N809NY
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.
56 reports on file, 1995-03-18 – 2000-12-21.
Part: STRUCTURE — CRACKED (TORQUE BOX) · airframe 52,294 hrs · 24,378 cycles
INSPECTION FOUND TORQUE BOX WEB CRACKED AT FS 200-208, LBL 54 (AFT OF L-1 DOOR). THE TORQUE BOX WEB WAS REMOVED AND REPLACED IAW SRM 51-30-1.
Part: CARGO TRACK — GOUGED (FS 693-788) · airframe 52,294 hrs · 24,378 cycles
INSPECTION FOUND GOUGES IN MID PIT RT AFT CARGO TRACK AT FS 693-788. THE TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-30-1.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 52,294 hrs · 24,378 cycles
INSPECTION FOUND RT Z-ANGLE THAT MOUNTS TO CARGO TRACK CORRODED AT FS 693-733. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-1 AND 51-10-4.
Part: WEB — CRACKED (FS 1211) · airframe 52,294 hrs · 24,378 cycles
INSPECTION FOUND A 2 INCH CRACK AT LIGHTENING HOLE OF AFT CARGO TORQUE BOX WEB, FS 1211, L27R. THE WEB, ATTACHING STRAPS, AND L-ANGLE SUPPORT WERE REMOVED AND A NEW WEB WAS INSTALLED USING ATTACHMENT PARTS IAW SRM 51-30-2 AND 51-30-5.
Part: SUPPORT — CRACKED (FUSELAGE) · airframe 52,294 hrs · 24,378 cycles
INSPECTION FOUND AFT CARGO FLOORBOARD SUPPORT IN CARGO DOOR AREA CRACKED AT FS 1136-1220. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-1, 51-30-2, AND 51-30-5.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 52,294 hrs · 24,378 cycles
INSPECTION FOUND L-1 DOOR JAMB CUSP ANGLE CORRODED AT FS 200, LBL 54. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2, 51-30-5, ECRA 5310-04082, AND EA 9-5310-2-A809.
Part: STOP — WORN (CARGO DOOR) · airframe 52,294 hrs · 24,378 cycles
INSPECTION FOUND MID CARGO DOOR STOP PADS NR 2, 5, & 6 CHAFED/WORN. THE WORN AREAS WERE REMOVED AND A REPAIR DOUBLER WAS INSTALLED AT EACH LOCATION IAW SRM 51-10-3 AND ECRA 5330-02819.
Part: SEAT TRACK — CORRODED (FS 896) · airframe 52,294 hrs · 24,378 cycles
INSPECTION FOUND CABIN LT I/B SEAT TRACK CORRODED AT FS 896. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-1 AND 51-30-5.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 52,294 hrs · 24,378 cycles
INSPECTION FOUND FLOOR SUPPORT I/B OF DOOR SCUFF PLATE AT AFT SERVICE DOOR CORRODED. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 53-14-3, FIGURE 12 AND 51-30-02.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 52,294 hrs · 24,378 cycles
INSPECTION FOUND FORWARD ENTRY SUBFLOOR CORRODED AT FS 148, RBL 6 AND AT FS 160-170, RBL 9. A REPAIR DOUBLER WAS INSTALLED AT EACH LOCATION IAW SRM 53-01, FIGURE 4 AND 51-10-3.
Part: ANGLE — CRACKED (PAX DOOR) · airframe 52,294 hrs · 24,378 cycles
INSPECTION FOUND A 2 INCH CRACK IN L-1 DOOR FORWARD LOWER CORNER ANGLE. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-10-4, 51-10-3, AND 51-30-8.
Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 52,294 hrs · 24,378 cycles
INSPECTION FOUND RT FORWARD CARGO TIE DOWN TRACK CORRODED AT STA 218-370. THE TIE DOWN TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-30-1 AND 51-10-4.
Part: SKIN — DENTED (CARGO DOOR) · airframe 52,294 hrs · 24,378 cycles
INSPECTION FOUND EXTERIOR SKIN OF MID CARGO DOOR DENTED IN TWO PLACES. THE DENTED AREAS WERE CUT OUT AND DOUBLER AND FILLER REPAIRS WERE INSTALLED IAW SRM 52-05, FIGURE 3, 51-10-3, AND ECRA 5230-01207.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 52,294 hrs · 24,378 cycles
INSPECTION FOUND INTERCOSTAL CORRODED AT FS 1022-1041. THE INTERCOSTAL WAS REMOVED AND A NEW INTERCOSTAL WAS INSTALLED IAW SRM 51-10-4, 51-10-3, AND 51-10-5.
Part: RIB — CORRODED (BULKHEAD) · airframe 52,294 hrs · 24,378 cycles
INSPECTION FOUND FASTENER HOLES CORRODED IN MID PIT FORWARD BULKHEAD SUPPORT RIBS. THE SUPPORT RIBS(2) WERE REMOVED AND TWO NEW SUPPORT RIBS WERE INSTALLED IAW SRM 51-10-4, 51-10-3, AND 51-30-2.
Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 52,294 hrs · 24,378 cycles
INSPECTION FOUND LT CARGO TRACK IN MID PIT CORRODED ON UPPER AND LOWER SURFACES BETWEEN STA 541 AND 788. THE TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-30-2, 51-30-5, AND 51-30-1.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 52,294 hrs · 24,378 cycles
INSPECTION FOUND CABIN RT SEAT TRACK CORRODED AT FS 265-790. THE SEAT TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-30-2, 53-04, FIGURE 4F, AND 53-05, FIGURE 4B.
Part: FLOOR SUPPORT — CORRODED (FS 160-200) · airframe 52,294 hrs · 24,378 cycles
INSPECTION FOUND FORWARD ENTRY SUBFLOOR AND FLOOR SUPPORT CORRODED AT FS 160-200, LBL 54. THE SUBFLOOR AND FLOOR SUPPORT WERE REMOVED AND A REPAIR WAS INSTALLED IAW SRM 51-30-1, 51-10-4, AND 53-14-1, FIGURE 11.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 52,294 hrs · 24,378 cycles
INSPECTION FOUND LT O/B SEAT TRACK CORRODED AT STA 256. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-05, FIGURE 4F.
Part: WEB — CRACKED (FUSELAGE) · airframe 52,294 hrs · 24,378 cycles
INSPECTION FOUND 1 INCH CRACKS IN LT CUSP WEBS AT STA 1032, 1231, AND 1260. DOUBLERS WERE INSTALLED AT EACH CRACK LOCATION IAW SRM 53-01, FIGURE 2 AND 51-30-2.
Part: WEB — CORRODED (FUSELAGE) · airframe 52,294 hrs · 24,378 cycles
INSPECTION FOUND CUSP WEB CORRODED AT FS 200-237, LBL 56. THE CUSP WEB WAS REMOVED AND A NEW CUSP WEB WAS INSTALLED IAW SRM 51-30-2, 51-30-5, AND 53-14-1, FIGURE 11.
Part: FITTING — CORRODED (FUSELAGE) · airframe 52,294 hrs · 24,378 cycles
INSPECTION FOUND NR 1 GALLEY SUPPORT FITTINGS (TWO EACH) CORRODED IN FASTENER HOLES AT STA 160, RBL 44 AND RBL 50. THE FITTINGS WERE REMOVED AND NEW FITTINGS WERE INSTALLED IAW SRM 51-30-5, 51-10-4, AND 51-10-3.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 52,294 hrs · 24,378 cycles
INSPECTION FOUND FORWARD ENTRY FLOOR SUPPORT CORRODED AT FS 140-150, RBL 54. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-5, 51-30-2, AND 51-30-4.
Part: DOUBLER — CHAFED (CARGO DOOR) · airframe 52,294 hrs · 24,378 cycles
INSPECTION FOUND DOUBLER AT FORWARD LOWER CORNER OF FORWARD CARGO DOOR CHAFED. THE DOUBLER WAS REMOVED AND A NEW DOUBLER WAS INSTALLED IAW SRM 51-10-4, 51-30-2, AND 51-10-3.
Part: DOOR FRAME — BROKEN (CARGO DOOR) · airframe 52,294 hrs · 24,378 cycles
INSPECTION FOUND A 2 INCH PIECE BROKEN OUT OF AFT CARGO DOOR FRAME CUTOUT AT AFT UPPER EDGE, BS 1211, LONGERON 21R. THE FRAME CUTOUT WAS REMOVED AND REPLACED IAW SRM 51-30-5.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 52,294 hrs · 24,378 cycles
INSPECTION FOUND LT O/B SEAT TRACKS CORRODED AT FS 807-1136 AND AT STA 1136-1309. THE SEAT TRACKS WERE REMOVED AND NEW TRACKS WERE INSTALLED IAW SRM 51-10-4, 51-10-3, 51-30-1, 51-30-2, AND 51-10-2.
Part: CARGO TRACK — CORRODED (FS 218-522) · airframe 52,294 hrs · 24,378 cycles
INSPECTION FOUND FORWARD CARGO LT TIE DOWN TRACK CORRODED BETWEEN FS 218 AND 522. THE TIE DOWN TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-30-1 AND 51-30-2.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 52,294 hrs · 24,378 cycles
INSPECTION FOUND LT CENTER SEAT TRACK CORRODED AT FS 1032-1309. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED USING A SPLICE REPAIR IAW SRM 51-30-1, 51-10-4, 53-05, FIGURE 4, 51-30-5, AND 51-30-2.
Part: WEB — CORRODED (FUSELAGE) · airframe 52,294 hrs · 24,378 cycles
INSPECTION FOUND FORWARD ENTRY CUSP WEB CORRODED AT FS 200-205, RBL 49-54 ON AFT SIDE OF FLOORBEAM. THE CORRODED SECTION OF CUSP WEB WAS CUT OUT AND A REPAIR DOUBLER AND FILLER WERE INSTALLED IAW SRM 51-10-3, 51-30-2, AND 51-30-8.
Part: FITTING — CORRODED (FUSELAGE) · airframe 52,294 hrs · 24,378 cycles
INSPECTION FOUND NR 1 GALLEY SUPPORT MOUNT FITTING CORRODED AT STA 160, RBL 12. THE GALLEY SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-5.
Part: DOUBLER — CHAFED (CARGO DOOR) · airframe 52,294 hrs · 24,378 cycles
INSPECTION FOUND FORWARD LOWER CORNER OF MID CARGO DOOR CHAFED. THE REPAIR DOUBLER WAS REMOVED AND A NEW DOUBLER WAS INSTALLED IAW SRM 51-10-4 AND 51-30-2.
Part: SKIN — DENTED (STA 1322) · airframe 52,294 hrs · 24,378 cycles
INSPECTION FOUND AFT FUSELAGE LT LOWER SKIN DENTED AT STA 1322, LONGERON 27L-28L. A DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38, 51-10-4, AND 51-10-3.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,294 hrs · 24,378 cycles
INSPECTION FOUND TOP OF FLOORBEAM CORRODED AROUND NUTPLATE HOLES IN R/H AFT LAV AT FS 1322, RBL 17 TO RBL 53. A REPAIR ANGLE WAS INSTALLED IAW SRM 53-05, FIGURE 20A AND 51-30-05.
Part: WEB — CORRODED (FUSELAGE) · airframe 52,294 hrs · 24,378 cycles
INSPECTION FOUND LT CUSP WEB CORRODED AT FS 1140 (L-2 DOOR). THE CUSP WEB WAS REMOVED AND A DOUBLER AND FILLER WERE INSTALLED IAW SRM 51-10-4, 53-14-3, AND 51-30-2.
Part: SKIN — DENTED (FUSELAGE) · airframe 52,294 hrs · 24,378 cycles
INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 294 BETWEEN LONGERON 24 AND 25L AND AT STA 225, L16L. A DOUBLER WAS INSTALLED AT EACH LOCATION IAW SRM 53-04, FIGURE 38, 51-10-3, AND 51-30-02.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 52,294 hrs · 24,378 cycles
INSPECTION FOUND FORWARD ENTRY SUB FLOOR AND ATTACHING STRUCTURE CORRODED AT FS 160-200, RBL 54. TORQUE BOX STRAP, SUB FLOOR ATTACH ANGLES, AND DOUBLER WERE REMOVED IAW SRM 51-30-5 AND 51-30-2. DOUBLERS WERE INSTALLED IAW SRM 51-30-2 AND 51-30-5.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 52,294 hrs · 24,378 cycles
INSPECTION FOUND CABIN RT CENTER SEAT TRACK CORRODED AT STA 225. THE SEAT TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-30-1, 53-05, FIGURE 4F, AND 51-30-5.
Part: SKIN — DENTED (FUSELAGE) · airframe 52,294 hrs · 24,378 cycles
INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 270, LONGERON 17L. A DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38, SHEET 21 AND 51-30-0.
Part: SKIN — DENTED (FUSELAGE) · airframe 52,294 hrs · 24,378 cycles
INSPECTION FOUND RT FUSELAGE SKIN DENTED AT STA 237-256. A DOUBLER AND FILLER WERE INSTALLED IAW SRM 53-04, FIGURE 38 AND 53-04.
Earlier reports · 1995–1999 · 17 reports
1999
Part: SENSOR — INOP (NLG)
THE NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION LEAVING IAH. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NOSE GEAR DOWNLOCK PROXIMITY SENSOR AT FAULT. THE NOSE GEAR DOWNLOCK PROXIMITY SENSOR WAS REMOVED AND REPLACED IAW MM 32-60-05. A NOSE GEAR SWING WAS PERFORMED AND ALL INDICATIONS WERE NORMAL.
1998
Part: CABLE — OUT OF ADJ (TAIL CONE)
THE AFT ENTRY DOOR TAILCONE RELEASE PULLED HIGH AT 25 POUNDS. THE CABLE AND CONDUIT WERE REPLACED AND AN ADJUSTMENT/TEST WAS PERFORMED IAW MM 53-53-00.
Part: LONGERON — CORRODED (BS 1231)
INSPECTION FOUND LONGERON 24L CORRODED IN AFT CARGO COMPARTMENT AT STA 1231. REPAIRED IAW SRM 53-02, FIGURE 18.
Part: BEAM — CRACKED (SERVICE DOOR)
INSPECTION FOUND A CRACK IN FORWARD SERVICE DOOR LOWER BEAM. THE LOWER BEAM WAS REPLACED IAW SRM 51-30-2.
Part: DOUBLER — CORRODED (BS 1309)
CORROSION IN AFT BAG BIN AT STA 1309 JUST ABOVE LONGERON 23 LEFT SIDE. REMOVED AND REPLACED DOUBLER PER 51-30-02.
Part: JAMB — CORRODED (CARGO DOORWAY)
MBB DOOR JAMB BEAM CORRODED. REMOVED AND REPLACED BEAM PER SRM 51-30-02 AND 51-30-05.
Part: STRUT — FLAT (NLG)
THE NLG WOULD NOT RETRACT AFTER TAKEOFF. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NLG STRUT FLAT. A NEW GLAND NUT WAS INSTALLED AND THE STRUT WAS REPACKED.
Part: SUPPORT — CRACKED (VERT STAB)
INSPECTION FOUND A .375 INCH CRACK AT LOWER RIVET HOLE IN FORWARD LEFT VERTICAL STABILIZER SPAR SUPPORT AT 37.3 INCHES AFT OF STA 1089.3 IN TAIL COMPARTMENT ABOVE CATWALK. THE AREA WAS REPAIRED IAW SRM 55-02, FIGURE 26.
1997
Part: OIL SCREEN COVER — LEAKING (NR 1 ENGINE)
THE NR 1 ENGINE OIL QUANTITY DROPPED TO ZERO FOLLOWED BY OIL PRESSURE DECREASING TO 10 PSI AFTER TAKEOFF. THE AIRCRAFT WAS RETURNED TO LAX WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND PLUG ON MAIN OIL SCREEN COVER LEAKING. A NEW OIL SCREEN COVER ASSEMBLY WAS INSTALLED AND THE ENGINE WAS SERVICED WITH OIL. LEAK AND OPERATIONAL CHECKS WERE GOOD.
Part: FAN — INOPERATIVE (CABIN)
LIGHT SMOKE WAS REPORTED IN CABIN WHILE EN ROUTE TO SEA. THE RECIRCULATION FAN CIRCUIT BREAKER WAS PULLED AND THE SMOKE CLEARED. THE AIRCRAFT LANDED AT SEA WITHOUT FURTHER PROBLEM. MAINTENANCE FOUND THE AIR DISTRIBUTION FAN AT FAULT. THE FAN WAS REMOVED AND REPLACED AND OPERATIONAL CHECKS WERE GOOD.
1996
Part: SUPPORT LEG — CRACKED (SPOILER)
FOUND OUTBOARD SUPPORT BRACKET OF LEFT HAND GROUND SPOILER UPPER AFT LEG WITH ONE INCH CRACK IN SUPPORT LEG. REPLACED CROSS BRACE PER EC/RA 5710-01756.
Part: GCU — INOPERATIVE (APU)
WHILE OPERATING THE APU DURING CRUISE FLIGHT WITH THE LEFT GENERATOR PLACARDED INOPERATIVE, THE APU GENERATOR TRIPPED OFF. THE FAILURE WAS ACCOMPANIED BY AN AC CROSSTIE LOCKOUT LIGHT. THE APU GENERATOR WAS RESET AND POWER WAS RESTORED. MAINTENANCE REMOVED AND REPLACED THE APU GENERATOR CONTROL UNIT PER MM 24-20-07 AND OPERATION CHECKED GOOD. PART TOTAL CYCLES, 14,523.
Part: BATTERIES — DISCHARGED (COCKPIT)
THE OVERHEAD EMERGENCY LIGHTS IN COCKPIT WOULD ONLY ILLUMINATE FOR FIVE SECONDS WHEN SELECTED. THE BATTERIES FOR COCKPIT EMERGENCY LIGHTS WERE REPLACED AND OPERATION OF LIGHTS WAS RESTORED.
Part: CONNECTORS — INOPERATIVE (NR 1 ENGINE)
THE NR 1 ENGINE FIRE WARNING LIGHT ILLUMINATED WHILE EN ROUTE. THE THROTTLE WAS RETARDED AND THE LIGHT EXTINGUISHED, THE LIGHT CAME BACK ON DURING APPROACH TO CLE. THE NR 1 ENGINE WAS SHUT DOWN AND THE FIRE BOTTLE WAS DISCHARGED AS A PRECAUTIONARY MEASURE. THE AIRCRAFT LANDED WITHOUT INCIDENT. TWO LOOP CONNECTORS ON LOWER A-LOOP OF NR 1 ENGINE WERE FOUND AT FAULT. THE LOOP CONNECTORS WERE REMOVED AND REPLACED. IN ADDITION, THE FIRE DETECTION UNIT AND A AND B LOOP SWITCHES WERE REPLACED AS A PRECAUTIONARY MEASURE. ALSO, THE FIRE BOTTLE WAS REPLACED. THE FIRE DETECTION SYSTEM TESTED NORMALLY.
1995
Part: OVENS — FAILED (GALLEY)
SFO - FLT 0151 - THE GALLEY POWER NR 2 PHASE 'A' 50 AMP CIRCUIT BREAKER ON AFT COCKPIT BULKHEAD TRIPPED DURING FLIGHT AND WAS ACCOMPANIED BY THE COPILOT'S INSTRUMENTS SHOWING FLAGS MOMENTARILY. THE FLIGHT ATTENDANT ALSO REPORTED SPARKS COMING FROM BEHIND OVENS LOCATED IN FIRST CLASS. THE SPARKS CEASED AFTER PULLING CIRCUIT BREAKERS. THE CAMLOCK RETAINER WAS REMOVED. THE OVENS LOCATED IN FIRST CLASS WERE PLACARDED INOPERATIVE AND THE CIRCUIT BREAKERS WERE PULLED AND COLLARED.
Part: TARGET — OUT OF ADJUST (LT MLG)
CLE - FLT 1473 - THE LT MLG RED UNSAFE LIGHT REMAINED ILLUMINATED AFTER TAKEOFF. CYCLING THE GEAR DID NOT HELP. THE LIGHT EXTINGUISHED WHILE ON DESCENT. MAINTENANCE FOUND THE LT MLG UPLOCK SENSOR TARGET OUT OF ADJUSTMENT. THE TARGET/SENSOR WAS ADJUSTED PER MM 32-60-05 AND GEAR OPERATION AND INDICATIONS CHECK GOOD. (X)
Part: BLADE — FAILED (3RD STG TURBINE)
MIA - FLT 0292 - A LOUD BANG WAS HEARD AND THE NR 1 ENGINE SPOOLED DOWN DURING A CLIMB OUT OF MIA AT 18,000 FEET. THE AIRCRAFT WAS RETURNED TO MIA WHERE IT LANDED WITHOUT INCIDENT. THE NR 1 ENGINE WAS REMOVED AND REPLACED. THE SDR WILL REMAIN OPEN FOR PART INFORMATION PENDING INVESTIGATION. SUPPLEMENT - INVESTIGATION REVEALED THE PRIMARY CAUSE OF ENGINE FAILURE WAS DUE TO FAIILURE OF A THIRD STAGE TURBINE BLADE. (X)