)
Part: POWER SUPPLY — DISCHARGED (FWD CABIN)
SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS AT ROWS 5-9 WERE FOUND TO BE INOPERATIVE. REPLACED THE POWER SUPPLY AND THE LIGHTS OPERATED NORMALLY. (M)
Part: LONGERON — CORRODED (FUSELAGE)
PHX - DURING SCHEDULED 30K CHECK, THE AFT CARGO COMPARTMENT STATION 1255, LONGERON 28R, WAS FOUND TO BE CORRODED. REPAIRED PER SRM. (M)
Part: FRAME — CORRODED (FUSELAGE)
PHX-DURING SCHEDULED 30K CHECK THE AFT CARGO COMPARTMENT FRAME AT STA 1250, LONG 26R, CAP STIFFENER WAS FOUND TO BE CORRODED. REPAIRED PER SRM.
Part: WEB — CORRODED (FUSELAGE)
PHX-DURING SCHEDULED 30K CHECK THE AFT CARGO COMPARTMENT LOWER DOOR WEB STA 1155 TO 1212, LONG 26R TO 29R, WAS FOUND TO BE CORRODED.REPAIRED PER SRM.
Part: WEB — CORRODED (FUSELAGE)
PHX - DURING SCHEDULED 30K CHECK, THE CUSP WEB AT STATION 598 TO 677, LONGERON 18L, WAS FOUND TO BE CORRODED. REPAIRED PER SRM. (M)
Part: SHEAR TIE — CORRODED (FUSELAGE)
PHX-DURING SCHEDULED 30K CHECK THE AFT CARGO COMPARTMENT STUB FRAME SHEAR TIE AT STA 1212, LONG 29L TO 29R WAS FOUND TO BE CORRODED.REPAIRED PER SRM.
Part: WEB — CORRODED (FUSELAGE)
PHX - DURING SCHEDULED 30K CHECK, THE RIGHT CUSP CHORD AT STATION 225, RBL 58, WAS FOUND TO BE CORRODED. REPAIRED PER SRM. (M)
Part: SHEAR TIE — CORRODED (FUSELAGE)
PHX - DURING SCHEDULED 30K CHECK, THE SHEAR TIE AT STATION 1155, LONGERON 29L TO 29R, WAS FOUND TO BE CORRODED. REPAIRED PER SRM. (M)
Part: SPLICE — CORRODED (FUSELAGE)
PHX-DURING SCHEDULED 30K CHECK THE AFT CARGO COMPARTMENT LONGERON 30 SPLICE AT STA 1212 WAS FOUND TO BE CORRODED WHERE THE FRAME BUTTS TO THE SPLICE.REPAIRED PER SRM.
Part: BATTERY — DISCHARGED (FWD CABIN)
PHX - DURING SCHEDULED 30K CHECK, THE OVERHEAD EMERGENCY LIGHTS AT ROWS 1-10 WERE FOUND TO BE INOPERATIVE. REPLACED THE BATTERIES AND THE LIGHTS OPERATED NORMALLY. (M)
Part: LONGERON — CORRODED (FUSELAGE)
PHX-DURING SCHEDULED 30K CHECK THE AFT CARGO COMPARTMENT AT STA 1200, LONGERON 29L WAS FOUND TO BE CORRODED. REPAIRED PER SRM.
Part: SHEAR TIE — CORRODED (FUSELAGE)
PHX-DURING SCHEDULED 30K CHECK THE SHEAR TIE AT STA 810 AFT LEG BETWEEN LONG 29R AND 30R WAS FOUND TO BE CORRODED. REPAIRED PER SRM.
Part: SHEAR TIE — CORRODED (FUSELAGE)
PHX - DURING SCHEDULED 30K CHECK, THE SHEAR TIE AT STATION 1174, LONGERON 29L TO 29R, WAS FOUND TO BE CORRODED. REPAIRED PER SRM. (M)
Part: FLOOR SUPPORT — CRACKED (FUSELAGE)
PHX-DURING SCHEDULED 30K CHECK STA. 148, LBL 7, SUBFLOOR SUPPORT WAS FOUND TO BE CRACKED. REPAIRED PER SRM.
Part: CARGO TRACK — CORRODED (FUSELAGE)
PHX-DURING SCHEDULED 30K CHECK THE CENTER CARGO COMPARTMENT CARGO TRACK AT STA 786, LBL 18, WAS FOUND TO BE CORRODED.REPAIRED PER SRM.
Part: SKIN — DAMAGED (FUSELAGE)
PHX-DURING SCHEDULED 30K CHECK THE L/H FUSELAGE STA 309-332 JUST BELOW LONG 22L WAS FOUND TO BE CREASED.REPAIRED PER EA 5330-01456.
Part: INTERCOSTAL — CORRODED (FUSELAGE)
PHX - DURING SCHEDULED 30K CHECK, THE AFT CARGO COMPARTMENT INTERCOSTAL AT STATION 1309 TO STATION 1322 BETWEEN LONGERON 28R AND 27R WAS FOUND TO BE CORRODED. REPAIRED PER SRM. (M)
Part: SKIN — CRACKED (FUSELAGE)
PHX-DURING SCHEDULED 30K CHECK THE NOSE LANDING GEAR WHEEL WELL OPENING LT FORWARD CORNER STA 47-83, LBL 24, WAS FOUND TO BE CRACKED.REPAIRED PER SRM.
Part: CARGO TRACK — CORRODED (FUSELAGE)
PHX-DURING SCHEDULED 30K CHECK THE CENTER CARGO COMPARTMENT CARGO TRACK AT STA 782, RBL 18, WAS FOUND TO BE CORRODED. REPAIRED PER SRM.
Part: SEAT TRACK — CORRODED (CABIN)
PHX - DURING SCHEDULED 30K CHECK, THE SEAT TRACK STATION 1155 TO 1174, LBL 44 WAS FOUND TO BE CORRODED. REPAIRED PER SRM. (M)
Part: FLOOR SUPPORT — CORRODED (FUSELAGE)
PHX-DURING SCHEDULED 30K CHECK THE FLOOR TRACK SECTION AT STA 1117-1136, LBL16, WAS FOUND TO BE CORRODED.REPAIRED PER SRM.
Part: SEAT TRACK — CORRODED (FUSELAGE)
PHX-DURING SCHEDULED 30K CHECK THE SEAT TRACK AT STA 200 TO STA 795, RBL24, WAS FOUND TO BE CORRODED.REPAIRED PER SRM.
Part: WEB — CORRODED (FUSELAGE)
PHX - DURING SCHEDULED 30K CHECK, THE RIGHT CUSP WEB STATION 1155-1174, RBL 58, WAS FOUND TO BE CORRODED. REPAIRED PER SRM. (M)
Part: FLOOR SUPPORT — CRACKED (FUSELAGE)
PHX-DURING SCHEDULED 30K CHECK THE MAIN CABIN FORWARD SUBFLOOR AT STA 164, LBL 54 WAS FOUND TO BE CRACKED. REPAIRED PER SRM.
Part: WEB — CORRODED (FUSELAGE)
PHX - DURING SCHEDULED 30K CHECK, THE MAIN CABIN SUB FLOOR STATION 200, BL 0 WAS FOUND TO BE CORRODED. REPAIRED PER SRM. (M)
Part: STRUCTURE — CORRODED (FUSELAGE)
PHX-DURING SCHEDULED 30K CHECK THE AFT CARGO COMPARTMENT STA 1200, LONGERON 30, BOTTOM SIDE OF HORIZONTAL LEG AT THE FASTENER WAS FOUND TO BE CORRODED.REPAIRED PER SRM.
Part: SKIN — DENTED (FUSELAGE)
PHX-DURING SCHEDULED 30K CHECK THE SKIN AT STA 1273 LONG 28R WAS FOUND TO BE DENTED. REPAIRED PER SRM.
Part: WEB — CORRODED (FUSELAGE)
PHX - DURING SCHEDULED 30K CHECK, THE CUSP WEB AT STATION 1195, LONGERON 18L, WAS FOUND TO BE CORRODED. REPAIRED PER SRM. (M)
Part: WEB — CORRODED (FUSELAGE)
PHX - DURING SCHEDULED 30K CHECK, THE RIGHT CUSP WEB AT STATINO 218 TO 237, LONGERON 18R, WAS FUOND TO BE CORRODED. REPAIRED PER SRM. (M)
Part: WEB — CORRODED (FUSELAGE)
PHX - DURING SCHEDULED 30K CHECK, THE RIGHT CUSP WEB STATION 237 TO 256, LONGERON 18R, WAS FOUND TO BE CORRODED. REPAIRED PER SRM. (M)
Part: SUPPORT — CORRODED (FUSELAGE)
PHX - DURING SCHEDULED 30K CHECK, THE LAV SUPPORT AT STATION 230, LBL 20 WAS FOUND TO BE CORRODED. REPAIRED PER SRM. (M)
Part: SKIN — CRACKED (FUSELAGE)
PHX-DURING SCHEDULED 30K CHECK THE NOSE LANDING GEAR WHEEL WELL OPENING RT FORWARD CORNER STA 47-83 RBL 24, WAS FOUND TO BE CRACKED.REPAIRED PER SRM.
Part: WEB — CORRODED (FUSELAGE)
PHX - DURING SCHEDULED 30K CHECK, THE CUSP WEB AT STATION 503 TO 598, LONGERON 18L, WAS FOUND TO BE CORRODED. REPAIRED PER SRM. (M)
Part: FITTING — CORRODED (FUSELAGE)
PHX - DURING SCHEDULED 30K CHECK, THE LONGERON FITTING AT STATION 826, LONGERON 30 WAS FOUND TO BE CORRODED. REPAIRED PER SRM. (M)
Part: WEB — CORRODED (FUSELAGE)
PHX-DURING SCHEDULED 30K CHECK THE CUSP WEB AT STA 503, STR 18L, WAS FOUND TO BE CORRODED.REPAIRED PER SRM.
Part: CARGO TRACK — CORRODED (FUSELAGE)
PHX-DURING SCHEDULED 30K CHECK THE AFT CARGO COMPARTMENT TRACK AT STA 1212 TO 1309, LONG 28R WAS FOUND TO BE CORRODED. REPAIRED PER SRM.
Part: FRAME — CORRODED (FUSELAGE)
PHX-DURING SCHEDULED 30K CHECK THE AFT CARGO COMPARTMENT STUB FRAME INNER DOOR BEAM AT STA 1218, LONG 29R, WAS FOUND TO BE CORRODED.REPAIRED PER SRM.
Part: WEB — CORRODED (FUSELAGE)
PHX - DURING SCHEDULED 30K CHECK, THE RIGHT CUSP MEMBER STATION 503 TO 522, LONGERON 18R, WAS FOUND TO BE CORRODED. REPAIRED PER SRM. (M)
Part: BATTERY — DISCHARGED (FWD CABIN)
PHX - DURING SCHEDULED 30K CHECK, THE FORWARD ENTRY EMERGENCY EXIT LIGHT WAS FOUND TO HAVE A SHORT TIME SPAN. REPLACED BATTERY AND LIGHT OPERATED NORMALLY. (M)
Part: SKIN — CORRODED (FUSELAGE)
PHX-DURING SCHEDULED 30K CHECK THE LT SIDE FORWARD FUSELAGE AT STA 228, JUST BELOW THE CUSP AT LONG 18L WAS FOUND TO BE BULGED.
Part: WEB — CRACKED (FUSELAGE)
PHX-DURING SCHEDULED 30K CHECK THE RT CUSP WEB AT STA 218 TO 237, RBL 48 WAS FOUND TO HAVE LIGHTNING HOLE CRACKS. REPAIRED PER SRM.
Part: BATTERY PACK — DISCHARGED (MID CABIN)
PHX - DURING SCHEDULED 30K CHECK, THE LEFT AND RIGHT FUSELAGE OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED THE RELAY R2-271 AND BATTERY PACK, THE LIGHTS OPERATED NORMALLY. (M)
Part: BATTERY — DISCHARGED (DOOR SLIDE)
PHX - DURING SCHEDULED 30K CHECK, THE AFT SERVICE DOOR SLIDE AMP MEASUREMENT WAS FOUND TO BE OUT OF TOLERANCE. REPLACED SLIDE. (M)
Part: WEB — CORRODED (FUSELAGE)
PHX-DURING SCHEDULED 30K CHECK THE CUSP WEB MEMBRANE AT STA 200, FROM LBL 45 TO LBL 58, WAS FOUND TO HAVE CORROSION. REPAIRED PER SRM.
Part: FRAME — CORRODED (FUSELAGE)
PHX-DURING SCHEDULED 30K CHECK THE AFT CARGO COMPARTMENT FRAME AT STA 1255, LONG 26L TO 26R, WAS FOUND TO BE CORRODED. REPAIRED PER SRM.
Part: SEAT TRACK — CORRODED (FUSELAGE)
PHX-DURING SCHEDULED 30K CHECK THE SEAT TRACK AT STA 1030 TO 1290, LBL 24, WAS FOUND TO BE CORRODED.REPAIRED PER SRM.
Part: WEB — CORRODED (FUSELAGE)
PHX-DURING SCHEDULED 30K CHECK THE CUSP WEB AT STA 489 TO 503, LONG 18L, WAS FOUND TO BE CORRODED.REPAIRED PER SRM.
Part: WEB — CANNING (FUSELAGE)
PHX-DURING SCHEDULED 30K CHECK THE FORWARD ENTRY WAY CUSP MEMBRANE AT STA 185, RBL24, WAS FOUND TO BE OIL CANNED APPROX. 2 INCH IN DIAMETER.REPAIRED PER SRM.
Part: WEB — CRACKED (FUSELAGE)
PHX-DURING SCHEDULED 30K CHECK THE FORWARD FLOOR WEB AT STA 148-160 RBL WAS FOUND TO BE CRACKED.REPAIRED PER SRM.
Part: CARGO TRACK — CORRODED (FUSELAGE)
PHX-DURING SCHEDULED 30K CHECK THE AFT CARGO COMPARTMENT FLOOR TRACK CHANNEL AT STA 1079 TO 1155, RBL 20, WAS FOUND TO BE CORRODED.REPAIRED PER SRM.
Part: CARGO TRACK — CORRODED (FUSELAGE)
PHX-DURING SCHEDULED 30K CHECK THE AFT CARGO COMPARTMENT TRACK SECTION AT STA 1250, LONG 27L, WAS FOUND TO BE CORRODED. REPAIRED PER SRM.
Part: LIGHT — INOPERATIVE (FWD CABIN)
PHX - DURING SCHEDULED 30K CHECK, THE L1 DOOR PORTABLE EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED PORTABLE LIGHT AND LIGHT OPERATED NORMALLY. (M)
Part: SKIN — DENTED (FUSELAGE)
PHX-DURING SCHEDULED 30K CHECK THE LT FUSELAGE STA 256 ABOVE LONG 18L WAS FOUND TO BE DENTED.REPAIRED PER SRM.
Part: RELAY — FAILED (CABIN)
PHX - DURING SCHEDULED 30K CHECK, THE LEFT AND RIGHT FUSELAGE OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED THE RELAY R2-271 AND BATTERY PACK, THE LIGHTS OPERATED NORMALLY. (M)
Part: WEB — CORRODED (FUSELAGE)
PHX - DURING SCHEDULED 30K CHECK, THE CUSP WEB MEMBRANE AT STATION 446 TO 465, LONGERON 18L, WAS FOUND TO BE CORRODED. REPAIRED PER SRM. (M)
Part: WEB — CORRODED (FUSELAGE)
PHX - DURING SCHEDULED 30K CHECK, THE RIGHT CUSP WEB AT STATION 1195 TO STATION 1212 WAS FOUND TO BE CORRODED. REPAIRED PER SRM. (M)
Part: BEAM — CORRODED (CARGO BAY)
PHX - DURING SCHEDULED 30K CHECK, THE MID CARGO COMPARTMENT LOWER DOOR BEAM AT STATION 636-693, LONGERON 27R, WAS FOUND TO BE CORRODED. REPAIRED PER SRM. (M)
Part: ATTACH FITTING — CORRODED (FUSELAGE)
PHX - DURING SCHEDULED 30K CHECK, THE AFT CARGO COMPARTMENT FRAME ATTACH FITTING AT STATION 1219, LONGERON 28R WAS FOUND TO BE CORRODED. (M)
1999
Part: LANYARD — DISCONNECTED (TAILCONE)
PDX - DURING MAINTENANCE CHECK, THE TAILCONE RELEASE LANYARD WAS FOUND DISCONNECTED FROM THE RETAINER PIN. RECONNECTED LANYARD TO RELEASE MECHANISM RETAINER PIN. (M)
Part: MODULE — DEFECTIVE (ROW 27-28)
PDX - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 27 TO 28 WERE FOUND INOPERATIVE. REPLACED LAMP MODULE AND OPERATED NORMALLY. (M)
Part: WIRE — DISCONNECTED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE FORWARD RED EMERGENCY FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED WIRING IN FLOOR TRACK AT ROW 1 AND OPERATED NORMALLY. (M)
Part: HINGE PIN — DAMAGED (COCKPIT WINDOW)
SEA - AFTER ARRIVAL OF FLIGHT 472, CREW REPORTED THE FLIGHT COMPARTMENT LEFT SLIDING WINDOW WOULD NOT OPEN. FOUND WINDOW AFT HINGE PIN MIGRATING OUT, REINSTALLED HINGE PIN AND OPERATED NORMALLY. (M)
Part: POWER SUPPLY — INOPERATIVE (CABIN)
SEA - DURING MAINTENANCE CHECK, THE EXTERIOR OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. REPLACED THE POWER SUPPLY AND OPERATED NORMALLY. (M)
1998
Part: DOOR HANDLE — MALFUNCTIONED (GALLEY DOOR)
SEA - AFTER ARRIVAL OF FLIGHT 545, CREW REPORTED THE L2 DOOR HANDLE WAS DIFFICULT TO OPERATE. ADJUSTED AND LUBRICATED THE L2 DOOR HANDLE OPERATING MECHANISM AND OPERATED NORMALLY. (M)
Part: LIGHT — INOPERATIVE (CABIN)
SEA - AFTER ARRIVAL OF FLT 531 - CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. RECONNECTED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (M)
Part: LIGHT — INOPERATIVE (FWD CABIN)
SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 1 TO 3 WERE FOUND INOPERATIVE. REPAIRED WIRING IN THE FLOOR TRACK AND OPERATED NORMALLY. (M)
Part: POWER SUPPLY — INOPERATIVE (CABIN)
SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE FORWARD ENTRY WERE FOUND INOPERATIVE. REPLACED THE POWER SUPPLY AND OPERATED NORMALLY. (M)
Part: BULB — DEFECTIVE (CABIN)
PDX - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE FWD CABIN WERE FOUND INOPERATIVE. REPLACED DEFECTIVE LAMP MODULE AND OPERATED NORMALLY. (M)
Part: WIRE — DISCONNECTED (CABIN)
PDX - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE FWD CABIN WERE FOUND INOPERATIVE. RECONNECTED WIRE IN FLOOR TRACK AND OPERATED NORMALLY. (M)
Part: WIRE — DEFECTIVE (CABIN)
SEA - PRIOR TO DEPARTURE FO FLT 722, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. REPAIRED WIRE IN FLOOR TRACK AND OPERATED NORMALLY. (M)
Part: CONNECTOR — LOOSE (CABIN)
SMF - PRIOR TO DEPARTURE OF FLT 409 - CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS FROM ROW 2 FORWARD AND ROWS 25 TO 29 WERE INOPERATIVE. SECURED LOOSE CONNECTORS AT ROW 2 AND ROW 25 AND OPERATED NORMALLY. (M)
1997
Part: LIGHT — INOPERATIVE (TAILCONE)
SEA - DURING MAINTENANCE CHECK, TWO TAILCONE EMERGENCY LIGHTS WERE FOUND INOPERATIVE. REPLACED AFT MOST CATWALK ILLUMINATION LIGHT ASSEMBLY AND OPERATED NORMALLY. (M)
Part: HARNESS — FAILED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE THREE FORWARD EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. REPLACED HARNESS AT THIRD TRACK LIGHT AND LIGHTS OPERATED NORMALLY. (M)
Part: CONNECTOR — LOOSE (CABIN)
SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY EXIT IDENTIFIER AT ROW 24 WAS INOPERATIVE. TIGHTENED LOOSE TERMINAL ON LIGHT SOCKET AND OPERATED NORMALLY. (M)
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 5730-01046. (M)
Part: LANYARD — DISCONNECTED (TAILCONE)
SEA - DURING INSPECTION OF THE TAILCONE EMERGENCY EVACUATION SLIDE THE AUTOMATIC DEPLOY LANYARD WAS FOUND DISCONNECTED FROM THE GIRT TAB. CONNECTED THE AUTOMATIC DEPLOY LANYARD TO THE GIRT TAB. (M)
1996
Part: DOOR JAMB — CORRODED (BS 1212)
OAK - DURNG 15K CHECK, CORROSION WAS FOUND ON THE AFT CARGO COMPARTMENT DOOR JAMB TORQUE BOX WEB AT Y1212. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM AND ASA EA 5310-01498. (M)
Part: BATTERIES — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, AFT SECTION OF EMERGENCY EXIT TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. REPAIRED SECTION OF WIRING AND REPLACED BATTERIES IN POWER PACK. LIGHTS OPERATED NORMALLY. (M)
Part: WIRE — DISCONNECTED (CABIN)
SEA - DURING MAINTENANCE CHECK, AFT SECTION OF EMERGENCY EXIT TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. REPAIRED SECTION OF WIRING AND REPLACED BATTERIES IN POWER PACK. LIGHTS OPERATED NORMALLY. REFERENCE ASAA9680090.
1995
Part: EEL PORTABLE — DEFECTIVE (CABIN)
LAX - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND DIM. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (W)
Part: COMPRESSOR — FOD DAMAGE (NR 2 ENGINE)
SEA - NR 2 ENGINE HAD COMPRESSOR STALL DURING TAKEOFF ROLL. MAINTENANCE FOUND FOD DAMAGE TO C1 BLADES. REPLACED ENGINE. (Z)