# N513AA: 1990 Mcdonnell Douglas DC-9-82(MD-82), registration cancelled 2019-09-06 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: September 6, 2019 - Status when cancelled: Sale reported, canceled - Airframe: [Mcdonnell Douglas DC-9-82(MD-82)](https://openairdocs.org/model/mcdonnell-douglas-dc-9-82-md-82) (registry code 3022082) - Engine: [Pratt & Whitney JT8D series](https://openairdocs.org/engine/pratt-whitney-jt8d-series) (registry code 52053) - Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (OpenAirDocs) - Serial number: 49890 - Year built: 1990 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard - Airworthiness date: March 5, 1990 - Last registry action: December 7, 2018 - Mode S code: A66C95 - Location: [Miami, FL](https://openairdocs.org/faa-place/FL/Miami) - Owner type: Individual - Owner's area on the map: 25.7743° N, 80.1937° W: Placed by OpenAirDocs: center of Miami, FL, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N513AA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=513AA - Page: https://openairdocs.org/deregistered/N513AA-2019-09-06 From the FAA registry file of November 4, 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-9-82(MD-82): https://openairdocs.org/model/mcdonnell-douglas-dc-9-82-md-82.md ## Service difficulty reports (164, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR AALA201706289025](https://openairdocs.org/sdr/AALA201706289025), Jun 27, 2017: RELAY. FAULTY. THE AIRCRAFT WAS GROUNDED. R CSD WARN LIGHT (LOW OIL PRESS) FIRST THEN R GEN INOP. DISCONNECTED R CSD PER PROCEDURE. APU WOULD NOT START AT 30,000 OR 28,000 OR - [SDR AALA20170628001](https://openairdocs.org/sdr/AALA20170628001), Jun 27, 2017: CSD. INOPERATIVE. THE AIRCRAFT WAS GROUNDED. R CSD WARN LIGHT (LOW OIL PRESS) FIRST THEN R GEN INOP. DISCONNECTED R CSD PER PROCEDURE. APU WOULD NOT START AT 30,000 OR 28,000 OR - [SDR AALA20170215008](https://openairdocs.org/sdr/AALA20170215008), Feb 12, 2017: HINGE PIN. MIGRATED. AIRCRAFT WAS GROUNDED. FIRST OFFICER SLIDING WINDOW HAS A HINGE PIN ON THE AFT LOCK BAR MIGRATING UPWARD. REPOSITIONED HINGE PIN AND REATTACHED LOWER AFT LINKAG - [SDR AALA20170109026](https://openairdocs.org/sdr/AALA20170109026), Jan 5, 2017: BALLAST. BURNED. DURING MANEUVERING FOR LANDING, THE ENTIRE CABIN AND COCKPIT EXPERIENCED AN UNUSUAL ODOR LASTING 3 OR 4 MINUTES. NO SMOKE OR HAZE PRESENT. AIRCRAFT WAS GROUNDED - [SDR AALA20161101004](https://openairdocs.org/sdr/AALA20161101004), Oct 29, 2016: SOLENOID VALVE. LEAKING. AIRCRAFT NOT GROUNDED. SMOKE AND ODOR IN CABIN PRIOR TO PUSHBACK FROM GATE DUE TO APU DE-OIL SOLENOID VALVE LEAKING OIL INTO INTAKE. REMOVED AND REPLACED VALVE - [SDR AALA20160424003](https://openairdocs.org/sdr/AALA20160424003), Apr 24, 2016: BOOT. DISCONNECTED. AIRCRAFT WAS GNDED. AIR INTERRUPT, DURING CLIMB THE TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. FOUND THE OUTFLOW DUCT CONNECTOR BOOT OFF AT THE AIR CY - [SDR AALA20160405017](https://openairdocs.org/sdr/AALA20160405017), Apr 5, 2016: WEB. CRACKED. AIRCRAFT WAS IN BASE MX. FWD ENTRY DOOR INTERNAL WEB SKIN IS CRACKED AT THE TOP FWD CORNER AT CROSSBEAM & NR 1 BEAM. REPAIRED WEB IAW EA 259387 DATED 4 5 16. - [SDR AALA20160404007](https://openairdocs.org/sdr/AALA20160404007), Apr 4, 2016: FRAME. WORN. AIRCRAFT WAS IN BASE MX. LT SIDE OF AFT ACCESSORY FRAME STRUCTURE IS WORN AT CANT 1510, BETWEEN LONGERON 28L & 30L. ACCOMPLISHED REPAIR IAW EA 259344. - [SDR AALA20160325002](https://openairdocs.org/sdr/AALA20160325002), Mar 24, 2016: PORTABLE LIGHT. FAULTY. AIRCRAFT WAS NOT GNDED. PORTABLE EMER LIGHT ASSEMBLY AT L1 DOOR WILL NOT SHUT OFF. R & R LIGHT ASSEMBLY IAW AMM 33-53-00. SYS CHECKED NORMAL. - [SDR AALA20160325001](https://openairdocs.org/sdr/AALA20160325001), Mar 24, 2016: BATTERY. DISCHARGED. AIRCRAFT WAS NOT GNDED. EMER LIGHTS BETWEEN AFT LAVATORIES WILL NOT TEST. R & R EMER LIGHT BATTERY ASSEMBLY IAW AMM 33-53-00. SYS CHECKED NORMAL. - [SDR AALA20151120002](https://openairdocs.org/sdr/AALA20151120002), Nov 20, 2015: LONGERON. CRACKED. CRACK FOUND AT FASTENER HOLE, UPPER FLANGE ON LONGERON 23L AT STATION 200. REPAIRED WITH SPLICE REPAIR IAW SRM 53-02-00. - [SDR AALA20150826004](https://openairdocs.org/sdr/AALA20150826004), Aug 25, 2015: BATTERY PACK. DISCHARGED. OVERHEAD EMER LIGHTS INOPERATIVE IN ROWS 3 & 6. R & R BATTERY PACK AT CTR AISLE AT FWD LAVATORY IAW WDM 33- 51-11. SYS CHECKED NORMAL. SEE ALSO AALA20150825022. - [SDR AALA20150825022](https://openairdocs.org/sdr/AALA20150825022), Aug 25, 2015: BATTERY PACK. DISCHARGED. OVERHEAD EMER LIGHTS INOPERATIVE IN ROWS 3 & 6. R & R BATTERY PACK AT ROW 5 IAW WDM 33- 51-11. SYS CHECKED NORMAL. - [SDR AALA20150825021](https://openairdocs.org/sdr/AALA20150825021), Aug 25, 2015: BATTERY. DISCHARGED. OVERHEAD EMER LIGHTS INOPERATIVE AT ROWS 12 - 15. R & R BATTERY AT ROW 13 IAW WDM 33-51-11. SYS CHECKED NORMAL. - [SDR AALA20150825020](https://openairdocs.org/sdr/AALA20150825020), Aug 25, 2015: WIRE HARNESS. FAULTY. SEAT MOUNTED EMER LIGHT AT 13DEF INOPERATIVE. INSTALLED SERVICEABLE WIRE HARNESS AT ROW 13DEF IAW WDM 33-51-11. SYS CHECKED NORMAL. - [SDR AALA20150326002](https://openairdocs.org/sdr/AALA20150326002), Mar 25, 2015: BATTERY PACK. DISCHARGED. AFT CABIN EMER LIGHTS BETWEEN LAVATORIES WON`T TEST. REPLACED EMER LIGHT CABIN BATTERY PACK FOR AFT AISLE LIGHTS IAW AMM 33-53-00. SYS CHECKED NORMAL. - [SDR AALA20150326001](https://openairdocs.org/sdr/AALA20150326001), Mar 25, 2015: CONTROL MODULE. FAULTY. FORWARD EMER PATH LIGHTS WON`T TEST USING PACK AB5-1. R & R AB5-1 EMER PATH LIGHTING CONTROL MODULE IAW AMM 33-60-00. SYS CHECKED NORMAL. - [SDR AALA20141013006](https://openairdocs.org/sdr/AALA20141013006), Oct 13, 2014: BRACKET. CRACKED. MID CARGO DOOR STOP PAD CRACKED ON FWD SIDE. REMOVED & INSTALLED SERVICEABLE BRACKET. - [SDR AALA20141013005](https://openairdocs.org/sdr/AALA20141013005), Oct 13, 2014: BRACKET. CRACKED. CARGO DOOR STOP PAD BRACKET CRACKED. REMOVED & INSTALLED SERVICEABLE BRACKET. - [SDR AALA20141010002](https://openairdocs.org/sdr/AALA20141010002), Oct 10, 2014: SHEAR TIE. CRACKED. SHEAR TIE CRACKED AT STATION 1437 OTBD OF LONGERON 2 RT. INSTALLED NEW SHEAR TIE IAW DWG 9911840, AARD 51-00-05-1 & SRM 53-05-00-001 FIGURE 99. - [SDR AALA20141010001](https://openairdocs.org/sdr/AALA20141010001), Oct 10, 2014: SHEAR TIE. CRACKED. SHEAR TIE CRACKED AT STATION 1437 & LONGERON 2 LT. REPLACED CLIP IAW DWG 9911840, SRM 53-05-00-001 FIGURE 99 & AARD 51-00-05-1 REPAIR 1. - [SDR AALA20140924007](https://openairdocs.org/sdr/AALA20140924007), Sep 24, 2014: FORMER. CRACKED. RIGHT WING LE NR 4 SLAT TRACK INBD FORMER IS CRACKED. INSTALLED RT WING NR 4 INBD FORMER DOUBLER & HAT BUSHING IAW WORK CARD 57-98-06. - [SDR AALA20140924006](https://openairdocs.org/sdr/AALA20140924006), Sep 24, 2014: FORMER. CRACKED. LEFT WING LE NR 4 SLAT TRACK INBD FORMER IS CRACKED. INSTALLED LT WING NR 4 SLAT INBD FORMER DOUBLER & HAT BUSHING IAW WORK CARD 57-98-05. - [SDR AALA20130815011](https://openairdocs.org/sdr/AALA20130815011), Aug 15, 2013: BATTERY PACK. DISCHARGED. CABIN EMERGENCY LIGHT WOULD NOT ILLUMINATE. REPLACED BATTERY PACK FOR CABIN EMERGENCY LIGHTS. OPERATIONS CHECKED NORMAL. - [SDR AALA20130521015](https://openairdocs.org/sdr/AALA20130521015), May 21, 2013: SENSE LINE. DISCONNECTED. CREW REPORTED PRESSURIZATION FLUCTUATION, AUTO PILOT DISCONNECT AND CAPTAINS PITOT FAULT. EMERGENCY DECLARED FLIGHT DIVERTED LIT LANDED WITHOUT INCIDENT. ACFT R - [SDR AALA20130501016](https://openairdocs.org/sdr/AALA20130501016), May 1, 2013: SKIN. DENTED. FUSELAGE DENT AT STATION 207 BETWEEN LONGERON 4 AND 5 LEFT WITH DEEP GOUGE. REMOVED DAMAGE SKIN PER 53-04-03 AND INSTALLED DOUBLER PER SRM 53-04-03 FIGURE 3 AND - [SDR AALA20130501015](https://openairdocs.org/sdr/AALA20130501015), May 1, 2013: LONGERON. CRACKED. LONGERON 4 LEFT IS CRACKED AT STATION 200. INSTALLED LONGERON SPLICE PER SRM 53-02-00 FIGURE 18. - [SDR AALA20130424010](https://openairdocs.org/sdr/AALA20130424010), Apr 24, 2013: DOUBLER. CORRODED. CORROSION ON DOUBLER UNDER G2 GALLEY MOUNT AT STATION 218. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-20-00-16. - [SDR AALA20130423006](https://openairdocs.org/sdr/AALA20130423006), Apr 23, 2013: LONGERON. CRACKED. LONGERON 2 LEFT CRACKED AT STATION 160. CUT OUT SECTION OF LONGERON FROM STATIONS 150 TO 171 AND INSTALLED SPLICE REPAIR PER SRM 53-02, FIGURE 18. - [SDR AALA20130422032](https://openairdocs.org/sdr/AALA20130422032), Apr 22, 2013: CUSP WEB. CORRODED. CORROSION ON LOWER SIDE OF RIGHT CUSP AT STATION 218 BELOW NUMBER 6 SEAT TRACK. REMOVED CORRODED CUSP AND INSTALLED NEW CUSP PER AARD 51-00-05-1. - [SDR AALA20130421001](https://openairdocs.org/sdr/AALA20130421001), Apr 21, 2013: PAN. CRACKED. FORWARD CARGO DOOR, NUMBER 1 BEAM FORWARD SIDE PAN CRACKED. STOP DRILLED PER ESO 80174 AND INSTALLED DOUBLER PER EA COMP-52-029331. - [SDR AALA20130419018](https://openairdocs.org/sdr/AALA20130419018), Apr 19, 2013: SKIN. CRACKED. LEFT SIDE FUSELAGE SKIN CRACKED AT STATION 1309 ABOVE LONGERON 7 LEFT. INSTALLED DOUBLER PER SRM 53-04-00 FIGURE 32. - [SDR AALA20130419017](https://openairdocs.org/sdr/AALA20130419017), Apr 19, 2013: CUSP WEB. DAMAGED. DAMAGE TO RIGHT CUSP AT STATION 237 BETWEEN STRINGERS 5 AND 6. INSTALLED DOUBLER REPAIR PER AARD 53-20-00-16. - [SDR AALA20130419014](https://openairdocs.org/sdr/AALA20130419014), Apr 19, 2013: ATTACH ANGLE. CORRODED. FORWARD DOOR JAMB LOWER ATTACH ANGLE HAS CORROSION STATION 1155. REMOVED AND REPLACED DOOR JAMB ANGLE PER SRM 51-30-05. - [SDR AALA20130419010](https://openairdocs.org/sdr/AALA20130419010), Apr 19, 2013: SKIN. CRACKED. RIGHT SIDE OF FUSELAGE SKIN CRACKED AT STATION 1309 ABOVE LONGERON 7 RIGHT. INSTALLED REPAIR DOUBLER SRM 53-04-00 FIGURE 32. - [SDR AALA20130418009](https://openairdocs.org/sdr/AALA20130418009), Apr 18, 2013: CUSP WEB. CRACKED. FASTENER HOLE CRACKED IN CUSP AT STATION 187, RIGHT BUTTLINE 63. INSTALLED DOUBLER REPAIR PER AARD 53-20-00-16. - [SDR AALA20130418006](https://openairdocs.org/sdr/AALA20130418006), Apr 18, 2013: STIFFENER. CRACKED. CRACK IN VERTICAL SUPPORT AT STATION 1338 BELOW LONGERON 1 LEFT. REPLACED VERTICLE STIFFENER PER AARD 51-00-05-1. - [SDR AALA20130417018](https://openairdocs.org/sdr/AALA20130417018), Apr 17, 2013: CUSP WEB. CRACKED. RIGHT CUSP IS CRACKED AT STATION 1022. INSTALLED DOUBLER REPAIR PER AARD 53-20-00-16. - [SDR AALA20130416014](https://openairdocs.org/sdr/AALA20130416014), Apr 16, 2013: CUSP WEB. CRACKED. RIGHT CUSP SHEET IS CRACKED UNDER SEAT TRACK SPLICE AT STATION 800. REPALCED CUSP SHEET PER AARD 51-00-05-1. - [SDR AALA20130416012](https://openairdocs.org/sdr/AALA20130416012), Apr 16, 2013: PAN. CRACKED. FORWARD CARGO DOOR, NUMBER 1 BEAM FORWARD SIDE PAN CRACKED. ACCOMPLISHED NESTED ANGLE REPAIR PER EA COMP-52-029331 AND ESO 80174 PAGE 601B BASED ON SRM 52-03-00 - [SDR AALA20130416010](https://openairdocs.org/sdr/AALA20130416010), Apr 16, 2013: DOOR FRAME. CRACKED. DOOR FRAME WEB CRACKED AT SCREW GOUGE, STATION 634, LONGERON 27 RIGHT. INSTALLED DOUBLER PER AARD 53-10-00-24 FIGURE 1 (SHEET 3). - [SDR AALA20130415003](https://openairdocs.org/sdr/AALA20130415003), Apr 15, 2013: MEMBRANE. CORRODED. CORROSION ON SUB-FLOOR UNDER G-1 GALLEY DRAIN PAN. INSTALLED SUB-FLOOR DOUBLER UNDER G1 GALLEY PAN PER AARD 53-20-00-16. - [SDR AALA20130412018](https://openairdocs.org/sdr/AALA20130412018), Apr 12, 2013: CUSP WEB. CORRODED. RIGHT CUSP AT STATION 494 CORRODED. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER PER AARD 53-20-00-16. - [SDR AALA20130412016](https://openairdocs.org/sdr/AALA20130412016), Apr 12, 2013: FRAME. WORN. FRAME 1380 HAS WEAR ON FORWARD SIDE, CONTACT WITH TEMPERATURE CONTROL VALVE, LEFT. CUT OUT DAMAGE AND INSTALLED DOUBLER PER AARD 53-10-00-28. - [SDR AALA20130501010](https://openairdocs.org/sdr/AALA20130501010), Apr 10, 2013: CUSP WEB. CORRODED. CUT OUT AREA OF SUBFLOOR AND EEXISTING DOUBLER CORRODED. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-20-00-16. - [SDR AALA20130420009](https://openairdocs.org/sdr/AALA20130420009), Apr 10, 2013: SKIN. DAMAGED. FORWARD CARGO DOOR HAS SEVERAL SCRATCHES ON EXTERIOR SKIN. INSTALLED NEW EXTERIOR SKIN ON FORWARD CARGO DOOR. - [SDR AALA20130501014](https://openairdocs.org/sdr/AALA20130501014), Apr 9, 2013: LONGERON. CRACKED. LONGERON 3 LEFT IS CRACKED AT STATION 160. INSTALLED LONGERON SPLICE PER SRM 53-02-00 FIGURE 18. - [SDR AALA20130501012](https://openairdocs.org/sdr/AALA20130501012), Apr 9, 2013: SILL. CORRODED. FORWARD SERVICE DOOR SILL CORRODED AT STATION 198. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-20-00-14. - [SDR AALA20120723001](https://openairdocs.org/sdr/AALA20120723001), Jul 22, 2012: BATTERY PACK. DISCHARGED. CEILING EMERGENCY LIGHTS FROM ROWS 3 TO 6 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS FROM ROWS 3 TO 6. OPS CHECK NORMAL. - [SDR AALA20120506006](https://openairdocs.org/sdr/AALA20120506006), May 5, 2012: BATTERY PACK. NOT SEATED. OVERHEAD EMERGENCY LIGHTS 3AB AND 3EF INOPERATIVE. RESEATED BATTERY PACK IN BIN 4DEF. OPS CHECK NORMAL. All 164: https://openairdocs.org/deregistered/N513AA-2019-09-06/reports.md ## FAA accident and incident reports (1) 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 19910317008799I](https://openairdocs.org/incident/19910317008799I), Mar 17, 1991: Doug DC982 (N513AA), Dallas-Ft Worth, TX. Fuel odor in cabin en route. Landed and evacuated on taxiway. Unable to duplicate problem. Two passengers treated. ## Other aircraft with N513AA - [Registered now](https://openairdocs.org/aircraft/N513AA): Anduril Industries ROADRUNNER, S/N 3188 --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.