N982AS
Registered owner: ABOVE STANDARD FLYING SERVICE LLC, LA (owner ≠ operator)
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.
107 reports on file, 1997-08-29 – 2007-12-18.
Part: SKIN — DENTED (FUSELAGE) · airframe 35,856 hrs · 18,160 cycles
FUSELAGE SKIN DENTED BY JETWAY. REPLACED DAMAGED SECTION OF SKIN. INSTALLED REPAIR DOUBLER PER SRM 53-04-12B.
Part: SKIN — DENTED (BS 235 S17-18L) · airframe 35,644 hrs · 18,052 cycles
TWO DENTS ON FUSELAGE SKIN AT STA 235 BETWEEN LEFT L 17 & 18. REPLACED FORMER & REPAIRED SKIN PER SRM 53-04 FIG 12B & EA 5330 02266.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,829 hrs · 17,631 cycles
OVERWING EMERGENCY EXIT LIGHT INOPERATIVE DURING TEST. REPLACED POWER SUPPLY.
Earlier reports · 1997–2006 · 104 reports
2006
Part: CUSP WEB — CORRODED (BS 1174-1212) · airframe 32,377 hrs · 16,466 cycles
CABIN FLOOR CUSP WEB IS CORRODED. REPLACED TWO DAMAGED AREAS OF WEB AND INSTALLED TWO REPAIR DOUBLERS PER SRM 51-70-4.
Part: FLOOR PANEL — DELAMINATED (BS 807-826) · airframe 32,377 hrs · 16,466 cycles
CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-05 DWG 9939195 AND MM 53-20-01.
2005
Part: SKIN — LIGHTNING STRIKE (FS 754-755)
OKC - DURING HV-CHECK, FOUND FUSELAGE HAS LIGHTNING DAMAGE. REMOVED DAMAGED SECTION. INSTALLED INTERNAL REPAIR DOUBLER. (M)
Part: SEAT TRACK — CORRODED (FS 200-256)
OKC - DURING HV CHECK, PAX CABIN SEAT TRACK IS CORRODED. REPLACED DAMAGED SECTION. INSTALLED PLUG AND CHANNEL. (M)
Part: SEAT TRACK — CORRODED (FS 200-256)
OKC - DURING HV CHECK, FOUND PAX CABIN SEAT TRACK IS CORRODED. REPLACED DAMAGED SECTION. INSTALLED PLUG AND CHANNEL. (M)
Part: SKIN — DETERIORATED (ELEVATOR)
OKC - DURING HV-CHECK, RIGHT ELEVATOR GEARED TAB INBOARD TRAILING EDGE SKIN IS DETERIORATED. SMOOTHED DETERIORATED AREA AND INSTALLED REPAIR DOUBLER. (M)
Part: TAB — DELAMINATED (RT ELEVATOR)
OKC - DURING HV-CHECK, FOUND RIGHT ELEVATOR GEARED TAB IS DELAMINATED ON LOWER SURFACE AT TRAILING EDGE. REMOVED DAMAGED SECTION. INSTALLED SKIN REPAIR FILLER AND DOUBLER. (M)
Part: WEDGE — CRACKED (TE FLAPS)
OKC - DURING HV-CHECK, FOUND RIGHT INBOARD FLAP INBOARD WEDGE TRAILING EDGE IS CRACKED. REMOVED DAMAGED SECTION. INSTALLED VACUUM CURED SPLICE. (M)
Part: INTERCOSTAL — CORRODED (FS 1212-1231)
OKC - DURING HV CHECK, FOUND INTERCOSTAL CORRODED. REPLACED INTERCOSTAL. (M)
Part: FLOOR PANEL — DELAMINATED (FS 196-256)
OKC - DURING HV CHECK, PAX CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL. (M)
Part: FLOOR PANEL — DELAMINATED (CABIN)
OKC - FOUND HV-CHECK, PASSENGER CABIN FLOOR PANEL IS DELAMINATED. REPLACED PANEL. (M)
Part: FRAME — CORRODED (FS 180)
OKC - DURING HV-CHECK, FOUND FRAME CORRODED. REMOVED DAMAGED SECTION. INSTALLED REPAIR FILLER, TWO REPAIR ANGLES AND TWO REPAIR PLATES. (M)
Part: CUSP WEB — CORRODED (FS 927-946)
OKC - FOUND HV CHECK, CUSP WEB CORRODED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER. (M)
Part: CHANNEL — CRACKED (FUSELAGE)
OKC - FOUND HV-CHECK, PASSENGER CABIN FLOOR PANEL HAS CRACKED HAT CHANNEL. REPLACED DAMAGED CHANNEL. (M)
Part: FLOOR PANEL — DELAMINATED (FS 864-886)
OKC - DURING HV-CHECK, FOUND PAX CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL. (M)
Part: ANGLE — CRACKED (FS 1479-1480)
OKC - DURING HV CHECK, FOUND VERTICAL STABILIZER TO FUSELAGE LEFT ATTACH ANGLE IS CRACKED. REMOVED DAMAGED SECTION. INSTALLED SKIN FILLER AND REPAIR ANGLE. (M)
Part: FLOOR PANEL — DELAMINATED (FS 886-927)
OKC - FOUND HV-CHECK, FOUND PAX CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL. (M)
Part: FLOOR PANEL — DELAMINATED (FS 160-200)
OKC - FOUND HV CHECK, PAX CABIN FLOOR PANEL HAS CORRODED INSERTS WITH DELAMINATION AROUND INSERTS. REPLACED FLOOR PANEL. (M)
Part: CUSP WEB — CORRODED (FS 522-541)
OKC - DURING HV CHECK, FOUND CUSP WEB CORRODED. REMOVED DAMAGED SECTION. INSTALLED REPAIR FILLER AND DOUBLER. (M)
Part: SHEAR TIE — CORRODED (FS 1231)
OKC - DURING HV-CHECK, FOUND SHEAR TIE CORRODED. REMOVED DAMGAED SECTION. INSTALLED REPLACEMENT SECTION WITH TWO REPAIR SPLICES. (M)
Part: FLOOR PANEL — DELAMINATED (FS 807-826)
OKC - DURING HV-CHECK, PASSENGER CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL. (M)
Part: WEB — CORRODED (FS 180-200)
OKC - DURING HV CHECK, FOUND PAX CABIN FLOOR WEB CORRODED. REPLACED DAMAGED SECTION. INSTALLED WEB REPAIR AND TWO DOUBLERS. (M)
Part: SKIN — DENTED (FS 291-293)
OKC - DURING HV CHECK, FOUND DENT IN FUSELAGE. COLD-FORMED SKIN TO ORIGINAL CONTOUR. INSTALLED INTERNAL REPAIR DOUBLER. (M)
Part: FLOOR PANEL — DELAMINATED (FS 826-864)
OKC - DURING HV C-CHECK, FOUND PAX CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL. (M)
Part: TAB — DELAMINATED (ELEVATOR)
OKC - FOUND DURING HV-CHECK, RIGHT ELEVATOR GEAR TAB UPPER SURFACE HAS DELAMINATION. REMOVED DAMAGED SECTION. INSTALLED SKIN FILLER AND REPAIR DOUBLER. (M)
Part: FLOOR SUPPORT — CORRODED (FS 160-200)
OKC - DURING HV CHECK, FOUND PAX CABIN FLOOR TRACK CORRODED. REPLACED TRACK. (M)
Part: SHEAR TIE — CORRODED (FS 1287)
OKC - DURING HV CHECK, FOUND SHEAR TIE CORRODED. REMOVED DAMAGED SECTION. INSTALLED REPLACEMENT SECTION WITH TWO REPAIR SPLICES. (M)
Part: FLOOR PANEL — DELAMINATED (FS 160-200)
OKC - DURING HV CHECK, FOUND PAX CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL. (M)
Part: INTERCOSTAL — CORRODED (FS 522-541)
OKC - DURING HV-CHECK, FOUND INTERCOSTAL CORRODED. REPLACED INTERCOSTAL. (M)
Part: FLOOR PANEL — CORRODED (FS 200-256)
OKC - DURING HV-CHECK, PAX CABIN FLOOR PANEL HAS CORRODED INSERTS WITH DELAMINATION AROUND INSERTS. REPLACED FLOOR PANEL. (M)
Part: INTERCOSTAL — CORRODED (FS 522-541)
OKC - FOUND DURING HV-CHECK, INTERCOSTAL CORRODED. REPLACED INTERCOSTAL. (M)
Part: FLOOR SUPPORT — CORRODED (FS 160-200)
OKC - DURING HV CHECK, PAX CABIN FLOOR TRACK CORRODED. REPLACED TRACK. (M)
Part: FLOOR PANEL — DELAMINATED (FS 160-180)
OKC - DURING HV-CHECK, FOUND PAX CABIN FLOOR PANEL HAS CORRODED INSERTS WITH DELAMINATION AROUND INSERTS. REPLACED FLOOR PANEL. (M)
Part: FLOOR PANEL — CORRODED (CABIN)
OKC - DURING HV CHECK, FOUND PAX CABIN FLOOR PANEL HAS CORRODED INSERTS WITH DELAMINATION AROUND INSERTS. REPLACED FLOOR PANEL. (M)
Part: FLOOR PANEL — DELAMINATED (FS 807-826)
OKC - DURING HV-CHECK, FOUND PAX CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL. (M)
Part: FRAME — CORRODED (FUSELAGE)
OKC - DURING HV-CHECK, FOUND FRAME CORRODED. REMOVED DAMAGED SECTION. INSTALLED TWO REPAIR DOUBLERS, TWO REPAIR PLATES, AND ONE REPAIR FILLER. (M)
Part: SHEAR TIE — CORRODED (FS 1250)
OKC - DURING HV CHECK, FOUND SHEAR TIE CORRODED. REMOVED DAMAGED SECTION. INSTALLED REPLACEMENT SECTION WITH TWO REPAIR SPLICES. (M)
Part: SHEAR TIE — CORRODED (FS 1136-1155)
OKC - DURING HV-CHECK, FOUND SHEAR TIE CORRODED. REPLACED SHEAR TIE. (M)
Part: PANEL — GOUGED (SPOILER)
OKC - DURING HV-CHECK, LEFT INBOARD SPOILER PANEL GOUGED ON UPPER SURFACE AT TRAILING EDGE. REPLACED DAMAGED PLIES. (M)
Part: SKIN — LIGHTNING STRIKE (FS 1237-1238)
OKC - DURING HV-CHECK, FOUND FUSELAGE HAS LIGHTNING DAMAGE. REMOVED DAMAGED SECTION. INSTALLED REPAIR FILLER AND INTERNAL DOUBLER. (M)
Part: DOUBLER — CORRODED (FS 1212-1231)
OKC - DURING HV-CHECK, FOUND ANTENNA DOUBLER CORRODED IN AFT CARGO BAY. REPLACED DOUBLER. (M)
Part: FLOOR PANEL — DELAMINATED (FS 886-927)
OKC - FOUND HV-CHECK, PAX CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL. (M)
Part: FLOOR PANEL — DELAMINATED (FS 180-200)
OKC - DURING HV-CHECK, FOUND PAX CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL. (M)
Part: FLOOR PANEL — DELAMINATED (CABIN)
OKC - DURING HV-CHECK, FOUND PAX CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL. (M)
Part: FLOOR PANEL — DELAMINATED (FS 927-1003)
OKC - DURING HV-CHECK, FOUND PAX CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL. (M)
Part: FLOOR PANEL — DELAMINATED (FS 200-256)
OKC - FOUND HV-CHECK, PAX CABIN FLOOR PANEL DELAMINATED. REPLAED FLOOR PANEL. (M)
Part: FLOOR PANEL — DELAMINATED (FS 826-886)
OKC - FOUND HV-CHECK, PAX CABIN FLOOR PANEL IS DELAMINATED. REPLACED PANEL. (M)
Part: TAB — DELAMINATED (ELEVATOR)
OKC - DURING HV CHECK, FOUND RIGHT ELEVATOR ANTI-FLOAT TAB LOWER SURFACE IS DELAMINATED. REMOVED DAMAGED SECTION. INSTALLED SKIN FILLER AND REPAIR DOUBLER. (M)
2004
Part: LANYARD — DISCONNECTED (R1 DOOR) · airframe 26,085 hrs · 13,385 cycles
PRE-FLIGHT CHECK - FWD SERVICE (R-1) DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (K)
Part: POWER SUPPLY — DISCHARGED (OVERWING EXIT) · airframe 25,931 hrs · 13,310 cycles
SERVICE CHECK- EMERGENCY OVERHEAD CABIN LIGHTS INOPERATIVE AT OVERWING EXIT ON BOTH SIDES. REPLACED ASSOCIATED BATTERY PACKS (POWER SUPPLYS). LIGHT THEN OPERATED PROPERLY.(K)
Part: SKIN — CRACKED (FUSELAGE)
C-CHECK- NLG RT DOOR AFT HINGE COUTOUT IS CRACKED. STOP-DRILLED CRACK. INSTALLED REPAIR DOUBLER IAW SRM.
Part: FLOOR PANEL — CRACKED (FLIGHT DECK) · airframe 25,925 hrs · 13,308 cycles
C-CHECK - FLIGHT DECK FLOOR PANEL IS CRACKED. FABRICATED REPLACEMENT FLOOR PANEL IAW SRM.(K)
Part: PAN — GOUGED (CARGO DOOR) · airframe 25,925 hrs · 13,308 cycles
C-CHECK - AFT CARGO DOOR LOWER FRAME AND INNER PAN ARE GOUGED ALONG EDGE ADJACENT TO RUB BLOCK. REMOVED DAMAGED AREA. REPAIRED IAW EA.(K)
Part: DOOR FRAME — CORRODED (FUSELAGE)
OKC - C-CHECK, AFT CARGO DOOR JAMB LOWER WEB IS CORRODED AT STA 1212 TO STA 1231. REMOVED DAMAGED SECTION OF WEB, ORDERED AND INSTALLED NEW WEB, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 51-70-04 AND 51-30-5.
Part: SKIN — DENTED (FUSELAGE)
OKC - C-CHECK, FUSELAGE SKIN, STA 218, BETWEEN LONGERON 18L AND 19L IS DENTED X=.042, D=2.20 WITHIN 1 INCH OF STRUCTURE. COLD WORKED SKIN TO CONTOUR, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-04, FIG 38.
Part: SKIN — GOUGED (FUSELAGE)
OKC - C-CHECK, FUSELAGE SKIN, STA 237, LONGERON 17L HAS GOUGE WITH DENTS LESS THAN 1 INCH FROM STRUCTURE X=.034, D=1.11. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER, DOUBLERS AND STRAPS IAW SRM 53-04, FIG 12C.
Part: SKIN — DENTED (MID CARGO DOOR)
OKC - C-CHECK, MID CARGO DOOR UPPER HAS NUMEROUS DENTS, FWD DENTS, X=.036, D=.800, 13 INCHES AFT OF FORWARD DENT X=.024, D=.800 AND IS OVER PREVIOUS REPAIR. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER AND STRAP DOUBLERS IAW SRM 53-04, FIG 12E.
Part: SKIN — DENTED (AFT CARGO DOOR)
OKC - C-CHECK, AFT PIT DOOR, AFT MID SECTION 3 INCHES FROM EDGE DENTED X=1.10, D=.027, COLD WORKED TO CONTOUR, COMPLIED WITH HFEC. NO DEFECTS NOTED, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-04, FIG 38.
Part: SKIN — DENTED (AFT CARGO DOOR)
OKC - C-CHECK, AFT PIT DOOR FORWARD MID SECTION 12 INCHES FROM TOP IS DENTED D=.920 X=.030. COLD WORKED DENT TO CONTOUR, HFEC COMPLIED WITH, NO DEFECTS NOTED. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-04, FIG 38.
Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT)
DURING PREFLIGHT CHECK, FOUND EMERGENCY TRACK LIGHTS INOPERATIVE AT ROW 3. RECONNECTED WIRE CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M)
Part: WIRE — INOPERATIVE (EMERGENCY LIGHT)
PDX - FOUND TWO EMERGENCY TRACK LIGHT INOPERATIVE IN 1ST CLASS CABIN. RECONNECTED, REPAIRED WIRING, LOOSE CONNECTOR WIRE. LIGHT THEN OPERATED PROPERLY. (M)
2003
Part: LANYARD — DISCONNECTED (R1 DOOR)
PREFLIGHT CHECK, FOUND FORWARD SERVICE R1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (M)
Part: LANYARD — DISCONNECTED (ESCAPE SLIDE)
PREFLIGHT CHECK, FOUND FORWARD SERVICE R-1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (M)
Part: LIGHT — INOPERATIVE (ROW 30)
PDX LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHT WIRING DISCONNECTED AT ROW 30. RECONNECTED WIRING AT ROW 30. LIGHTS THEN OPERATED PROPERLY. (M)
Part: LIGHT — INOPERATIVE (ROW 30)
RNO - PREFLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHT WIRING DISCONNECTED/DAMAGED AT ROW 30. SPLICED WIRING AT ROW 30. LIGHTS THEN OPERATED PROPERLY. (M)
2002
Part: LIGHT — INOPERATIVE (CABIN)
SEA - DURING LINE CHECK, FOUND PORTABLE EMERGENCY LIGHT AT FORWARD ENTRY DOOR INOPERATIVE. REPLACED LIGHT ASSEMBLY, INCLUDING BATTERY PACK. LIGHT THEN OPERATED NORMALLY. (M)
Part: LANYARD — DISCONNECTED (EVAC SLIDE)
SEA - DURING PREFLIGHT CHECK, LANYARD BETWEEN GIRT BAR AND SLIDE COVER WAS FOUND DISCONNECTED. REATTACHED LANYARD. (M)
Part: LIGHT — INOPERATIVE (CABIN)
SEA - DURING LINE CHECK, FOUND PORTABLE EMERGENCY LIGHT AT FORWARD ENTRY DOOR INOPERATIVE. REPLACED LIGHT ASSEMBLY (INCLUDING BATTERY PACK). LIGHT THEN OPERATED NORMALLY. (M)
Part: DOOR FRAME — CORRODED (FUSELAGE)
PAE - DURING C-CHECK, FOUND MID CARGO BAY LOWER DOOR BEAM TO BE CORRODED ON VERTICAL FACE AND LOWER HORIZONTAL LUG. REPAIRED PER EA 5310-02090. (M)
Part: SKIN — BENT (PAX DOOR)
PAE - DURING C-CHECK, FOUND FORWARD PAX ENTRANCE DOOR SKIN BENT ALONG FORWARD BOTTOM EDGE. REPAIRED PER SRM 52-05, FIG 37. (M)
Part: SPACER — CORRODED (FUSELAGE)
PAE - DURING C-CHECK, FOUND CORROSION ON AFT CARGO BAY THRESHOLD SPACER AT FS 1160-1207. REPAIRED PER EO 5300-0101. (M)
Part: LIGHT — OUT OF POSITION (CABIN)
SEA - DURING PREFLIGHT CHECK, FOUND EMERGENCY TRACK LIGHTS INOPERATIVE AT ROWS 6 THROUGH 9. RECONNECTED (REPOSITIONED) LIGHT MODULES. LIGHTS THEN OPERATED PROPERLY. (M)
Part: CONNECTOR — DISCONNECTED (FWD CABIN)
PDX - DURING LINE CHECK, FOUND 5 EMERGENCY TRACK LIGHTS INOPERATIVE, ROWS 6 TO 8. RESECURED ELECTRICAL CONNECTORS. LIGHTS THEN OPERATED PROPERLY. (M)
2001
Part: BATTERY PACK — DISCHARGED (COCKPIT)
SEA - DURING PREFLIGHT CHECK, FOUND COCKPIT OVERHEAD EMERGENCY LIGHTING WAS INOPERATIVE. REPLACED ASSOCIATED BATTERY POWER SUPPLY PACK. LIGHTS THEN OPERATED PROPERLY. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
PDX - DURING LINE CHECK, OVERHEAD EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE BETWEEN ROW 8 AND 17. REPLACED ASSOCIATED BATTERY POWER SUPPLY PACK AT B5-101. LIGHTS THEN OPERATED PROPERLY. (M)
Part: LIGHT — INOPERATIVE (CABIN)
PDX - DURING SERVICE CHECK, THE EMERGENCY CEILING LIGHT AT ROW 17 WAS FOUND TO BE INOPERATIVE. REPLACED THE LAMP ASSEMBLY AT ROW 17. THE LIGHTS OPERATED NORMALLY. (M)
Part: LANYARD — DISCONNECTED (EMERGENCY SLIDE)
ANC - DURING PRE-FLIGHT CHECK, L1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND TO BE DETACHED FROM GIRT BAR. RE-SECURED LANYARD. (M)
Part: GIRT BAR — INOPERATIVE (EMERGENCY SLIDE)
LAX - DURING PRE-FLIGHT CHECK. L-2 DOOR EMERGENCY SLIDE GIRT BAR WAS FOUND TO BE IMPROPERLY INSTALLED. RE-INSTALLED GIRT BAR PROPERLY. (M)
Part: BATTERY — DISCHARGED (CABIN)
PHX - DURING K-CHECK, FOUND LEFT AND RIGHT OVERWING EMERGENCY EXIT OVERHEAD LIGHTS INOPERATIVE. REMOVED AND REPLACED THE TWO BATTERIES IN THE ASSOCIATED BATTERY PACK. LIGHTS THEN OPERATED NORMALLY. (M)
Part: INTERCOSTAL — WORN (FUSELAGE)
PHX - DURING K-CHECK, FOUND WEAR MARK ON OUTER RADIUS OF TRIANGLE INTERCOSTAL AT FS 1385, LBL 48. FABRICATED AND INSTALLED A DOUBLER REPAIR PER SRM 53-01. (M)
Part: INTERCOSTAL — CORRODED (FUSELAGE)
PHX - DURING K-CHECK, FOUND AFT CARGO BAY FRAME TO INTERCOSTAL ANGLE CORRODED AT FS 1155, RBL 3. REMOVED CORRODED ANGLE, FABRICATED AND INSTALLED NEW ANGLE PER ASA DWG 5936071. (M)
Part: DOUBLER — CORRODED (FUSELAGE)
PHX - DURING K-CHECK, FOUND CLAIRCOM (PAX PHONE) ANTENNA MOUNT INTERNAL DOUBLER, LOCATED IN THE AFT CARGO BAY, CORRODED. REMOVED CORRODED DOUBLER. FABRICATED AND INSTALLED A REPLACEMENT DOUBLER PER SRM 51-30-2 AND DWG C23AL-2300. (M)
Part: CARGO TRACK — CORRODED (FUSELAGE)
PHX - DURING K-CHECK, FOUND AFT CARGO BAY CARGO TRACK CORRODED BETWEEN FS 1088 AND 1221, AT BL 15. REMOVED CORRODED TRACK. FABRICATED AND INSTALLED NEW TRACK PER SRM 53-24-0. (M)
Part: CARGO TRACK — CORRODED (CARGO BAY)
PHX - DURING K-CHECK, FOUND AFT CARGO BAY CARGO TRACK AND SPLICES CORRODED AT LBL 15, FS 1221-1322. REMOVED AND REPLACED CARGO TRACK AND SPLICES, REF SRM 51-30-0. (M)
Part: INTERCOSTAL — CORRODED (FUSELAGE)
PHX - DURING K-CHECK, FOUND AFT CARGO BAY INTERCOSTAL AT FS 1149-1155, RBL 3, CORRODED. REMOVED AND REPLACED INTERCOSTAL, REF DWG 5936071. (M)
Part: CARGO TRACK — CORRODED (FUSELAGE)
PHX - DURING K-CHECK, FOUND CORROSION ON RIGHT CARGO TRACK AT FS 1212-1322 IN AFT CARGO BAY. REMOVED AND REPLACED CORRODED CARGO TRACK. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
SJC - DURING PREFLIGHT CHECK, OVERHEAD EMERGENCY LIGHTS BETWEEN ROWS 19 AND 22 REMAINED ILLUMINATED WITH ALL POWER AND SWITCHES OFF. REPLACED ASSOCIATED BATTERY PACKS. LIGHTS THEN OPERATED PROPERLY. (M)
2000
Part: BATTERY PACK — DISCHARGED (AFT CARGO BAY)
SEA - DURING MAINTENANCE CHECK, BOTH EXTERIOR OVERWING EMERGENCY EXIT LIGHTS WERE DETERMINED TO BE INOPERATIVE. REPLACED BOTH BATTERY PACKS. LIGHTS THEN OPERATED NORMALLY. (M)
Part: LANYARD — DISCONNECTED (PAX DOOR SLIDE)
SEA PRIOR TO FLIGHT 571 THE L1 DOOR SLIDE LANYARD WAS FOUND TO BE DETACHED. RECLIPPED THE L1 DOOR LANYARD.
Part: BATTERY PACK — DISCHARGED (AFT CABIN)
SEA - DURING MAINTENANCE CHECK, THE AFT CABIN AND TAILCONE EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED THE BATTERY PACK AND THE LIGHTS OPERATED NORMALLY. (M)
Part: WIRE — BROKEN (CABIN)
ANC - PRIOR TO DEPARTURE OF FLIGHT 190, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHT WIRES AT ROW 24 WERE EXPOSED. REPAIRED BROKEN WIRE IN FLOOR TRACK AT ROW 24 AND OPERTED NORMALLY. (M)
Part: BATTERY — DISCHARGED (ROW 22)
OAK - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE MID AND AFT CABIN WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLYS AT ROW 22 FORWARD, ROW 22 AFT, AND ROW 24 AND OPERATED NORMALLY. (M)
Part: BATTERY — INOPERATIVE (CABIN)
OAK - DURING MAINTENANCE CHECK, THE AFT OVERWING EMERGENCY EXIT IDENTIFIERS WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POER SUPPLY AND OPERATED NORMALLY. (M)
Part: BATTERY — DISCHARGED (CABIN)
OAK - DURING MAINTENANCE CHECK, THE EMERGENCY LIGHTS IN THE AFT CATWALK AREA, THE AFT CABIN ENTRY DOOR EMERGENCY EXIT IDENTIFER, THE L2 DOOR EMERGENCY EXIT IDENTIFER, AND THE EMERGENCY FLOOR TRACK LIGHTS IN THE AFT CABIN WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWR SUPPLY AND OPERATED NORMALLY. (M)
Part: BATTERY — DISCHARGED (CABIN)
OAK - DURING MAINTENANCE CHECK, THE AFT OVERWING EMERGENCY EXIT IDENTIFIERS WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M)
1999
Part: WIRE — DISCONNECTED
SEA - AFTER ARRIVAL OF FLIGHT 557, CRWE REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE.. RECONNECTED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (M)
Part: WIRE — FAILED (ROW 13-15)
SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 13 TO 15 WERE FOUND INOPERATIVE. REPLACED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (M)
Part: HOOK — DAMAGED (L1 DOOR)
SEA - FLT 94 - PRIOR TO DEPARTURE, CREW REPORTED THE L1 DOOR WOULD NOT CLOSE, DOOR RESTING ON JETWAY. STRAIGHTENED LOWER RT CORNER OF DOOR AND STRAIGHTENED HOLD OPEN HOOK. DOOR OPERATED NORMALLY. (M)
Part: LIGHT — DEFECTIVE (CABIN)
SEA - DURING MAINTENANCE CHECK THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. PART TC: 14,132. (X)
Part: POWER SUPPLY — INOPERATIVE (CABIN)
SEA - DURING MAINTENANCE CHECK, THE AFT OVERWING EMERGENCY EXIT IDENTIFIERS FLASH WHEN THE AUXILIARY HYDRAULIC PUMP IS SWITCHED ON. REPLACED THE POWER SUPPLY AND OPERATED NORMALLY. (M)
1998
Part: PORTABLE LIGHT — INOPERATIVE (CABIN)
PDX - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M)
Part: LIGHT — INOP (CABIN)
SEA - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M)
Part: SKIN — BIRD STRIKE (BS 37-69)
SEA - DURING APPROACH OF FLT 537, CREW REPORTED STRIKING AN EAGLE ON THE FORWARD FUSELAGE AREA AT 3,000 FEET MSL. FOUND DAMAGE CONTAINED WITHIN THE UNPRESSURIZED AREA FROM FS 37 TO FS 69.55 FROM THE FRP TO Z-30. REMOVED DAMAGED STRUCTURES AND INSTALLED NEW STRUCTURES IAW ASA EA 5330-01322. (M)
1997
Part: SWITCH — MALFUNCTIONED (FLIGHT COMPT)
SEA - AFTER ARRIVAL OF FLT 379, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS ILLUMINATE INTERMITTENTLY DURING FLIGHT. ACCOMPLISHED OPERATIONAL CHECK OF EMERGENCY FLOOR TRACK LIGHTING SYSTEM, UNABLE TO DUPLICATE DISCREPANCY. PRECAUTONARY REPLACED THE EMERGENCY LIGHTS CONTROL SWITCH S1-177 ON THE OVERHEAD PANEL IN THE FLIGHT COMPARTMENT AND OPERATED NORMALLY. (X)