# N433AA: 1987 Mcdonnell Douglas DC-9-83(MD-83), registration cancelled 2019-01-07 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: January 7, 2019 - Status when cancelled: Second renewal notice - Airframe: [Mcdonnell Douglas DC-9-83(MD-83)](https://openairdocs.org/model/mcdonnell-douglas-dc-9-83-md-83) (registry code 3022083) - 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: 49451 - Year built: 1987 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: December 29, 1992 - Certificate issued: February 23, 2016 - Last registry action: February 23, 2016 - Mode S code: A52E44 - Owner when cancelled: [Delta Air Lines Inc](https://openairdocs.org/faa-owner/DELTA%20AIR%20LINES%20INC) - Location: [Atlanta, GA](https://openairdocs.org/faa-place/GA/Atlanta) - Owner type: Corporation - Owner's area on the map: 33.6604° N, 84.3865° W: Placed by OpenAirDocs at the center of ZIP code 30354, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N433AA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=433AA - Page: https://openairdocs.org/deregistered/N433AA-2019-01-07 From the FAA registry file of October 29, 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-9-83(MD-83): https://openairdocs.org/model/mcdonnell-douglas-dc-9-83-md-83.md ## Service difficulty reports (94, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR AALA20131126015](https://openairdocs.org/sdr/AALA20131126015), Nov 25, 2013: BATTERY PACK. DISCHARGED. OVERWING EMERGENCY EXIT SIGN AT 21AB INOPERATIVE. REPLACED BATTERY PACK FOR OVERWING EMERGENCY EXIT SIGN AT 21AB. OPERATIONS CHECKED NORMAL. - [SDR AALA20131126014](https://openairdocs.org/sdr/AALA20131126014), Nov 25, 2013: BATTERY PACK. DISCHARGED. OVERWING EMERGENCY EXIT SIGN AT 20AB INOPERATIVE. REPLACED BATTERY PACK FOR OVERWING EMERGENCY EXIT SIGN AT 20AB. OPERATIONS CHECKED NORMAL. - [SDR AALA20131126020](https://openairdocs.org/sdr/AALA20131126020), Nov 25, 2013: BATTERY PACK. DISCHARGED. OVERHEAD EMERGENCY LIGHTS BETWEEN ROWS 37 & 30 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS BETWEEN ROWS 37 & 30. OPERATIONS CHECKED NORMAL. - [SDR AALA20131126019](https://openairdocs.org/sdr/AALA20131126019), Nov 25, 2013: PORTABLE LIGHT. INOPERATIVE. HAND HELD PORTABLE EMERGENCY LIGHT AT LT NR 1 DOOR INOPERATIVE. REPLACED HAND HELD PORTABLE LIGHT. OPERATIONS CHECKED NORMAL. - [SDR AALA20131126018](https://openairdocs.org/sdr/AALA20131126018), Nov 25, 2013: BATTERY PACK. DISCHARGED. TAIL COMPARTMENT OVERHEAD & SLIDE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK IN AFT LAVATORY TAIL COMPARTMENT. OPERATIONS CHECKED NORMAL. - [SDR AALA20131126017](https://openairdocs.org/sdr/AALA20131126017), Nov 25, 2013: BATTERY PACK. DISCHARGED. OVERHEAD EMERGENCY LIGHTS FROM ROWS 23 TO 26 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS FROM ROWS 23 TO 26. OPERATIONS CHECKED NORMAL. - [SDR AALA20131126016](https://openairdocs.org/sdr/AALA20131126016), Nov 25, 2013: BATTERY PACK. DISCHARGED. OVERHEAD EMERGENCY LIGHTS FROM ROWS 13 TO 16 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS FROM ROWS 13 TO 16. OPERATIONS CHECKED NORMAL. - [SDR AALA20130222008](https://openairdocs.org/sdr/AALA20130222008), Feb 22, 2013: PITOT TUBE. FAILED. IAD - INFLIGHT DCA-ORD. CREW REPORTED FIRST OFFICER PITOT HEAT FAILED. EMERGENCY DECLARED FLIGHT DIVERTED IAD LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SER - [SDR AALA20120918007](https://openairdocs.org/sdr/AALA20120918007), Sep 17, 2012: LIGHT. DEFECTIVE. FORWARD EMERGENCY LIGHT IS DIM. REPLACED LAMP FOR FORWARD EMERGENCY LIGHT. - [SDR AALA20120420013](https://openairdocs.org/sdr/AALA20120420013), Apr 20, 2012: FRAME. CRACKED. FRAME 1418 CRACKED ON AFT SIDE AT LONGERON 2 RIGHT. INSTALLED DOUBLER AND FILLER REPAIR PER AARD 53-10-00-15 AND SRM 53-01-00. - [SDR AALA20120411005](https://openairdocs.org/sdr/AALA20120411005), Apr 10, 2012: BATTERY PACK. INOPERATIVE. EMERGENCY CEILING LIGHTS INOPERATIVE. RESEATED CEILING EMERGENCY LIGHTS BATTERY PACK. OPS CHECK NORMAL. - [SDR AALA20120129RDU01](https://openairdocs.org/sdr/AALA20120129RDU01), Jan 27, 2012: LENS. MISSING. EMERGENCY EXIT LIGHT AT LEFT AFT OVERWING EXIT DOOR MISSING LENS. REPLACED LENS. OPS CHECK NORMAL. - [SDR AALA20120106DFW01](https://openairdocs.org/sdr/AALA20120106DFW01), Jan 6, 2012: PROXIMITY SENSOR. INOPERATIVE. DFW - CREW REPORTED ON APPROACH WHEN LOWERING SLATS RECEIVED A SLAT DISAGREE WARNING INDICATION. EMERGENCY DECLARED FLIGHT LANDED DFW WITHOUT INCIDENT. AIRCRAFT - [SDR AALA20110522DFW01](https://openairdocs.org/sdr/AALA20110522DFW01), May 22, 2011: DISPLAY. INOPERATIVE. DFW - INFLIGHT AUS-ORD. CREW REPORTED NAVIGATION DISPLAY INOPERATIVE. EMERGENCY DECLARED FLIGHT DIVERTED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERV - [SDR AALA20101221DFW04](https://openairdocs.org/sdr/AALA20101221DFW04), Dec 21, 2010: CHARGER. INOPERATIVE. DFW - CREW REPORTED BATTERY DISCHARGE LIGHT ILLUMINATED DURING FLIGHT. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SER - [SDR AALA20101018TUL10](https://openairdocs.org/sdr/AALA20101018TUL10), Oct 16, 2010: SKIN. CRACKED. STATION 161 LONGERONS 16 LEFT TO 22 LEFT, HIGH FREQUENCY EDDY CURRENT INSPECTION INDICATES CRACK AROUND FASTENERS IN FUSELAGE SKIN. INSTALLED DOUBLER PER EA MD8 - [SDR AALA20100813LGA01](https://openairdocs.org/sdr/AALA20100813LGA01), Aug 12, 2010: BATTERY PACK. DISCHARGED. EMERGENCY LIGHTING AT AFT SERVICE DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT AFT SERVICE DOOR. - [SDR AALA20100418SFO01](https://openairdocs.org/sdr/AALA20100418SFO01), Apr 18, 2010: TUBE. LEAKING. SFO - CREW REPORTED RIGHT ENGINE OIL PRESSURE LIGHT DROPPED TO 20 PSI AND STABILIZED. RIGHT HAND THROTTLE REDUCED TO IDLE. FLIGHT RETURNED SFO LANDED WITHOUT IN - [SDR AALA20100216LGA02](https://openairdocs.org/sdr/AALA20100216LGA02), Feb 15, 2010: BATTERY. NOT SEATED. EMERGENCY LIGHTS OVERHEAD ADJACENT TO AFT LAVATORIES INOPERATIVE. RE-SEATED AFT EMERGENCY LIGHT BATTERY. OPS CHECKED NORMAL. - [SDR AALA20100216LGA01](https://openairdocs.org/sdr/AALA20100216LGA01), Feb 15, 2010: LIGHT. INOPERATIVE. SEAT 8D EGRESS LIGHT INOPERATIVE. RE-PINNED LIGHT ASSEMBLY FOR SEAT 8D EGRESS LIGHT. - [SDR AALA20090515TUL01](https://openairdocs.org/sdr/AALA20090515TUL01), May 14, 2009: SEAT TRACK. CORRODED. NR 1 SEAT TRACK CORRODED OUT OF LIMITS. INSTALLED SEAT TRACK PLUG PER SRM 53-10-3. - [SDR AALA20090513TUL40](https://openairdocs.org/sdr/AALA20090513TUL40), May 12, 2009: ANGLE. CORRODED. CORROSION ON PLOW ANGLE AT STA 1338. INSTALLED NEW PLOW ANGLE DOUBLER, P/N 9915561-73, PER SRM 51-30-00. - [SDR AALA20090513TUL21](https://openairdocs.org/sdr/AALA20090513TUL21), May 11, 2009: CARGO TRACK. CORRODED. CORROSION ON LT TIE DOWN TRACK STA 1211-1287. SPLICED IN NEW SECTION OF TIE DOWN TRACK PER SRM 53-05-00. - [SDR AALA20090513TUL29](https://openairdocs.org/sdr/AALA20090513TUL29), May 9, 2009: BRACKET. CORRODED. CORNER BRACKET CORRODED LOWER FWD CORNER OF AFT CARGO DOOR CUT-OUT. REPLACED BRACKET PER SRM 51-10-03. - [SDR AALA20090513TUL27](https://openairdocs.org/sdr/AALA20090513TUL27), May 9, 2009: INTERCOSTAL. CORRODED. CORROSION ON INTERCOSTAL IN AFT CARGO. REPLACED INTERCOSTAL PER SRM 51-30-05. - [SDR AALA20090513TUL30](https://openairdocs.org/sdr/AALA20090513TUL30), May 8, 2009: BEAM. CORRODED. CORROSION ON AFT CARGO DOOR BEAM. INSTALLED REPAIR DOUBLER PER AARD 53-10-00-3. - [SDR AALA20090513TUL22](https://openairdocs.org/sdr/AALA20090513TUL22), May 8, 2009: SKIN. GOUGED. DRILL DAMAGE TO SKIN 2 INCHES BELOW LONG 10L. REMOVED DAMAGE AND INSTALLED DOUBLER WITH FILLER PER EA 53-006187. - [SDR AALA20090513TUL20](https://openairdocs.org/sdr/AALA20090513TUL20), May 8, 2009: PLATE. CORRODED. CORROSION IN DELTA PLATE IN AFT CARGO. - [SDR AALA20090513TUL18](https://openairdocs.org/sdr/AALA20090513TUL18), May 8, 2009: ANGLE. CORRODED. CORROSION ON RT TIE DOWN TRACK Z ANGLE IN MID CARGO. REPLACED Z ANGLE PER SRM 51-30-01. - [SDR AALA20090513TUL12](https://openairdocs.org/sdr/AALA20090513TUL12), May 8, 2009: CARGO TRACK. CORRODED. RT TIE DOWN TRACK HAS CORROSION STA 1211-1287, AFT CARGO. REMOVED AND REPLACED RT AFT TIE DOWN TRACK PER SRM 51-30-00. - [SDR AALA20090513TUL01](https://openairdocs.org/sdr/AALA20090513TUL01), May 8, 2009: SKIN. DAMAGED. DRILL START IN EXTERIOR FUSE SKIN AT STA 886, 2 INCH BELOW L10L. INSTALLED FUSELAGE SKIN DOUBLER, STA 886 LT LONGERON 10, PER EA MD80-53-006187. - [SDR AALA20090513TUL19](https://openairdocs.org/sdr/AALA20090513TUL19), May 7, 2009: FLOOR SUPPORT. CORRODED. CORROSION ON FLOORBOARD SUPPORT ANGLE INBD OF DOOR BEAM IN AFT CARGO. REPLACED FLOORBOARD SUPPORT ANGLE PER SRM 51-30-2. - [SDR AALA20090513TUL17](https://openairdocs.org/sdr/AALA20090513TUL17), May 7, 2009: CARGO TRACK. CORRODED. CORROSION ON RT TIE DOWN TRACK IN MID CARGO. INSTALLED NEW TIE DOWN TRACK PER SRM 51-30-01. - [SDR AALA20090513TUL33](https://openairdocs.org/sdr/AALA20090513TUL33), May 6, 2009: CUSP WEB. CORRODED. REMOVED SMALL EDGE OF CUSP SHEET FOR CORROSION REMOVAL, STA 871. INSTALLED SMALL DOUBLER ON CUSP, .032; 7075-T6, PER AARD 53-20-00-16. - [SDR AALA20090513TUL25](https://openairdocs.org/sdr/AALA20090513TUL25), May 6, 2009: STRAP. CORRODED. STRAP ABOVE DOOR BEAM, ON WEB, HAS CORROSION, STA 1174. INSTALLED NEW STRAP, STA 1174, MADE OF 7075-T6; .063, PER SRM 51-30-02. - [SDR AALA20090512TUL63](https://openairdocs.org/sdr/AALA20090512TUL63), May 6, 2009: SEAT TRACK. CORRODED. CORROSION OUT OF LIMITS ON SEAT TRACK NR 6 STA 1090. REMOVED CORROSION AND INSTALLED SEAT TRACK PLUG PER AARD 53-20-00-10 AND EA MD80-53-006/62 - [SDR AALA20090513TUL39](https://openairdocs.org/sdr/AALA20090513TUL39), May 5, 2009: SUPPORT. CORRODED. CORROSION AT FWD GIRT BAR SUPPORT, STA 1142. INSTALLED NEW GIRT BAR SUPPORT PER SRM 51-30-05. - [SDR AALA20090513TUL38](https://openairdocs.org/sdr/AALA20090513TUL38), May 5, 2009: LONGERON. CORRODED. CORROSION ON LONG 30. REMOVED DAMAGED SECTION AND REPAIRED PER SRM 53-02-00 FIG 18. - [SDR AALA20090513TUL31](https://openairdocs.org/sdr/AALA20090513TUL31), May 5, 2009: CUSP WEB. CORRODED. CORROSION ON TOP OF SUBFLOOR, BELOW FWD GIRT BAR SUPPORT. REMOVED DAMAGE AND INSTALLED DOUBLER PER AARD 53-20-00-16. - [SDR AALA20090513TUL28](https://openairdocs.org/sdr/AALA20090513TUL28), May 5, 2009: CUSP WEB. CORRODED. CORROSION ON TOP OF SUBFLOOR, BELOW AFT GIRT BAR SUPPORT. INSTALLED REPAIR DOUBLER AND CUSP SUPPORT PER AARD 53-20-00-16. - [SDR AALA20090513TUL26](https://openairdocs.org/sdr/AALA20090513TUL26), May 5, 2009: SUPPORT. CORRODED. CORROSION ON AFT GIRT BAR SUPPORT, STA 1166. INSTALLED NEW GIRT BAR SUPPORT PER SRM 51-30-05. - [SDR AALA20090512TUL68](https://openairdocs.org/sdr/AALA20090512TUL68), May 5, 2009: SKIN. DENTED. DENT IN FUSELAGE RT SIDE (ENGINE COWL DRAIN MAST DAMAGE) STA 1309 BELOW LONGERON 18. INSTALLED DOUBLER PER SRM 53-04 FIG 38 AND INSTALLED SCUFF PLATE PER AARD 5 - [SDR AALA20090512TUL51](https://openairdocs.org/sdr/AALA20090512TUL51), May 5, 2009: STRUCTURE. CORRODED. CORROSION ON TOP OF SUBFLOOR BELOW FWD GIRT BAR SUPPORT STA 1142. CUT OUT DAMAGE, INSTALLED DOUBLER, .0406AL-4V TITANIUM AND FILLER 7075-T6 .063 PER AARD 53-20- - [SDR AALA20090512TUL48](https://openairdocs.org/sdr/AALA20090512TUL48), May 5, 2009: SUPPORT. CORRODED. CORROSION ON TOP OF SUBFLOOR BELOW AFT GIRT BAR SUPPORT STA 1166. CUT OUT DAMAGED AREA, INSTALLED DOUBLER .040 6AL-4V TITANIUM PER AARD 53-20-00-16. - [SDR AALA20090512TUL46](https://openairdocs.org/sdr/AALA20090512TUL46), May 5, 2009: SUPPORT. CORRODED. CORROSION ON AFT GIRT BAR SUPPORT BS 1166. INSTALLED SERVICEABLE GIRT BAR SUPPORT BS 1166. - [SDR AALA20090512TUL44](https://openairdocs.org/sdr/AALA20090512TUL44), May 5, 2009: FITTING. CORRODED. CORROSION ON FWD GIRT BAR SUPPORT FITTING STA1142. INSTALLED NEW GIRT BAR SUPPORT AT STA 1142 PER 51-30-05. - [SDR AALA20090513TUL36](https://openairdocs.org/sdr/AALA20090513TUL36), May 4, 2009: CUSP WEB. CORRODED. CORROSION ON CUSP SHEET, STA 503-598, RT SIDE. INSTALLED NEW CUSP SHEET, STA 503- 598, PER SRM 51-30-05. - [SDR AALA20090513TUL32](https://openairdocs.org/sdr/AALA20090513TUL32), May 4, 2009: FRAME. DENTED. FRAME DENTED AT RT STA 522 6 INCHES ABOVE CUSP. INSTALLED J ANGLE REPAIR PER AARD 53-10-00-17 FIG 1. - [SDR AALA20090513TUL34](https://openairdocs.org/sdr/AALA20090513TUL34), May 3, 2009: LONGERON. CRACKED. CRACK IN LONG 4L. REMOVED AND REPLACED LONG 4L FROM STA 168-230 PER SRM 53-02-00. - [SDR AALA20090512TUL31](https://openairdocs.org/sdr/AALA20090512TUL31), May 2, 2009: CUSP WEB. CRACKED. CRACK IN RT CUSP STA 597. INSTALLED DOUBLER PER AARD 53-20-00-16. All 94: https://openairdocs.org/deregistered/N433AA-2019-01-07/reports.md ## 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 ATL99LA049](https://openairdocs.org/ntsb/ATL99LA049), Feb 8, 1999: McDonnell Douglas MD-80 (N433AA), Raleigh, NC, no damage. Probable cause: The flight encountered clear air turbulence while descending through 17,000 feet mean sea level (MSL). ## 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. - [Accident 19990208023969A](https://openairdocs.org/incident/19990208023969A), Feb 8, 1999: Doug DC983 (N433AA), Raleigh-Durham, NC. (.4) According to the pilot, the airplane was descending through 17,000 feet for an approach into Raleigh, north carolina when severe turbulence was… ## Other aircraft with N433AA - [Registered now](https://openairdocs.org/aircraft/N433AA): Anduril Industries ROADRUNNER, S/N 3113 --- 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.