# N906DA: 1995 Mcdonnell Douglas MD-90-30, registration cancelled 2021-02-12

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: February 12, 2021
- Status when cancelled: First renewal notice
- Airframe: [Mcdonnell Douglas MD-90-30](https://openairdocs.org/model/mcdonnell-douglas-md-90-30) (registry code 3023690)
- Engine: [IAE V2500SERIES](https://openairdocs.org/engine/iae-v2500series) (registry code 34601)
- Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (OpenAirDocs)
- Serial number: 53386
- Year built: 1995
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: July 13, 1995
- Certificate issued: September 7, 1995
- Last registry action: February 23, 2018
- Mode S code: AC85C2
- 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/N906DA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=906DA
- Page: https://openairdocs.org/deregistered/N906DA-2021-02-12

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 MD-90-30: https://openairdocs.org/model/mcdonnell-douglas-md-90-30.md

## Service difficulty reports (166, newest 50)

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

- [SDR DALA2019072404396](https://openairdocs.org/sdr/DALA2019072404396), Jul 23, 2019: BATTERY PACK. DISCHARGED. ON SVC CK FOUND EMERGENCY LIGHTS AT ROWS 35 CDE AND AFT GALLEY EMERGENCY LIGHTS INOP. R+R EMERGENCY LIGHTS BATTERY PACK AT B5-237 AND CHARGE PER AMM 33-51. OPS 
- [SDR DALA2019071504250](https://openairdocs.org/sdr/DALA2019071504250), Jul 13, 2019: BATTERY PACK. DISCHARGED. ON SVC CHECK FOUND EMERGENCY LIGHTS AT ROWS 35 CDE, 37 CDE AND AFT GALLEY EMERGENCY LIGHTS INOP. R+R EMERGENCY LIGHTS BATTERY PACK AT B5-237 AND CHARGER PER AM 
- [SDR DALA2019031901787](https://openairdocs.org/sdr/DALA2019031901787), Mar 15, 2019: WIRE. DAMAGED. INOPERATIVE EMERGENCY LIGHTS (3 EAS) IN CEILING AREA AT PAX CABIN. ELECTRICAL WIRING L827BT18 ON ELECTRICAL CONECTOR R5-1202 AND ELECTRICAL WIRING L2495B16 ON E
- [SDR DALA2019031501703](https://openairdocs.org/sdr/DALA2019031501703), Mar 14, 2019: WEB. CRACKED. SUMMARY OF NRC 00043: SUPPORT WEB (RT AREA) IN VERTICAL STABILIZER INNER STRUCTURE STA ZRS 134 WAS REPAIRED PER ETI-90-19-012 REV. 3 AND ER/A. 576366-14 REV.ORI
- [SDR DALA2019030701520](https://openairdocs.org/sdr/DALA2019030701520), Mar 6, 2019: SPACER. CORRODED. CORROSION ON PREVIOUS REPAIR (SPACER) AT AFT CARGO DOOR CUT OUT LWR AREA. CORROSION LEVEL 2. SPACER AT AFT CARGO DOOR CUT OUT LWR AREA WAS REPLACED PER SRM VOL.
- [SDR DALA2019020540751](https://openairdocs.org/sdr/DALA2019020540751), Jan 21, 2019: DEFLECTOR. DAMAGED. RT NOSE LANDING GEAR DEBRIS DEFLECTOR HAS A PIECE MISSING. FLT CREW PLACARD INSTALLED AT NEK PER CDL 32-37-01. REMOVED AND REPLACED DEBRIS DEFLECTOR PER MD-90 A
- [SDR DALA2019011700307](https://openairdocs.org/sdr/DALA2019011700307), Jan 16, 2019: CONNECTOR. DISCONNECTED. DURING SERVICE CHECK FOUND CEILING EMERGENCY LIGHT L2-772 INOP. FOUND CONNECTOR J2-38 DISCONNECTED. RECONNECTED, OPS CHECK GOOD. OK FOR SVC. (LP# 4679590)
- [SDR DALA2019011700309](https://openairdocs.org/sdr/DALA2019011700309), Jan 16, 2019: POWER SUPPLY. INOPERATIVE. DURING SERVICE CHECK FOUND CEILING MOUNTED EMERGENCY LIGHTS INOP AFT OF L2 SERVICE DOOR. R&R POWER SUPPLY & BATTERY B5-237. OPS CHECK GOOD. OK FOR SERVICE. (LP 
- [SDR DALA2019010800097](https://openairdocs.org/sdr/DALA2019010800097), Jan 7, 2019: PLATE. MISSING. RT WING SLAT PLATE X2 MISSING. FWD TO CDL 57-30-06. REPLACED RT NR 5 METAL SLAT SEAL. CDL REMOVED. OK FOR SERVICE. (LP# 4988518)
- [SDR DALA2018110806541](https://openairdocs.org/sdr/DALA2018110806541), Nov 5, 2018: STARTER. ODOR. APU FAULT MESSAGE WITH ATTEMPTED APU START ACCOMPANIED BY REPORTED UNUSUAL ODOR BY FLIGHT ATTENDANTS IN THE BACK OF AIRCRAFT. APU INSPECTED AND BURN SMELL COMIN
- [SDR DALA2017122708904](https://openairdocs.org/sdr/DALA2017122708904), Dec 21, 2017: THRUST REVERSER. OUT OF RIG. DIVERTED TO ORD DUE TO LT REVERSER EOAP ILLUMINATED SHORTLY AFTER TAKE OFF. LT REVERSER UNLOCK LIGHT ILLUMINATED. FOUND LT THRUST REVERSER IN THE STOWED LOCKED 
- [SDR DALA2017112208277](https://openairdocs.org/sdr/DALA2017112208277), Nov 14, 2017: SIGN. INOPERATIVE. L2 OVERHEAD EXIT SIGN BROKEN. REMOVED AND REPLACED THE SIGN.
- [SDR DALA2017062605151](https://openairdocs.org/sdr/DALA2017062605151), Jun 24, 2017: SIGN. MISSING. FORWARD EXIT SIGNS MISSING. REPLACED.
- [SDR DALA2017040402838](https://openairdocs.org/sdr/DALA2017040402838), Apr 4, 2017: PRESSURE BLKHD. DAMAGED. FASTENER HOLE DAMAGED IN P DOME, ANGLE TAB, FORWARD OUTBOARD HOLE INBOARD OF STRINGER 26L END FITTING. REPAIRED IAW ERA 556923-14, REV O.
- [SDR DALA2016121509952](https://openairdocs.org/sdr/DALA2016121509952), Dec 14, 2016: BULB. INOPERATIVE. TWO BULBS INOPERATIVE AT R1 DOOR EMERGENCY EXIT. REMOVED AND REPLACED THE BULBS. OPERATION CHECKED OKAY.
- [SDR DALA2015051403346](https://openairdocs.org/sdr/DALA2015051403346), May 13, 2015: ANGLE. CRACKED. TAIL INTERIOR SUPPORT ANGLE CRACKED AT LT OTBD END OF VENTRAL STAIR TORQUE TUBE SUPPORT BEAM. COMPLIED WITH PRI 535833-14, REV O. REPAIRED IAW ERA 535833-14, RE
- [SDR DALA2014120906498](https://openairdocs.org/sdr/DALA2014120906498), Dec 6, 2014: LANYARD. WORN. FORWARD RT SERVICE DOOR SLIDE COVER LANYARD CABLE ASSY WORN. R & R SLIDE COVER LANYARD ASSY IAW AMM.
- [SDR DALA14018209206](https://openairdocs.org/sdr/DALA14018209206), Mar 23, 2014: SLIDE. LOW PRESSURE. DURING SERVICE CHECK, FOUND R1 DOOR SLIDE PRESSURE LOW. R & R R1 SLIDE IAW AMDS CARD 2500-4332.
- [SDR DALA13050379206](https://openairdocs.org/sdr/DALA13050379206), Oct 5, 2013: WIRE. DAMAGED. DURING SERVICE CHECK, MX FOUND CEILING EMERGENCY LIGHT 10R, INOPERATIVE. FOUND BROKEN SPLICE CONNECTOR OVER CEILING PANER REPAIRED IAW SWPM. OPS CHECKS GOOD.
- [SDR DALA13050369206](https://openairdocs.org/sdr/DALA13050369206), Oct 5, 2013: WIRE. DAMAGED. DURING SERVICE CHECK, MX FOUND CEILING EMERGENCY LIGHT 10L INOPERATIVE. FOUND BROKEN SPLICE CONNECTOR OVER CEILING PANEL. REPAIRED IAW SWPM. OPS CHECKS GOOD.
- [SDR DALA13050359206](https://openairdocs.org/sdr/DALA13050359206), Oct 5, 2013: WIRE. DAMAGED. DURING SERVICE CHECK, MX FOUND CEILING EMERGENCY LIGHT 37L INOPERATIVE. TROUBLESHOT, FOUND SPLICE CONNECTOR ABOVE CEILING PANEL OPEN. REPAIRED SPLICE CONNECTOR 
- [SDR DALA13050349206](https://openairdocs.org/sdr/DALA13050349206), Oct 5, 2013: WIRE. DAMAGED. DURING SERVICE CHECK, MX FOUND CEILING LIGHT 30L , EMERGENCY LIGHT INOPERATIVE. FOUND BROKEN SPLICE CONNECTOR ABOVE OVERHEAD PANEL. REPAIRED IAW SWPM. OPERATION
- [SDR DALA13040709206](https://openairdocs.org/sdr/DALA13040709206), Aug 21, 2013: FLOOR SUPPORT. CRACKED. FORWARD WET ARE, BS 344 - 360, LBL 11, FLOOR SUPPORT INTERCOSTAL IS CRACKED AT NUTPLATE HOLE. REMOVED AND REPLACED INTERCOSTAL IAW DWG 141A5400.
- [SDR DALA13039919206](https://openairdocs.org/sdr/DALA13039919206), Aug 17, 2013: FLOORBEAM. CORRODED. FLOORBEAM AT BS 1364 HAS CORROSION ON THE BEAM. REPAIRED OUT OF LIMITS FLOORBEAM IAW ERA 516865-14, REV O.
- [SDR DALA13039909206](https://openairdocs.org/sdr/DALA13039909206), Aug 15, 2013: PRESSURE BLKHD. CORRODED. AFT PRESSURE BULKHEAD, ON LOWER DOOR JAMB VERTICAL FRAME, CORRODED. REMOVED CORROSION. MATERIAL LOSS IS OUT OF LIMITS. REPAIRED IAW ERA 516848-14, REV O, PRI 51
- [SDR DALA13039899206](https://openairdocs.org/sdr/DALA13039899206), Aug 14, 2013: DOOR FRAME. GOUGED. AFT CABIN ENTRY DOOR FRAME IS GOUGED IN SEVERAL PLACES. REMOVED DAMAGE. FOUND TO BE OUT OF LIMITS. R & R CHANNEL IAW SRM 51-30-05, 51-30-02, 51-30-04.
- [SDR DALA13039499206](https://openairdocs.org/sdr/DALA13039499206), Aug 14, 2013: DOOR FRAME. GOUGED. AFT CABIN ENTRY DOOR FRAME, BOTTOM SIDE, IS GOUGED IN SEVERAL AREAS. REMOVED DAMAGE. FOUND TO BE OUT OF LIMITS. R & R CHANNEL IAW SRM 51-30-05, 51-30-02 AND 51-
- [SDR DALA13039489206](https://openairdocs.org/sdr/DALA13039489206), Aug 14, 2013: SKIN. CHAFED. NR 2 ENGINE PYLON LOWER SKIN HAS CHAFING DAMAGE AT OTBD END FROM FRONT SPAR TO AFT ENGINE MOUNT. REPAIRED CHAFING IAW ERA PRI 561053-14, REV 1, ERA 516053-14, R
- [SDR DALA13039889206](https://openairdocs.org/sdr/DALA13039889206), Aug 13, 2013: DOOR FRAME. GOUGED. AFT CABIN ENTRY DOOR LOWER RT FRAME GOUGED. R & R AFT CABIN ENTRY DOOR LOWER RT IAW SRM 51-30-02, 51-30-01, AND DWG 9929480.
- [SDR DALA13039479206](https://openairdocs.org/sdr/DALA13039479206), Aug 13, 2013: FRAME. DENTED. AFT CARGO DOOR, FORWARD INNER FRAME EDGE HAS DENT APPROXIMATE 6 INCHES BELOW CENTER OF DOOR SKIN OVERLAP. ACCOMPLISH REPAIR TO AFT CARGO DOOR INNER PAN LOWER FO
- [SDR DALA13039469206](https://openairdocs.org/sdr/DALA13039469206), Aug 13, 2013: CUSP WEB. CRACKED. BS 1360, CUSP WEB HAS CRACK. REPAIRED CRACKED CUSP WEB IAW SRM 53-20-02.
- [SDR DALA13038989206](https://openairdocs.org/sdr/DALA13038989206), Aug 10, 2013: SKIN. CRACKED. WHILE ACCOMPLISHING REPETITIVE INSPECTION OF FUSELAGE SKIN REPAIR AT BS 1475 BETWEEN LONGERONS 1 AND 3R, FOUND REPAIR TO HAVE 2" CRACK IN RADIUS, STA 1475 BETWE
- [SDR DALA13039049206](https://openairdocs.org/sdr/DALA13039049206), Aug 9, 2013: CUSP WEB. CRACKED. PASSENGER CABIN STA 1360, RIGHT CUSP WEB HAS CRACK. REMOVED, FABRICATED, TREATED, PRIMED AND INSTALLED FILLER AND DOUBLER IAW SRM 51-10-03, 51-30-02.
- [SDR DALA13039009206](https://openairdocs.org/sdr/DALA13039009206), Aug 9, 2013: CUSP WEB. CORRODED. MAIN CABIN LT CUSP WEB IS CORRODED FROM STA 1267 -1305. R & R DAMAGED CUSP WEB IAW SRM 51-30-02, 51-30-03, AND 51-10-05.
- [SDR DALA13038999206](https://openairdocs.org/sdr/DALA13038999206), Aug 9, 2013: SPAR CAP. DAMAGED. DURING NDT INSPECTION FOUND 1EACH FASTENER HOLE WITH CRACK ON RT VERTICAL STAB FRONT SPAR CAP FORWARD FLANGE. STA ZFS-52.267. REMOVED UPPER L/E SURFACE AND REMO
- [SDR DALA13038979206](https://openairdocs.org/sdr/DALA13038979206), Aug 8, 2013: CUSP WEB. DAMAGED. CUSP WEB AT BS 883+14" LT SIDE HAS DAMAGE. REPAIRED CUSP WEB IAW SRM 53-20-02, FIG 28.
- [SDR DALA13038969206](https://openairdocs.org/sdr/DALA13038969206), Aug 8, 2013: CUSP WEB. CORRODED. RIGHT CABIN CUSP WEB BS 655-674 CORRODED. FOUND OUT OF LIMITS. FABRICATED AND INSTALLED WEB IAW SRM 53-10-02 AND DWG 990443, REV A.
- [SDR DALA13038609206](https://openairdocs.org/sdr/DALA13038609206), Aug 7, 2013: BULKHEAD. CORRODED. AFT PRESSURE BULKHEAD, UNDERSIDE OF DOOR FRAME IS CORRODED. REMOVED CORROSION. 100 PERCENT MATERIAL LOSS. R & R DOOR SILLL IAW DWG 5917579, SRM 51-10-4, 51-10-0
- [SDR DALA13038579206](https://openairdocs.org/sdr/DALA13038579206), Aug 7, 2013: SEAT TRACK. CORRODED. PASSENGER CABIN LT OTBD SEAT TRACK, BS 735 HAS CORROSION. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. R & R SEAT TRACK IAW AMM.
- [SDR DALA13038569206](https://openairdocs.org/sdr/DALA13038569206), Aug 7, 2013: CUSP WEB. CORRODED. MAIN CABIN BS 598 - 617 LBL 60 CUSP WEB UPPER SURFACE HAS CORROSION. REPAIRED OUT OF LIMITS CUSP WEB IAW SRM 53-20-02.
- [SDR DALA13038399206](https://openairdocs.org/sdr/DALA13038399206), Aug 5, 2013: CUSP WEB. DAMAGED. CUSP WEB BS 552 DAMAGED. FOUND TO BE OUT OF LIMITS. REMOVED, FABRICATED, TREATED, PRIMED AND INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 51-30-00, 51-30-01, 53-
- [SDR DALA13038379206](https://openairdocs.org/sdr/DALA13038379206), Aug 5, 2013: CUSP WEB. CORRODED. MAIN CABIN BS 544, LBL 60 CUSP WEB UPPER SURFACE HAS CORROSION. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR IAW SRM 53-20-02, 
- [SDR DALA13038369206](https://openairdocs.org/sdr/DALA13038369206), Aug 5, 2013: CUSP WEB. CORRODED. MAIN CABIN BS 617-636 LBL 60 CUSP WEB UPPER SURFACE HAS CORROSION. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR IAW SRM 53-20-0
- [SDR DALA13038359206](https://openairdocs.org/sdr/DALA13038359206), Aug 4, 2013: CUSP WEB. DAMAGED. RIGHT CABIN CUSP WEB, BS 698 DAMAGED. REMOVED DAMAGE AREA AND REPAIRED IAW SRM 53-20-02, FIG 19.
- [SDR DALA13038389206](https://openairdocs.org/sdr/DALA13038389206), Aug 3, 2013: CUSP WEB. DAMAGED. CUSP WEB DAMAGED. FABRICATED DOUBLER, RING DOUBLER AND CUSP WEB IAW SRM 51-30-02, 53-20-02, FIG 19, 51-10-03 PARA 21.
- [SDR DALA13037619206](https://openairdocs.org/sdr/DALA13037619206), Aug 3, 2013: SEAT TRACK. CORRODED. LEFT OTBD CABIN SEAT TRACK CORRODED, BS 579-588, LBL 54. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. R & R SEAT TRACK IAW SRM 53-40-01, FIG 6 AND 51-30-01, PG
- [SDR DALA13038429206](https://openairdocs.org/sdr/DALA13038429206), Aug 1, 2013: FLOORBEAM. CORRODED. FORWARD WET AREA, FLOORBEAM HAS CORROSION ON TOP TEE BS 179 FROM LBL 17-38. REMOVED CORROSION. FOUND OUT OF LIMITS. REPLACED FLOORBEAM TEE IAW SRM 51-30-02 PARA
- [SDR DALA13038549206](https://openairdocs.org/sdr/DALA13038549206), Jul 31, 2013: FLOOR SUPPORT. CORRODED. MAIN CABIN BS 148+9, RBL 58 FLOOR SUPPORT ANGLE HAS CORROSION. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED ANGLE IAW SRM 51-30-02.
- [SDR DALA13037189206](https://openairdocs.org/sdr/DALA13037189206), Jul 30, 2013: FRAME. CORRODED. AFT CARGO FRAME, BS 1366, HAS AREAS OF CORROSION BETWEEN LONGERONS 28L AND 28R. TASK 35-302-07. FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 53-10-02, FIG 2.
- [SDR DALA13036729206](https://openairdocs.org/sdr/DALA13036729206), Jul 28, 2013: SEAT TRACK. CORRODED. BS 1210-1212, LBL 45 SEAT TRACK HAS CORROSION AROUND FLOORBOARD HOLES. REPAIRED SEAT TRACK. R & R WITH NEW REPAIR SECTION IAW SRM 53-40-01.

All 166: https://openairdocs.org/deregistered/N906DA-2021-02-12/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 DEN07FA008](https://openairdocs.org/ntsb/DEN07FA008), Oct 12, 2006: McDonnell Douglas MD-90-30 (N906DA), Denver, CO, substantial damage. Probable cause: A fractured nose gear assembly spray deflector that blocked the nose gear from extending during landing, and resulted in an intentional nose gear up landing.

## 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.

- [Accident 20061011021509A](https://openairdocs.org/incident/20061011021509A), Oct 11, 2006: Doug MD9030 (N906DA), Denver, CO, Substantial damage. (-23) Delta 1636 on a routine flight from kslc to kden encountered a nose gear malfunction on lowering the gear for landing @ den, leveled off at 1000' AGL,…
- [Incident 20011124035559I](https://openairdocs.org/incident/20011124035559I), Nov 24, 2001: Doug MD9030 (N906DA), Santa Ana, CA, Minor damage. (-23) After touchdown at sna the pilot stated the left anti skid system failed. The left MLG tires blew out due to the excessive stress put on the braking…
- [Incident 19960517015339I](https://openairdocs.org/incident/19960517015339I), May 17, 1996: Doug MD9030 (N906DA), Kansas City, MO. Narrative: on 5/17/96, delta flight dal 1893 departed mci. The aircrew returned to mci because the landing gear would not retract. Maintenance inspected the…

---
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.