# N411EA: 1977 Mcdonnell Douglas DC-9-51, registration cancelled 2002-10-02

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: October 2, 2002
- Exported to: Uganda
- Status when cancelled: Valid registration
- Airframe: [Mcdonnell Douglas DC-9-51](https://openairdocs.org/model/mcdonnell-douglas-dc-9-51) (registry code 3022051)
- Engine: [Pratt & Whitney JT8D-9 series](https://openairdocs.org/engine/pratt-whitney-jt8d-9-series) (registry code 52048)
- Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs)
- Serial number: 47732
- Year built: 1977
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: August 26, 1977
- Certificate issued: April 29, 2002
- Last registry action: July 2, 2002
- Mode S code: A4D83C
- Owner when cancelled: [Boeing Capital Loan Corp](https://openairdocs.org/faa-owner/BOEING%20CAPITAL%20LOAN%20CORP)
- Location: [Las Vegas, NV](https://openairdocs.org/faa-place/NV/Las%20Vegas)
- Owner type: Corporation
- Owner's area on the map: 36.0845° N, 115.1461° W: Placed by OpenAirDocs at the center of ZIP code 89119, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N411EA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=411EA
- Page: https://openairdocs.org/deregistered/N411EA-2002-10-02

From the FAA registry file of November 5, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Mcdonnell Douglas DC-9-51: https://openairdocs.org/model/mcdonnell-douglas-dc-9-51.md

## Service difficulty reports (34)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR WXOA01012B](https://openairdocs.org/sdr/WXOA01012B), Aug 21, 2001: STRINGER. CRACKED. LAS - AIRCRAFT FUSELAGE DAMAGED BY GROUND SERVICE EQUIPMENT WITH AIRCRAFT POSITIONED AT GATE. DAMAGE IDENTIFIED AS PUNCTURED FUSELAGE SKIN AT FUSELAGE STATION 1
- [SDR WXOA01011](https://openairdocs.org/sdr/WXOA01011), Aug 13, 2001: TERMINAL. CORRODED. FAT - DURING AIRCRAFT SCHEDULED INSPECTION, FOUND EMERGENCY LIGHTS INOPERATIVE IN TAILCONE COMPARTMENT. MAINTENANCE FOUND CORRODED TERMINAL CONNECTION. CLEANED 
- [SDR WXOA01010](https://openairdocs.org/sdr/WXOA01010), Aug 7, 2001: LIGHT. INOPERATIVE. FAT - DURING AIRCRAFT SCHEDULED INSPECTION, FOUND EMERGENCY LIGHTS INOPERATIVE IN TAILCONE COMPARTMENT. MAINTENANCE FOUND INOPERATIVE BULBS. RELAMPED LIGHTS. EM
- [SDR WXOA01009](https://openairdocs.org/sdr/WXOA01009), Aug 1, 2001: LIGHT. INOPERATIVE. FAT - DURING AIRCRAFT SCHEDULED INSPECTION, FOUND CABIN EMERGENCY LIGHTS INOPERATIVE AT STATION 1167 (AFT CABIN EXIT DOOR AREA). MAINTENANCE FOUND LOOSE WIRE CO
- [SDR WXOA00032](https://openairdocs.org/sdr/WXOA00032), Nov 14, 2000: FLOOR SUPPORT. CORRODED. MHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, FORWARD CABIN FLOOR STRUCTURE AT FUSELAGE STATION 188, RBL 45, FLOOR SUPPORT SHOWS EVIDENCE OF LEV
- [SDR WXOA00031](https://openairdocs.org/sdr/WXOA00031), Nov 14, 2000: ANGLE. CORRODED. MHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, AFT AIRSTAIR, 4TH STAIR FROM TOP SHOWS EVIDENCE OF LEVEL 2 CORROSION ON BACK AND LOWER SURFACE OF 
- [SDR WXOA00030](https://openairdocs.org/sdr/WXOA00030), Nov 14, 2000: SUPPORT. CORRODED. MHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, AFT CARGO PIT AT FUSELAGE STATION 1167 STRINGER 30, CENTER VERTICAL SUPPORT POST SHOWS EVIDENCE OF
- [SDR WXOA00029](https://openairdocs.org/sdr/WXOA00029), Nov 14, 2000: SKIN. CORRODED. MHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, AFT CARGO PIT AT FUSELAGE STATION 1167 STRINGER R28, STRINGER TO FRAME TIE IN SHOWS EVIDENCE OF MO
- [SDR WXOA00028](https://openairdocs.org/sdr/WXOA00028), Nov 14, 2000: WEB. CORRODED. MHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, FORWARD CARGO DOOR LOWER TORQUE BOX WEB TWO EACH P/N 391Z-509-1 STAINLESS TEAR STRAPS AND P/N'S 59
- [SDR WXOA00027](https://openairdocs.org/sdr/WXOA00027), Nov 14, 2000: PAN. CORRODED. MHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, FOUND LEVEL 2 CORROSION AT FORWARD CARGO DOOR LOWER PAN. REPAIRED/SPLICED FORWARD CARGO DOOR LOWER
- [SDR WXOA00012](https://openairdocs.org/sdr/WXOA00012), Nov 14, 2000: FLOORBEAM. CRACKED. MHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, FOUND CRACK IN CABIN FLOORBEAM AT FS 1080, LBL 45, STRINGER 18 FLOOR WEB. CRACK REPORTED APPROXIMA
- [SDR WXOA00015](https://openairdocs.org/sdr/WXOA00015), Nov 14, 2000: RETAINER. DAMAGED. MHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, FOUND RIGHT WING INBOARD PANEL NR 2214A TO HAVE DAMAGED RETAINER. REMOVED DAMAGED SECTION OF RETAI
- [SDR WXOA00014](https://openairdocs.org/sdr/WXOA00014), Nov 14, 2000: SEAL. CRACKED. MHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, FOUND LEFT WING INBOARD FILLET PANEL METAL RUB SEAL DAMAGED. REMOVED DAMAGED RUB SEAL, FABRICATED 
- [SDR WXOA00013](https://openairdocs.org/sdr/WXOA00013), Nov 14, 2000: SKIN. CRACKED. MHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, FOUND CRACK IN LEFT WING VERTICAL VANE. STOP DRILLED CRACK AND FABRICATED AND INSTALLED DOUBLER PE
- [SDR WXOA00026](https://openairdocs.org/sdr/WXOA00026), Nov 14, 2000: SKIN. DENTED. MHV - DURING AIRCRAFT SCHEDULED INSPECTIN AT REPAIR STATION, FOUND THREE DENTS WITH GOUGES EXISTING ADJACENT TO EXISTING REPAIR AT FUSELAGE STATION 207 TO 229, 
- [SDR WXOA00024](https://openairdocs.org/sdr/WXOA00024), Nov 14, 2000: SKIN. DENTED. MHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, FOUND FUSELAGE SKIN DENT AT FS 283, WL 170. REMOVED DAMAGE AND REPAIRED IAW DC9 SRM 53-04, FIGURE 
- [SDR WXOA00025](https://openairdocs.org/sdr/WXOA00025), Nov 14, 2000: INTERCOSTAL. CRACKED. MHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, FOUND FUSELAGE INTERCOSTAL CRACKED AT FUSELAGE STATION 361, STRINGER 19R. FABRICATED REPLACEMENT I
- [SDR WXOA00023](https://openairdocs.org/sdr/WXOA00023), Nov 14, 2000: SKIN. GOUGED. MHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, FOUND RIGHT FUSELAGE SKIN GOUGED AT FS 522, WL 175. RESULTING GOUGE AND DENT MEASURES .053 INCH DE
- [SDR WXOA00022](https://openairdocs.org/sdr/WXOA00022), Nov 14, 2000: LONGERON. CUT. MHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, FOUND FUSELAGE LONGERON SPLICE AT 17L AND STATION 229 DAMAGED. REMOVED DAMAGED SPLICE, FABRICATED 
- [SDR WXOA00021](https://openairdocs.org/sdr/WXOA00021), Nov 14, 2000: STRINGER. CRACKED. MHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, FOUND FUSELAGE STRINGER 17L CRACKED AROUND FASTENERS BETWEEN FRAME 237 AND 255. REMOVED AND REPLAC
- [SDR WXOA00020](https://openairdocs.org/sdr/WXOA00020), Nov 14, 2000: PLATE. CORRODED. MHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, FOUND CORROSION AT FUSELAGE STATION 465 UNDER VHF ANTENNA AT BASE PLATE. REMOVED SURFACE CORROSION
- [SDR WXOA00019](https://openairdocs.org/sdr/WXOA00019), Nov 14, 2000: ANGLE. CRACKED. MHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, FOUND TWO STRUT SUPPORT ANGLES CRACKED AT NOSE LANDING GEAR NOSE WHEEL WELL AREA FUSELAGE STATION 
- [SDR WXOA00018](https://openairdocs.org/sdr/WXOA00018), Nov 14, 2000: SKIN. DENTED. MHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, FOUND RIGHT WING FLAP TRAILING EDGE LOWER SURFACE TO HAVE A DENT. DIMENSIONS OF DENT .800 INCH BY 
- [SDR WXOA00017](https://openairdocs.org/sdr/WXOA00017), Nov 14, 2000: SKIN. DAMAGED. MHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, FOUND RIGHT WING UPPER SKIN SURFACE FORWARD OF OUTBOARD SPOILER HAS CRACK. REMOVED DAMAGED AREA OF
- [SDR WXOA00016](https://openairdocs.org/sdr/WXOA00016), Nov 14, 2000: SKIN. DAMAGED. MHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, FOUND RIGHT WING UPPER SKIN SURFACE INBOARD OF INBOARD SPOILER HAS CRACK AROUND THREE RIVETS AT ST
- [SDR TWAA9816504](https://openairdocs.org/sdr/TWAA9816504), Oct 7, 1998: BULKHEAD. CORRODED. DURING CHECK-C MAINT, FOUND AFT CARGO BIN WITH CORROSION AT BOTTOM OF AFT PRESSURE BULKHEAD, STA 1168, LBL 1 IN. INSTALLED NEW T PART NR 5910130-65, AND NEW GUS
- [SDR TWAA9813801](https://openairdocs.org/sdr/TWAA9813801), Aug 26, 1998: CONTROL CABLE. BROKEN. DURING TAXI TOWARD THE GATE IN A 90 DEGREE RIGHT ANGLE TURN CREW HEARD LOUD SNAP AND LOST NOSE WHEEL STEERING. ACFT WAS TOWED INTO GATE. REPLACED BROKEN STEERIN
- [SDR TWAA9810202](https://openairdocs.org/sdr/TWAA9810202), Jun 25, 1998: BOLT. BROKEN. STL - FLT 617 - AFTER TAKEOFF FROM SGF, THE RT MAIN LANDING GEAR WOULD NOT RETRACT. OPERATED SGF TO STL WITH RT GEAR EXTENDED AT REDUCED AIR SPEED. FOUND RT MLG
- [SDR TWAA9714902](https://openairdocs.org/sdr/TWAA9714902), Dec 17, 1997: BEARING. FAILED. STL - FLT 676 - DURING CRUISE, AT FL330, RT ENGINE RUMBLED AND COMPRESSOR STALL WAS EXPERIENCED. REPLACED RT ENGINE. ENGINE WAS DISASSEMBLED AND NR 3 BEARING WA
- [SDR TWAA9727001](https://openairdocs.org/sdr/TWAA9727001), Feb 20, 1997: TIRE. FAILED. STL - DURING TAKEOFF , NR 3 MAIN TIRE BLEW OUT. REMOVED AND REPLACED NR 3 MAIN TIRE, MFG P/N 9560859-7. FUNCTIONAL CHECK NORMAL. (M)
- [SDR TWAA9708003](https://openairdocs.org/sdr/TWAA9708003), Jan 13, 1997: LINK ASSY. MALFUNCTIONED. HOU - AFTER TAKEOFF WHEN LANDING GEAR WAS RETRACTED, RIGHT NOSE LANDING GEAR DOOR DID NOT CLOSE. FOUND RIGHT NOSE LANDING GEAR DOOR LINK ASSEMBLY, MFG P/N 39567
- [SDR TWAA9614801](https://openairdocs.org/sdr/TWAA9614801), Nov 29, 1996: CONTROL CABLE. BROKEN. STL - FLT 627 - AFTER TAKEOFF WHEN LANDING GEAR WAS RETRACTED, HAD LOUD NOISE FROM NOSE LANDING GEAR AND UNSAFE LIGHT REMAINED ILLUMINATED. FOUND RIGHT NOSE LAN
- [SDR 96ZZZM1526](https://openairdocs.org/sdr/96ZZZM1526), Oct 21, 1996: RETRACT MECH. LACK OF LUBE. STL - AFTER TAKEOFF HAD VIBRATION FROM NOSE LANDING GEAR DOORS AFTER LANDING GEAR RETRACTION. CYCLED LANDING GEAR. FOUND RIGHT NOSE LANDING GEAR DOOR BUNGEE LIN
- [SDR 96ZZZX3656](https://openairdocs.org/sdr/96ZZZX3656), Jun 2, 1996: WIRE. BROKEN. HOU - FLT 639 - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED, NOSE LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED. CYCLED LANDING GEAR. FOUND BROKEN WIRE AT N

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB MIA84IA242](https://openairdocs.org/ntsb/MIA84IA242), Aug 25, 1984: Mcdonnell Douglas DC-9-51 (N411EA), Orlando, FL, incident, minor damage

## FAA accident and incident reports (3)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 19951214045719I](https://openairdocs.org/incident/19951214045719I), Dec 14, 1995: Doug DC951 (N411EA), Little Rock, AR, Minor damage. Narrative: history of flight; on December 15, 1995, flight #227 from st. louis, MO to Little Rock, AR a DC-9-51, N411EA, operated by trans world airlines…
- [Incident 19870713044899I](https://openairdocs.org/incident/19870713044899I), Jul 13, 1987: Doug DC951 (N411EA), Washington, DC. Landed after loss of oil quantity in engine. Found faulty scavenge pump.
- [Incident 19840825070049I](https://openairdocs.org/incident/19840825070049I), Aug 25, 1984: Doug DC951 (N411EA), Orlando, FL, Minor damage. Tire or tires in left main gear blew out. Aborted takeoff. Flying tire and wheel rim darts made holes in skin.

## Other aircraft with N411EA

- [Registered now](https://openairdocs.org/aircraft/N411EA): Tomark Aero CZ Sro VIPER SD-4, S/N 41118, built 2023

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