N933AS
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.
78 reports on file, 1995-03-29 – 2002-07-14.
Part: POWER SUPPLY — DISCHARGED (CABIN)
SEA - DURING LINE CHECK, OVERHEAD EMERGENCY LIGHTING WAS INOPERATIVE AT ROW 9. REPLACED POWER SUPPLY (BATTERY PACK). LIGHTS THEN OPERATED PROPERLY. (M)
Part: LANYARD — DETACHED (EVAC SLIDE)
SEA - DURING PREFLIGHT CHECK, R1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND TO BE DETACHED. ATTACHED LANYARD. (M)
Part: LANYARD — DISCONNECTED (EVAC SLIDE)
SEA - DURING PREFLIGHT CHECK, R2 DOOR EMERGENCY SLIDE LANYARD WAS FOUND TO BE DETACHED. ATTACHED LANYARD. (M)
Part: LANYARD — DISCONNECTED (ESCAPE SLIDE)
SEA - DURING PREFLIGHT CHECK, R-1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND TO BE DETACHED. REATTACHED LANYARD. (M)
Earlier reports · 1995–2001 · 74 reports
2001
Part: BATTERY PACK — DISCHARGED (CABIN)
SEA - DURING LINE MAINTENANCE CHECK, DETERMINED EMERGENCY TRACK LIGHTING TO BE INOPERATIVE IN FORWARD CABIN. REPLACED DISCHARGED BATTERY PACK AND REPAIRED BROKEN WIRE AT PIN 1 IN THE CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M)
Part: MODULE — LOOSE (CABIN)
SEA - DURING PRE-FLIGHT CHECK, DETERMINED EMERGENCY TRACK LIGHTING TO BE INOPERATIVE IN FORWARD CABIN. RECONNECTED LOOSE LIGHT MODULE. LIGHTS THEN OPERATED PROPERLY. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
SEA - DURING PREFLIGHT CHECK, DETERMINED EMERGENCY TRACK LIGHTING TO BE INOPERATIVE IN FORWARD CABIN. REPLACED DISCHARGED BATTERY PACK. LIGHTS THEN OPERATED NORMALLY. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
LAX - DURING PRE-FLIGHT CHECK, DETERMINED EMERGENCY TRACK LIGHTING TO BE INOPERATIVE IN FIRST CLASS CABIN. REPLACED DISCHARGED BATTERY PACK. LIGHTS THEN OPERATED PROPERLY. (M)
Part: SKIN — CORRODED (FUSELAGE)
OAK - DURING C-CHECK, FOUND CORROSION UNDER RIBSTRIP FROM FS STATION 788 TO 1361. REMOVED CORROSION AND INSTALLED DOUBLER PER EA 5330-01539. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
PDX - DURING RON CHECK, OVERHEAD EMERGENCY LIGHTING WAS INOPERATIVE BETWEEN ROWS 7 AND 13. REPLACED ASSOCIATED BATTERY POWER SUPPLY PACK. LIGHTS THEN OPERATED PROPERLY. (M)
Part: SPLICE — LOOSE (CABIN)
SAN - DURING PREFLIGHT CHECK, EMERGENCY FLOOR TRACK LIGHTING WAS INOPERATIVE FROM ROW 6 FORWARD. RESECURED LOOSE SPLICE. LIGHT THEN OPERATED PROPERLY. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
PDX - DURING PRE-FLIGHT CHECK, FOUND FIRST NINE EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE. REPLACED ASSOCIATED BATTERY PACKS. LIGHTS THEN OPERATED PROPERLY. (M)
Part: POWER SUPPLY — INOPERATIVE
PHX - DURING A-CHECK, EXTERIOR OVERWING EMERGENCY EXIT LIGHTS ON BOTH SIDES OF AIRCRAFT WERE DETERMINED TO BE INOPERATIVE. REPLACED ASSOCIATED BATTERY PACK. LIGHTS THEN OPERATED NORMALLY. (M)
Part: POWER SUPPLY — DISCHARGED (FWD CABIN)
PHX - PRIOR TO FLT 707 - THE EMERGENCY EXIT LIGHTS FROM ROW 10 FORWARD WERE FOUND TO BE INOPERATIVE. REPLACED THE POWER SUPPLY AND THE LIGHTS OPERATED NORMALLY. (M)
Part: BATTERY — DISCHARGED (CABIN)
SEA - DURING LINE CHECK, BATTERIES FOR THE OVERHEAD EMERGENCY LIGHTS IN MID CABIN WERE DETERMINED TO HAVE LOW CHARGE. REMOVED AND REPLACED ASSOCIATED BATTERY PACKS. LIGHTS THEN OPERATED PROPERLY. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
SEA - DURING PRE-FLIGHT CHECK, OVERHEAD EMERGENCY LIGHTS AT VARIOUS LOCATIONS WERE DETERMINED TO BE INOPERATIVE. REPLACED ASSOCIATED BATTERY PACKS. LIGHTS THEN OPERATED PROPERLY. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
LAX - DURING PRE-FLIGHT, EMERGENCY LIGHTS IN BOTH THE PASSENGER CABIN AND COCKPIT WERE DETERMINE TO BE INOPERATIVE. REPLACED ASSOCIATED BATTERY PACKS. LIGHTS THEN OPERATED PROPERLY. (M)
2000
Part: BATTERY PACK — DISCHARGED (CABIN)
SEA - DURING LINE CHECK, OVERHEAD EMERGENCY LIGHTS BETWEEN CABIN ROWS 91-2 WERE DETERMINED TO BE INOPERATIVE. REPLACED ASSOCIATED BATTERY ASSEMBLIES. LIGHTS THEN OPERATED NORMALLY. (M)
Part: POWER SUPPLY — DISCHARGED (GALLEY)
SEA - DURING LINE CHECK, OVERHEAD EMERGENCY LIGHTING AT AFT GALLEY WAS DETERMINED TO BE INOPERATIVE. REPLACED ASSOCIATED BATTERY POWER SUPPLY. LIGHTS THEN OPERATED NORMALLY. (M)
Part: LATCH — INOPERATIVE (PAX DOOR)
ZIH PRIOR TO FLIGHT 291 THE L1 DOOR WOULD NOT LATCH OPEN AND THE LATCH MECHANISM WOULD NOT RETRACT WHEN THE DOOR CLOSES. REMOVED THE HOLD OPEN HOOK AND INSPECTED THE AIRCRAFT FOR FERRY FLIGHT TO LAX FOR REPAIR. FERRIED AIRCRAFT TO LAX. LAX MAINTENANCE REPLACED THE DOOR OPEN LATCH CRANK ASSEMBLY AND THE DOOR OPERATED NORMALLY.
Part: BATTERY — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS BETWEEN THE AFT LAVATORIES WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M)
Part: POWER SUPPLY — INOPERATIVE (CABIN)
SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROW 6 TO 8 WERE FOUND INOPERATIVE. REPLACED THE POWER SUPPLY AND OPERATED NORMALLY. (M)
Part: SPAR CAP — DAMAGED (RT WING)
OAK: DURING C CHECK 2 SMALL DRILL HOLES WERE FOUND IN RT WING L/E LOWER SPAR CAP AT XRS 522.7. TRIMMED OUT DAMAGED AREA AND INSTALLED FILLER AND DOUBLER IAW ASA EA 5710-01060.
Part: BATTERY — DISCHARGED (CABIN)
OAK - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS AT ROW 22 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M)
Part: LIGHT — SHORTED (CABIN)
OAK - DURING MAINTENANCE CHECK, THE FORWARD OVERWING EMERGENCY EXIT IDENTIFIERS WERE FOUND INOPERATIVE. REPAIRED SHORTED LIGHT CONTACTS AND OPERATED NORMALLY. (M)
Part: DOUBLER (SKIN)
OAK: DURING C CHECK DENTS AND GOUGES WERE FOUND IN EXISTING INTERIM REPAIR DOUBLER ON FUSELAGE SKIN, FS1322, LONGERON 19L TO 22L.REMOVED EXISTING DOUBLER AND INSTALLED NEW DOUBLER IAW ASA EA 5330-01400.
Part: WEB — CRACKED (FUSELAGE)
OAK: DURING C CHECK CRACKS WERE FOUND IN LT CABIN MEMBRANE, FS 1287 TO 1309, LONGERON 18L. REMOVED CRACKED SECTIONS AND INSTALLED REPAIR DOUBLER IAW ASA EA 5320-01203.
Part: SKIN — CORRODED (FUSELAGE)
OAK: DURING C CHECK CORROSION WAS FOUND ON FUSELAGE SKIN AND ANTENNA DOUBLER, FS 636 TO 655, LONGERON 29L TO 29R. REMOVED CORRODED SECTION OF INNER SKIN AND ANTENNA DOUBLER. INSTALLED INTERNAL DOUBLER AND TRIPLER IAW ASA EA 5330-01430. INSTALLED ANTENNA DOUBLER IAW DC9 SRM 51-30-05, PG 12.
Part: BATTERY — DISCHARGED (CABIN) · airframe 46,300 hrs · 29,757 cycles
SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY EXIT LIGHTS AT ROWS 19 - 22 WERE FOUND INOPERATIVE. REPLACED BATTERIES IN BATTERY PACK AND LIGHTS OPERATED NORMALLY. (X)
Part: BATTERY — DISCHARGED (CABIN) · airframe 46,300 hrs · 29,757 cycles
SEA - DURING MAINTENANCE CHECK, THE FORWARD OVERWING EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. REPLACED BATTERIES IN BATTERY PACK AND LIGHTS OPERATED NORMALLY. (X)
1999
Part: POWER SUPPLY — DEFECTIVE (CABIN)
PDX - DURING MAINTENANCE CHECK, THE EXTERIOR OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. REPLACED THE POWER SUPPLY AND OPERATED NORMALLY. (M)
Part: BATTERIES — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK THE AFT OVERWING EMERGENCY EXIT IDENTIFIERS WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (X)
Part: BATTERIES — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE AFT GALLEY WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M)
Part: GROUND — CORRODED (COCKPIT)
SEA - AFTER ARRIVAL OF FLIGHT 731, CREW REPOTED THE OVERHEAD EMERGENCY LIGHT IN THE FLIGHT COMPARTMENT WAS DIM. CLEANED CORROSION FROM GROUND STUD 128 ON OVERHEAD PANEL AND OPERTED NORMALLY. (M)
1998
Part: MECHANISM — OUT OF ADJUST (L1 DOOR)
SEA - DURING MAINTENANCE CHECK, THE L1 DOOR WOULD NOT LATCH OPEN. ADJUSTED DOOR HOLD OPEN MECHANISM 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)
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)
Part: SKIN — CORRODED (BS 662)
LCQ - DURING 15K CHECK, FOUND CORROSION ON LOWER FUSELAGE SKIN AT FS 662. REPAIRED IAW ASA EA 5330-01360. (M)
Part: LONGERON — CORRODED (BS 636-650)
LCQ - DURING 15K CHECK, FOUND CORROSION ON LONGERON 30 FROM FS 636 TO 650. REPAIRED IAW ASA EA 5310-01637. (M)
Part: JAMB — CRACKED (L1 DOOR)
LCQ - DURING 15K CHECK, THE L1 DOOR JAMB INNER SKIN TO INTERCOSTAL ATTACH TABS WERE FOUND CRACKED AT FS 208 AT LONGERONS 11L AND 15L. REPAIRED IAW ASA EA 5310-01635. (M)
Part: CONNECTOR — FAILED (ROW 22-23)
SEA - CREW REPORTED HOT SCORCHED PLASTIC ODOR IN AREA OF ROWS 22 THROUGH 25. REPLACED MELTED CONNECTORS P2-3291 AND R5-3292 ABOVE ROW 22 LT, BALLAST AT ROWS 22-32 RT AND BULBS FROM ROWS 18-28. NO ODORS WERE DETECTED. (M)
Part: SPRING — DISCONNECTED (PAX DOOR)
PDX - DURING MAINTENANCE CHECK, THE L2 DOOR WOULD NOT LATCH OPEN. RECONNECTED SPRING TO HOLD OPEN MECHANISM AND OPERATED NORMALLY. (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: BATTERY — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 24 TO 27 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M)
Part: MECHANISM — LACK OF LUBE (R1 DOOR)
LAX - DURING MAINTENANCE CHECK, THE R1 DOOR WAS FOUND DIFFICULT TO OPEN AND CLOSE. LUBED THE R1 DOOR MECHANISM AND OPERATED NORMALLY. (M)
1997
Part: RIB — WORN (WS 138)
OAK - DURING C-CHECK, THE RIGHT WING TRAILING EDGE RIB AND SPOILER WEAR PADS WERE FOUND WORN BEYOND LIMITS. REPAIRED RIB AND WEAR PADS IAW ASA EA 5720-01130. (M)
Part: HOLD OPEN HOOK — OUT OF ADJUST (L1 DOOR)
PDX - AFTER ARRIVAL OF FLT 459, CREW REPORTED THE L1 DOOR WAS DIFFICULT TO OPEN OR CLOSE. REPLACED THE BAYONET ASSEMBLY AND ADJUSTED THE HOLD OPEN HOOK AND DOOR OPERATED NORMALLY. REFERENCE ASAA9780011
Part: BAYONET ASSY — DEFECTIVE (L1 DOOR)
PDX - AFTER ARRIVAL OF FLT 459, CREW REPORTED THE L1 DOOR WAS DIFFICULT TO OPEN OR CLOSE. REPLACED THE BAYONET ASSEMBLY AND ADJUSTED THE HOLD OPEN HOOK AND DOOR OPERATED NORMALLY. (M)
1996
Part: MECHANISM — OUT OF ADJUST (L-1 DOOR)
SEA - FLT 325 - CREW REPORTED FORWARD ENTRY DOOR DIFFICULT TO OPEN. RECYCLED DOOR AND OPENED EASIER. ADJUSTED DOOR PER THE MM, PRESSURIZED AIRCRAFT TO 7.5 PSI AND DOOR OPERATED NORMALLY. (M)
Part: DOOR — MISADJUSTED (CABIN)
SEA - FLT 425 - CREW REPORTED FORWARD ENTRY DOOR DIFFICULT TO OPEN. PRESSURIZED AIRCRAFT TO 7.5 PSI. FOUND DOOR DIFFICULT TO OPEN ON FIRST ATTEMPT, BUT OPERATED NORMALLY AFTER BEING OPENED ONCE. ADJUSTED DOOR PER THE MM, PRESSURIZED AIRCRAFT TO 7.5 PSI AND DOOR OPERATED NORMALLY. (M)
Part: MECHANISM — OUT OF ADJUST (L1 DOOR)
LAX - AFTER ARRIVAL OF FLT 291 - CREW REPORTED THE L1 DOOR WAS DIFFICULT TO OPEN. ADJUSTED L1 DOOR AND LUBED LINKAGES AND DOOR OPERATED NORMALLY. (M)
Part: DOOR — OUT OF ADJUST (L1 DOOR)
SFO - AFTER ARRIVAL OF FLIGHT 496 - CREW REPORTED THE L1 DOOR HANDLE WAS DIFFICULT TO UNLOCK. ADJUSTED L1 DOOR AND OPERATED NORMALLY. (M)
Part: LIGHT — INOPERATIVE (TAILCONE)
SEA - DURING MAINTENANCE CHECK, THE FIRST OVERHEAD EMERGENCY EXIT LIGHT IN THE TAILCONE AREA WAS FOUND INOPERATIVE AND BROKEN. REPLACED LIGHT ASSEMBLY AND OPERATED NORMALLY. (M)
Part: SPRING — BROKEN (L2 DOOR)
ANC - DURING MAINTENANCE CHECK, THE L2 DOOR HOLD OPEN LATCH SPRING WAS FOUND BROKEN. REPLACED THE SPRING AND OPERATED NORMALLY. (M)
Part: HANDLE — OUT OF ADJUST (PAX DOOR)
PDX - AFTER ARRIVAL OF FLT 485, CREW REPORTED THE L1 DOOR WAS DIFFICULT TO OPEN, HANDLE STOPPED AND HAD TO BE CYCLED TO OPEN DOOR. CLEANED AND LUBED L1 DOOR MECHANISM AND DOOR OPERATED NORMALLY. (M)
Part: BATTERY — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE L-1 DOOR PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED BATTERIES IN LIGHT ASSY AND LIGHT OPERATED NORMALLY. (X)
Part: CONTAINER LATCH — LOOSE (L1 DOOR)
PDX - AFTER ARRIVAL OF FLT 586 - CREW REPORTED, THE L1 DOOR WAS DIFFICULT TO OPEN. FOUND EMERGENCY EVACUATION SLIDE CONTAINER LATCH LOOSE, SECURED LATCH AND OPERATED NORMALLY. (M)
1995
Part: BATTERIES — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN AFT CABIN WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND LIGHTS OPERATED NORMALLY. (X)
Part: LATCH MECHANISM — LACK OF LUBE (L1 DOOR)
ANC - ON ARRIVAL OF FLIGHT 112, CREW REPORTED THE L1 DOOR LEVER LATCH DIFFICULT TO OPEN. LUBED LATCH MECHANISM AND OPERATED NORMALLY. (M)
Part: BATTERY — DISCHARGED (CABIN)
SEA - DURING MAINTENACNE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 19 TO 22 AND BETWEEN AFT LAVS WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND LIGHTS OPERATED NORMALLY. (M)
Part: PORTABLE EEL — DEFECTIVE (CABIN)
SEA - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT CHARGE INDICATOR LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M)
Part: HANDLE MECH — LACK OF LUBE (FWD ENTRY DOOR)
SEA - ON ARRIVAL OF FLIGHT 367 - CREW REPORTED, THE FORWARD ENTRY DOOR HANDLE DIFFICULT TO UNLATCH. LUBED DOOR HANDLE MECHANISM AND DOOR OPERATED NORMALLY. (M)
Part: EEL PORTABLE — INOPERATIVE (CABIN)
PDX - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSY AND OPERATED NORMALLY. (W)
Part: FRAME — CORRODED (FS 503)
PAE - DURING 30K CHECK, CORROSION WAS FOUND ON FRAME AT Y503, Z PLUS 54, LONGERON 28L TO 28R. REPLACED FRAME IAW DC-9 SRM 53-03. (W)
Part: SKIN — CORRODED (FS 560-592)
PAE - DURING 30K CHECK, CORROSION WAS FOUND ON SKIN AT Y560 TO Y592, X PLUS 10 TO X-4, Z-50. REMOVED CORROSION AND INSTALLED INTERNAL DOUBLER IAW ASA EA 5330-01193. (W)
Part: FRAME — DAMAGED (FS 1212)
PAE - DURING 30K CHECK, DAMAGE WAS FOUND ON FRAME AT Y1212, LONGERON 3L. REMOVED AND REPALCED DAMAGED FRAME IAW DC-9 SRM 53-03 AND 51-10-03. (W)
Part: LONGERON — CORRODED (FS 579)
PAE - DURING 30K CHECK, CORROISON WAS FOUND ON LONGERON 29L AT Y579. REPLACED LONGERON IAW DC-9 SRM 53-01 AND 53-02. (W)
Part: LONGERON — CORRODED (FS 1128-1155)
PAE - DURING 30K CHECK, CORROSION WAS FOUND ON LONGERON 29R AT Y1128 TO Y1155. REMOVED CORROSION AND INSTALLED REPAIR IAW ASA EA 5310-01360. (W)
Part: FLOOR SUPPORT — CORRODED (FS 788)
PAE - DURING 30K CHECK, CORROSION WAS FOUND ON FLOOR SUPPORT AT Y788, X-5 TO X PLUS 4, Z-47 TO Z-50. REPLACED FLOOR SUPPORT IAW DC-9 SRM 51-10-03, 51-30-05, 51-30-02, 51-20-00. (W)
Part: SKIN — CORRODED (FS 1100-1170)
PAE - DURING 30K CHECK, CORROSION WAS FOUND ON INTERNAL SKIN AT Y1100 TO Y1170, X-5 TO Z-53. BLENDED AND TREATED AREA AND INSTALLED EXTERNAL DOUBLER IAW DC-9 SRM 53-04. (W)
Part: SUPPORT — CORRODED (FS 1030-1060)
PAE - DURING 30K CHECK, CORROSION WAS FOUND ON FAIRING SUPPORT AT Y1030 TO Y1060, X-0 TO Z-50. REPLACED FAIRING SUPPORT IAW DC-9 ARM 51-10-03, 51-10-01, 51-30-05. (W)
Part: FLOOR SUPPORT — CORRODED (FS 786)
PAE - DURING 30K CHECK, CORROSION WAS FOUND ON FLOOR SUPPORT AT Y786, X-15 TO X PLUS 15, Z-45. REPLACED FLOOR SUPPORT IAW DC-9 SRM 51-10-04. (W)
Part: RETAINER — CRACKED (LT COCKPIT)
PAE - DURING 30K CHECK, A CRACK WAS FOUND IN FASTENER HOLE OF WINDOW RETAINER BETWEEN LEFT CLEARVIEW WINDOW AND AFT COCKPIT WINDOW. STOP DRILLED CRACK AND INSTALLED DOUBLER IAW DC-9 SRM 56-01 AND 51-60-00. (W)
Part: FRAME — CORRODED (FS 1231)
PAE - DURING 30K CHECK, CORROSION WAS FOUND ON FRAME AND SHEAR TIE AT Y1231, X PLUS 15 TO X-15, Z-45 AND Y1231, X PLUS 0 TO X PLUS 12, Z-49. REMOVED CORRODED AREA OF FRAME. INSTALLED NEW FRAME, REPAIR ANGLES AND SPLICE PLATES IAW DC-9 SRM 53-03, 53-04, 53-10-03, 51-30-02. (W)
Part: LONGERON — CORRODED (FS 219-220)
PAE - DURING 30K CHECK, CORROSION WAS FOUND ON LONGERON 30L AT Y219 TO Y220. REPLACED LONGERON IAW DC-9 SRM 51-01, 51-10-01, 51-10-03. (W)
Part: FRAME — CORRODED (FS 1320)
PAE - DURING 30K CHECK, CORROSION WAS FOUND ON FRAME AT Y1320, X PLUS 20 TO X-10, Z-45. REMOVED CORRODED AREA OF FRAME. INSTALLED NEW FRAME AND REPAIR ANGLES IAW DC-9 SRM 53-03 AND 53-10-03. (W)
Part: SKIN — CORRODED (FS 216-221)
PAE - DURING 30K CHECK, DENTS WERE FOUND ON OUTER SKIN AT Y216 TO Y221, X PLUS 63 TO Z PLUS 4. REPAIRED SKIN IAW DC-9 SRM 53-04. (W)
Part: WEB — CORRODED (FS 1145-1167)
PAE - DURING 30K CHECK, CORROSION WAS FOUND ON L-2 WEB, STATION 1145 TO 1167. REMOVED CORROSION PER SRM AND EA 5320-01203. (W)