N33414
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.
55 reports on file, 1995-05-14 – 2009-09-16.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 67,895 hrs · 36,156 cycles
EMERGENCY LIGHT BATTERY PACK AT OVERHEAD SEAT ROW 29DEF INOPERATIVE. REPLACED BATTERY PACK AND CHARGER.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 67,862 hrs · 36,138 cycles
EMERGENCY LIGHT AT OVERHEAD SEAT ROW 4AB INOP. REPLACED LAMP, OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 67,862 hrs · 36,138 cycles
EMERGENCY LIGHT AT OVERHEAD SEATS 5AB INOPERATIVE. REPLACED LAMP AT OVERHEAD SEAT 5AB.
Part: SKIN — DAMAGED (NR 1 SLAT) · airframe 66,770 hrs · 35,537 cycles
RIGHT WING NR 1 SLAT SKIN IS BENT AT AFT INBOARD SIDE. INSTALLED DOUBLER REPAIR PER AARD 57-50-00-5, FIGURE 1 SHEET 1, AND SRM 51-60-00 FIGURE 1, SHEET 1.
Part: LONGERON — CRACKED (ZONE 200) · airframe 66,770 hrs · 35,537 cycles
CRACK IN LONGERON 2R AT STATION 1418. INSTALLED LONGERON SPLICE PER AARD 53-30-00-2.
Part: SKIN — CRACKED (ZONE 200) · airframe 66,770 hrs · 35,537 cycles
SKIN CRACKED UNDER LONGERON 2R AT STATION 1418. STOP DRILLED CRACK AND INSTALLED INTERNAL AND EXTERNAL DOUBLERS PER SRM 53-04-00.
Part: LONGERON — CRACKED (ZONE 200) · airframe 66,770 hrs · 35,537 cycles
LEFT SIDE LONGERON 2 IS CRACKED IN RADIUS AT FRAME STATION 1418. SPLICE REPAIR ACCOMPLISHED PER AARD 53-30-00-2.
Part: BEAM — DAMAGED (ZONE 100) · airframe 66,770 hrs · 35,537 cycles
FASTENER HOLE DAMAGED IN AFT CARGO DOOR BEAM STATION 1163. INSTALLED FREEZE PLUG PER EA MD80-53-005908.
Part: WEB — CORRODED (ZONE 100) · airframe 66,772 hrs · 35,538 cycles
LEVEL 1 CORROSION ON WEB INSIDE THE LOWER DOOR AREA FROM STATION 1155-1174. REMOVED SECTION OF WEB AND SPLICED IN NEW SECTION FROM STATION 1143-1163 PER AARD 53-10-00-24, AND BLENDED SPOTS OF LIGHT CORROSION FROM STATION 1163-1174 WITHIN LIMITS.
Part: FRAME — CRACKED (ZONE 200) · airframe 66,770 hrs · 35,537 cycles
AFT ACCESSORY LEFT SIDE CANTED FRAME 1463 HAS A CRACKED DOUBLER AT LONGERON 18L. INSTALLED DOUBLER PER SRM 53-01-00 FIGURE 2, SHEET 4 AND AARD 51-00-00-014.
Part: FRAME — CORRODED (ZONE 100) · airframe 66,772 hrs · 35,538 cycles
LEVEL 1 CORROSION ON LOWER FRAME IN AFT CARGO AT STATION 1309 FROM LONGERON 25R TO LONGERON 25L. REPLACED FRAME SECTION AT STATION 1309 PER SRM 53-03-00 FIGURE 2A.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 66,772 hrs · 35,538 cycles
LEVEL 1 CORROSION ON SEAT TRACK NR 6 OUTBOARD FLANGE BETWEEN STATION 216-237. INSTALLED NEW SEAT TRACK PER AARD 51-00-00 PAGE 12.
Part: INTERCOSTAL — CRACKED (ZONE 100) · airframe 66,770 hrs · 35,537 cycles
INTERCOSTAL CRACKED AROUND CLIP NUTS IN AFT CARGO, STATION 1271-1287. INSTALLED SERVICEABLE INTERCOSTAL PER AARD 51-00-00-012.
Part: CARGO TRACK — CORRODED (ZONE 100) · airframe 66,772 hrs · 35,538 cycles
LEVEL 1 CORROSION ON LEFT TIE DOWN TRACK IN AFT CARGO STATION 1022-1220 AROUND SCREWS AT ATTACH FRAMES. REMOVED AND REPLACED TIE DOWN TRACK FROM STATION 1022-1220 PER SRM 51-30-01.
Part: CUSP WEB — CORRODED (ZONE 200) · airframe 66,772 hrs · 35,538 cycles
LEVEL 1 CORROSION ON RIGHT CUSP SHEET AT STATION 219. CUSP SHEET REPLACED PER AARD 53-20-00-16.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 66,772 hrs · 35,538 cycles
LEVEL 1 CORROSION ON NR 5 SEAT TRACK FROM STATION 203-204. REPLACED NR 5 SEAT TRACK FROM STATION 200-246 PER SRM 51-30-01.
Part: WEB — CRACKED (ZONE 100) · airframe 66,770 hrs · 35,537 cycles
CRACK AT INBOARD EDGE OF LIGHTENING HOLE IN AFT CARGO STATION 1212, LONGERON 25R. REPAIRED WEB PER AARD 53-10-00-24 FIGURE 1 AND EA MD80-53-005921 DATED 04/06/09.
Part: BEAM — CORRODED (ZONE 100) · airframe 66,772 hrs · 35,538 cycles
LEVEL 1 CORROSION ON THREE AREAS OF MID CARGO DOOR BEAM VERTICAL LEG. ACCOMPLISHED REPAIR PER AARD 53-10-00-3.
Part: FITTING — CORRODED (ZONE 200) · airframe 66,772 hrs · 35,538 cycles
LEVEL 1 CORROSION ON FORWARD GIRT BAR FITTING AT AFT SERVICE DOOR. REPLACED GIRT BAR FITTING PER SRM 51-30.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 66,772 hrs · 35,538 cycles
LEVEL 1 CORROSION ON NR 1 SEAT TRACK AT STATION 1026. INSTALLED SERVICABLE SEAT TRACK PER SRM 51-30-01.
Part: CUSP WEB — CORRODED (ZONE 200) · airframe 66,772 hrs · 35,538 cycles
LEVEL 1 CORROSION UNDER FORWARD GIRT BAR BRACKET AT AFT SERVICE DOOR. INSTALLED DOUBLER ON CUSP PER AARD 53-20-00-16.
Part: SUPPORT BRACKET — CORRODED (ZONE 200) · airframe 66,772 hrs · 35,538 cycles
LEVEL 1 CORROSION AT AFT SERVICE DOOR ON AFT GIRT BAR SUPPORT BRACKET. REPLACED GIRT BAR AT AFT SERVICE DOOR PER SRM 51-01.
Part: FITTING — CORRODED (ZONE 200) · airframe 66,772 hrs · 35,538 cycles
LEVEL 1 CORROSION FOUND ON NR 2 GALLEY INBOARD FORWARD ATTACH FITTING. REPLACED MOUNT FITTING PER SRM 51-01.
Part: MOUNT — CORRODED (GALLEY) · airframe 66,772 hrs · 35,538 cycles
LEVEL 1 CORROSION FOUND ON NR 2 GALLEY INBOARD AFT ATTACH FITTING. INSTALLED NEW GALLEY TIE DOWN FITTING PER SRM 51-30.
Part: CUSP WEB — CRACKED (ZONE 200) · airframe 66,770 hrs · 35,537 cycles
CUSP SHEET CRACKED AT STATION 905 LEFT HAND, UNDER NR 1 SEAT TRACK. INSTALLED DOUBLER PER AARD 53-20-00-16.
Part: CUSP WEB — CRACKED (ZONE 200) · airframe 66,770 hrs · 35,537 cycles
LEFT CUSP CRACKED AT STATION 812. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 66,772 hrs · 35,538 cycles
NR 1 SEAT TRACK CORRODED AT STA 931, LEVEL 1 CORROSION. INSTALLED SEAT TRACK PLUG IAW AARD 53-20-00-10.
Part: CUSP WEB — CRACKED (ZONE 200) · airframe 66,770 hrs · 35,537 cycles
LEFT CUSP CRACKED AT STATION 227. INSTALLED DOUBLER PER AARD 53-20-00-16.
Part: CASTING — CRACKED (ZONE 200) · airframe 66,770 hrs · 35,537 cycles
CASTING AT STATION 927, BELOW NR 5 SEAT TRACK CRACKED ON THE BOTTOM END. REMOVED AND REPLACED CASTING PER SRM 51-01.
Part: STIFFENER — CRACKED (ZONE 200) · airframe 66,770 hrs · 35,537 cycles
VERTICAL STIFFENER AT STATION 1338, LONGERON 1 IS CRACKED ABOVE TOP FASTENER. INSTALLED DOUBLER PER AARD 53-10-00-15.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 66,772 hrs · 35,538 cycles
LEVEL 1 CORROSION ON NR 2 SEAT TRACK AT STATION 1200. INSTALLED SEAT TRACK PLUG REPAIR PER AARD 53-20-00-10.
Earlier reports · 1995–2008 · 24 reports
2008
Part: STRAP — BROKEN (FLASHLIGHT) · airframe 65,398 hrs
LGA - EMERGENCY FLASHLIGHT AT AFT RIGHT LAVATORY HAS STRAP BROKEN. REPLACED STRAP FOR EMERGENCY FLASHLIGHT AT AFT RIGHT LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 65,398 hrs
LGA - LEFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR EXTERIOR LEFT EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.
2007
Part: STRAP — DAMAGED (FLASHLIGHT)
LGA - EMERGENCY FLASHLIGHT AT AFT FLIGHT ATTENDANT SEAT HAS DAMAGED STRAP. REPLACED STRAP FOR EMERGENCY FLASHLIGHT AT AFT FLIGHT ATTENDANT SEAT. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)
LGA - SEAT MOUNTED EMERGENCY LIGHTS AT AFT CABIN INOPERATIVE. REPLACED BATTERY PACK AB5 3 FOR SEAT MOUNTED EMERGENCY LIGHTS AT AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: SOCKET — INOPERATIVE (EMERGENCY LIGHT)
LGA - FOUND EMERGENCY LIGHT AT SEAT 14D INOPERATIVE. REPLACED LIGHT SOCKET ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 14D. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)
LGA - FOUND EMERGENCY LIGHT IN FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK IN FIRST CLASS OVERHEAD PANEL FOR EMERGENCY LIGHTS IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION.
2005
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)
SFO - SEAT MOUNTED EMERGENCY LIGHTS FROM 21D TO AFT CABIN INOPERATIVE. REPLACED AFT BATTERY PACK FOR SEAT MOUNTED EMERGENCY LIGHTS FROM 21D TO AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BATTERY PACK — DISCHARGED (CABIN)
SFO - CEILING EMERGENCY LIGHTS AT ROWS 23 TO 27 INOPERATIVE. REPLACED BATTERY PACK AT ROW 27 FOR CEILING EMERGENCY LIGHTS AT ROWS 23 TO 27. SYSTEM GROUND CHECKED NORMAL OPERATION.
2004
Part: WIRE — INOPERATIVE (EMERGENCY LIGHT)
DFW - EMERGENCY ESCAPE PATH LIGHT AT FORWARD GALLEY WALL INOPERATIVE. REPAIRED WIRE FOR EMERGENCY ESCAPE PATH LIGHT AT FORWARD GALLEY WALL. SYSTEM GROUND CHECKED NORMAL OPERATION.
2002
Part: CONTACTOR — DIRTY (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, BOTH FORWARD OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. CLEANED CONTACTS ON OVERWING BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: BATTERY — DISCHARGED (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AFT CABIN INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: SKIN — CRACKED (WING)
TUL - FOUND NR 8 SLAT TRACK AREA, TOP OF LEADING EDGE HAS CRACK TO SKIN, XRS 256. STOP DRILLED CRACK AND INSTALLED DOUBLER PER AARD 57-30-00-8. (M)
Part: SHEAR TIE — CRACKED (FUSELAGE)
TUL - FOUND SHEAR TIE DOUBLER CRACKED UNDER LEFT SIDE VERTICAL STABILIZER ATTACH ANGLE. INSTALLED NEW SHEAR TIE PER SRM 51. (M)
Part: SHEAR TIE — CRACKED (FUSELAGE)
TUL - FOUND SHEAR TIE CRACKED ON AFT SIDE OF STATION 1437. INSTALLED NEW SHEAR TIE PER SRM. (M)
Part: SKIN — CRACKED (FUSELAGE)
TUL - FOUND FUSELAGE SKIN CRACKED AT RIVET ABOVE PYLON ANGLE STATION 1380. STOP DRILLED CRACK. FABRICATED AND INSTALLED DOUBLER PER AARD 53-30-00-2. (M)
2000
Part: LIGHT — INOPERATIVE (SEAT 30)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT AT SEAT 30D INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT SEAT 30D. SYSTEM GROUND CHECK NORMAL OPERATION.. (M)
1999
Part: NLG — LACK OF LUBE (NOSE)
LGA - FLT 693 - AFTER TAKEOFF RED NOSE GEAR LIGHT REMAINED ILLUMINATED. LOUD AIR NOISE. RECYCLED GEAR NO HELP. RETURNED AND LANDED LGA WITHOUT INCIDENT. SERVICED NOSE STRUT AND ACCOMPLISHED GEAR SWING SEVERAL TIMES. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
Part: WIRE — CHAFED (CABIN)
DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS IN FIRST CLASS WERE INOPERATIVE. REPAIRED EMERGENCY FLOOR PATH LIGHTING WIRE THAT WAS SHORTING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1998
Part: WIRE — LOOSE (COCKPIT)
DFW - DURING OVERNIGHT MAINTENANCE, COCKPIT EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE. RESECURED LOOSE GROUND WIRE AT COCKPIT EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: JAMB — CORRODED (BS 370-427)
TUL - FORWARD CARGO DOOR JAMB BEAM HAS CORROSION ON UPPER AND LOWER LEG. REMOVED AND REPLACED WITH NEW LOWER DOOR JAMB PAN. TST: 34,516.38 HOURS. CYCLES: 19,391. (X)
1997
Part: WINDOW — CRACKED (CABIN)
DTW - FLT 0366 - EN ROUTE ORD/LGA DURING CRUISE, PASSENGER SEATED AT 12A REPORTED POPPING SOUND AND OUTER WINDOW PANEL WAS NOTED TO HAVE VERTICAL CRACK EXTENDING UP FROM LOWER AFT CORNER OF WINDOW. AIRCRAFT DIVERTED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED WINDOW PANEL ASSEMBLY BY PASSENGER SEAT 12A. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
Part: VALVE — DEFECTIVE (NLG STRUT)
DFW - FLT 1789 - AFTER TAKEOFF TUL, GEAR UNSAFE MESSAGE WHEN LANDING GEAR RETRA CTED. RECYLED LANDING GEAR AND ALL INDICATIONS RETURNED TO NORMAL. AIRCRAFT PROCEEDED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR STRUT SCHRADER VALVE AND PACKING. SERVICED NOSE LANDING GEAR STRUT WITH OIL AND NITROGEN. ACCOMPLISHED NOSE LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: PRESSURE SYSTEM — MALFUNCTIONED (CABIN)
BNA - FLT 1997 - EN ROUTE BOS/DFW DURING CRUISE AT FL 350 WITH PRESSURIZATION SWITCH IN PRIMARY, CABIN ALTITUDE ALERT SOUNDED WITH CABIN ALTITUDE INDICATING 10,000 FEET. ALL PAX O2 MASKS DEPLOYED NORMALLY. ACCOMPLISHED EMERGENCY DESCENT AND AIRCRAFT DIVERTED TO BNA, LANDING WITHOUT INCIDENT. ACCOMPLISHED BITE CHECK OF BOTH RPESSURIZATION CONTROLLERS WITH NO DEFECTS FOUND. CHECKED ALL DOORS AND SEALS WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. ACCOMPLISHED FUNCTIONAL CHECK FLIGHT/ MAINTENANCE FERRY BNA/DFW WITH NO PRESSURIZATION DEFECTS FOUND. SYSTEM OPERATIONAL CHECKED NORMAL. RESTOWED ALL PAX O2 MASKS. OXYGEN SYSTEM GROUND CHECK NORMAL OPERATION. (M)
1995
Part: PRESSURIZATION — MALFUNCTIONED (CABIN)
BNA - FLT NR 0807 - EN ROUTE LGA/DFW, DURING CRUISE AT FL 370, CABIN ALTITUDE ALARM SOUNDED WITH FLOW LIGHT ILLUMINATED. SELECTED MANUAL CABIN ALTITUDE CONTROL AND WITH OUTFLOW VALVES CLOSED, CABIN CONTINUED TO CLIMB. AS CABIN ALTITUDE APPROACHED FL 110, INITIATED EMERGENCY DESCENT AND ALL PAX OXYGEN MASKS DEPLOYED. A/C DIVERETED TO BNA AND LANDED W/O INCIDENT. ACCOMPLISHED BITE CHECK OF BOTH PRESS CONTROLLERS WITH NO DEFECTS FOUND. OUTFLOW VALVE CHECKED NORMAL OPERATION. ACCOMP GROUND ENG RUN AND PRESSURIZED A/C IN AUTO AND MANUAL MODES WITH NO DEFECTS FOUND. ACCOMP PRESS LEAK CHECKS WITH NO DEFECTS FOUND. RESTOWED ALL PAX OXYGEN MASKS. UNABLE TO DUP PROBLEM. A/C RETURNED TO SERVICE. (M)