# N936DN: 1996 Mcdonnell Douglas MD-90-30, registration cancelled 2022-12-31

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: December 31, 2022
- Status when cancelled: Valid registration
- 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: 53461
- Year built: 1996
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: February 20, 2012
- Certificate issued: July 1, 2016
- Last registry action: June 13, 2022
- Mode S code: ACFC4B
- 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/N936DN
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=936DN
- Page: https://openairdocs.org/deregistered/N936DN-2022-12-31

From the FAA registry file of November 7, 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 (126, newest 50)

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

- [SDR DALA2019110706455](https://openairdocs.org/sdr/DALA2019110706455), Nov 7, 2019: BATTERY PACK. INOPERATIVE. DURING SVC FOUND CON EXIT FLOOD LIGHTS INOP.REPLACED EMERGENCY BATTER B5-239 PER MD90MM 33-51. OPS CHECK NORM(6611867)
- [SDR DALA2019102906230](https://openairdocs.org/sdr/DALA2019102906230), Oct 25, 2019: APU BAY. CONTAMINATED. DURING TAKEOFF AND CLIMBOUT. FLIGHT ATTENDANT COULD SMELL A BURNT RUBBER SMELL THROUGHOUT THE ENTIRE A/C. IN THE COCKPIT IT SMELLED LIKE A PETROLEUM PRODUCT OIL
- [SDR DALA2019101605932](https://openairdocs.org/sdr/DALA2019101605932), Oct 15, 2019: SENSOR. FAILED. ELEVATOR SPLIT INDICATION IN FLIGHT 12000 MSL 320 KTS. T/S PER NO-GO ODI PROCEDURES. CONFIRMED CONTORL COLUMNS NOT DISCONNECTED. VISUALLY CONFIRMED ELEVATOR SUR
- [SDR DALA2019092605519](https://openairdocs.org/sdr/DALA2019092605519), Sep 25, 2019: STRUCTURE. CRACKED. C/W HFEC OF RT HORIZ STAB UPPER REAR SPAR AFT 2 BARREL NUT HOLES PER CARD 5510-01099-01B. AFT BARREL NUT HOLE HAS CRACK INDICATION. END OF CRACK MARKED. HORIZON
- [SDR DALA2019092005460](https://openairdocs.org/sdr/DALA2019092005460), Sep 19, 2019: PLATE. GALLED. THE RIGHT INBOARD AFT ATTACH POINT MOUNTING PLATE FOR THE HORIZONTAL STABILIZER SHOWS SIGNS OF GALLING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 014-0003:5510-
- [SDR DALA2019092005459](https://openairdocs.org/sdr/DALA2019092005459), Sep 19, 2019: PLATE. GALLED. THE LEFT INBOARD AFT ATTACH POINT MOUNTING PLATE FOR THE HORIZONTAL STABILIZER SHOWS SIGNS OF GALLING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 014-0003:5510-4
- [SDR DALA2019092005458](https://openairdocs.org/sdr/DALA2019092005458), Sep 19, 2019: PLATE. GALLED. THE RIGHT OUTBOARD AFT ATTACH POINT MOUNTING PLATE FOR THE HORIZONTAL STABILIZER SHOWS SIGNS OF GALLING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 014-0003:5510
- [SDR DALA2019092005457](https://openairdocs.org/sdr/DALA2019092005457), Sep 19, 2019: PLATE. GALLED. THE LEFT OUTBOARD AFT ATTACH POINT MOUNTING PLATE FOR THE HORIZONTAL STABILIZER SHOWS SIGNS OF GALLING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 014-0003:5510-
- [SDR DALA2019031801785](https://openairdocs.org/sdr/DALA2019031801785), Mar 17, 2019: BATTERY PACK. DISCHARGED. DURING SVC CHECK FOUND LOWER AFT BULKHEAD EMERGENCY EXIT LIGHT INOP. FOUND EMERGENCY LIGHT BATTERY DEAD. R+R BTTERY PACK PER AMM 33-51. OPS CHECK GOOD. A/C OK F
- [SDR DALA2019010200006](https://openairdocs.org/sdr/DALA2019010200006), Jan 1, 2019: DEFLECTOR. MISSING. RT MLG DEBRIS DEFLECTOR O/B MISSING. FWD TO MCO PER CDL 32-12-03. PLACARDS INSTALLED. REMOVED AND REPLACED RT MLG O/B SPRAY DEFLECTOR PER AMM 32-12. CDL AND PLA
- [SDR DALA2018110876540](https://openairdocs.org/sdr/DALA2018110876540), Nov 5, 2018: SKIN. CRACKED. WHILE IN ATL FOR C-CHECK MTC REPORTED A CRACK COMMON TO THE V. STAB. RAM INLET SKIN. THE CRACK IS LOCATED AFT OF WHERE THE REMOVABLE SKIN ATTACHES. THE ER/A 00-
- [SDR DALA2018110606473](https://openairdocs.org/sdr/DALA2018110606473), Nov 5, 2018: BATTERY PACK. INOPERATIVE. CABIN EMER LIGHTS AT ROW 34 INOP. REMOVED & REPLACED BATTERY AT POWER SUPPLY B5-231. OPS CHECK GOOD. (LP# 3762934)
- [SDR DALA2018110606472](https://openairdocs.org/sdr/DALA2018110606472), Nov 5, 2018: BATTERY PACK. MALFUNCTIONED. DOOR 1L & 1R EMER LIGHTS FLASH ON THEN OFF. REMOVED & REPLACED BATTERY AT POWER SUPPLY B5-211. OPS CHECK GOOD. (LP# 3762933)
- [SDR DALA2018070304345](https://openairdocs.org/sdr/DALA2018070304345), Jun 30, 2018: LIGHT. INOPERATIVE. FWD GALLEY EMER. EXIT SIGN HAS SEVERAL INOP BULBS. RELAMPED FWD GALLEY EMER EXIT SIGN LIGHT BULBS PER AMM 33-51-18. OPS CHECKS GOOD.
- [SDR DALA2017120608482](https://openairdocs.org/sdr/DALA2017120608482), Dec 5, 2017: BATTERY PACK. DISCHARGED. L2 DOOR EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK B5-241 PER MM. OPERATION CHECKS GOOD.
- [SDR DALA2017112208274](https://openairdocs.org/sdr/DALA2017112208274), Nov 21, 2017: STRUCTURE. CORRODED. CORROSION ON STRUCTURE BS 904 LBL 22 AND BS 900 LBL 21. REPAIRED IAW ERA 563304-14.LP# 0308510.
- [SDR DALA2017112208273](https://openairdocs.org/sdr/DALA2017112208273), Nov 21, 2017: SKIN. DAMAGED. FUSELAGE FWD CARGO BELLY SKIN IS CREASED AT BS 408 BETWEEN LONGERONS 29 AND 30R AT THE FRAME SHEAR TIE. REPAIRED IAW ERA 563268-14, REV C.
- [SDR DALA2017060404449](https://openairdocs.org/sdr/DALA2017060404449), May 31, 2017: UNKNOWN. MALFUNCTIONED. 1/2 OF THE CEILING EMERGENCY LIGHTS REMAINED ILLUMINATED FOR ENTIRE FLIGHT. CYCLED EMERGENCY POWER SWITCH. OPERATION CHECKS NORMAL.
- [SDR DALA2017013100855](https://openairdocs.org/sdr/DALA2017013100855), Jan 28, 2017: LIGHT. MALFUNCTIONED. EMERGENCY CEILING LIGHTS ILLUMINATED WITH CABIN AND FLIGHT DECK SWITCH IN NORMAL POSITION. CYCLED EMERGENCY POWER SWITCH. OPS CHECKED GOOD.
- [SDR DALA2017011800439](https://openairdocs.org/sdr/DALA2017011800439), Jan 16, 2017: LIGHT. UNSECURE. EMERGENCY LIGHT UNSECURE AT ROW 26A. SECURED THE LIGHT.
- [SDR DALA2017010900166](https://openairdocs.org/sdr/DALA2017010900166), Jan 5, 2017: BATTERY PACK. INOPERATIVE. CABIN EMERGENCY CEILING LIGHTS INOPERATIVE AT ROW 33 LEFT AND RIGHT. REMOVED AND REPLACED BATTERY PACK.
- [SDR DALA2015121507673](https://openairdocs.org/sdr/DALA2015121507673), Dec 14, 2015: SKIN. DAMAGED. LIGHTNING STRIKE ON RT WINDOW BELT, BS 807. REMOVED AND REWORKED IAW SRM 53-30-03 AND 51-10-03. FOUND TO BE OUT OF LIMITS.
- [SDR DALA2015121407601](https://openairdocs.org/sdr/DALA2015121407601), Dec 13, 2015: STRUCTURE. CORRODED. CORROSION ON LT BARREL NUT HOLE NR 10 AT HORIZONTAL STABILIZER. REPAIRED IAW ETI 90-15-108, REV 1 AND ERA 541540-14 REV O.
- [SDR DALA2015121407600](https://openairdocs.org/sdr/DALA2015121407600), Dec 13, 2015: STRUCTURE. CORRODED. CORROSION ON RT BARREL NUT HOLE NR 15 AT HORIZONTAL STABILIZER. REPAIRED IAW ETI 90-15-108, REV 1 AND ERA 541540-14, REV.
- [SDR DALA2015121407598](https://openairdocs.org/sdr/DALA2015121407598), Dec 13, 2015: SPAR CAP. CORRODED. CORROSION ON INTERNAL DOUBLER AT RT WING FRONT SPAR LOWER CAP, XOS 257. REPAIRED IAW ETI 90-15-100, REV 2 AND ERA 539955-14, REV O.
- [SDR DALA2015121407599](https://openairdocs.org/sdr/DALA2015121407599), Dec 12, 2015: STRUCTURE. CORRODED. CORROSION ON BARREL NUT HOLE NR 12, BS 7.2 LT SIDE AT HORIZONTAL STABILIZER. REPAIRED IAW ETI 90-15-107, REV 2 AND ERA 541538-14, REV O.
- [SDR DALA2015121307596](https://openairdocs.org/sdr/DALA2015121307596), Dec 12, 2015: RIB. CRACKED. CRACK ON FORMER RIB, XOS=456, FIXED L/E INTERIOR SURFACE LEFT WING. REPAIRED FORMER RIB IAW ETI-90-15-112 AND SRM 51-30-05, 51-30-02, 51-10-03 AND ERA 541549-14
- [SDR DALA2015121307595](https://openairdocs.org/sdr/DALA2015121307595), Dec 12, 2015: CARGO TRACK. CORRODED. CORROSION ON LT CARGO TRACK FROM BS 1136 TO 1307, TASK 53-100-61. NEW CARGO TRACK INSTALLED IAW SRM 51-10-05, 51-30-02, 51-30-01 AND 51-10-03.
- [SDR DALA2015121307594](https://openairdocs.org/sdr/DALA2015121307594), Dec 12, 2015: DOOR FRAME. CORRODED. CORROSION ON WEB AND STRAP BS 1269 DOOR JAMB AFT CARGO COMPARTMENT. REPAIRED IAW ERA 541577-14, REV O.
- [SDR DALA2015121407602](https://openairdocs.org/sdr/DALA2015121407602), Dec 11, 2015: STRUCTURE. CORRODED. CORROSION AT BORES INNER DIAMETER OF HORIZONTAL STABILIZER LT SIDE HINGE NR 1. REPAIRED IAW ETI-90-15-105, REV 1 AND ERA 541536-14, REV O.
- [SDR DALA2015121307597](https://openairdocs.org/sdr/DALA2015121307597), Dec 11, 2015: FRAME. CORRODED. CORROSION ON FRAME CLIP, BS 1520 CANT BETWEEN LONGERON 23L TO VENTRAL STAIRWAY DOORJAMB IN AFT ACCESSORY COMPARTMENT. REPAIRED IAW ETI-90-15-116 AND SRM 51-30-0
- [SDR DALA2015121007532](https://openairdocs.org/sdr/DALA2015121007532), Dec 9, 2015: ACCESS PANEL. CORRODED. CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE 620EB. NEW BUSHING WAS FABRICATED AND INSTALLED IAW SRM 57-00-04.
- [SDR DALA2015121007531](https://openairdocs.org/sdr/DALA2015121007531), Dec 9, 2015: ACCESS PANEL. WORN. WEAR AT HOLE DIAMETER OF ACCESS PLATE-MID. REPAIRED HOLES IAW ETI 90-15-111, REV O AND ERA 541543-14, REV O.
- [SDR DALA2015121007530](https://openairdocs.org/sdr/DALA2015121007530), Dec 9, 2015: STRUCTURE. WORN. WEAR ON INNER BORES, 3 EA OF HORIZONTAL STABILIZER UPPER FORWARD ACCESS PLATE. REPAIRED IAW ETI 90-15-111, REV O AND ERA 541543-14, REV O.
- [SDR DALA2015120907529](https://openairdocs.org/sdr/DALA2015120907529), Dec 8, 2015: INTERCOSTAL. CRACKED. CRACK ON LOWER INTERCOSTAL OF HYDRAULIC SERVICE PANEL AT LT WHEEL WELL JAMB. REPLACED IAW SRM 51-30-02, 51-30-05 AND DWG 5930584.
- [SDR DALA2015120907528](https://openairdocs.org/sdr/DALA2015120907528), Dec 8, 2015: LONGERON. CRACKED. CRACK ON LONGERON 12L AND 4L, BS 1494 IN AFT ACCESSORY COMPARTMENT. REPAIRED IAW SRM 53-10-01.
- [SDR DALA2015120907527](https://openairdocs.org/sdr/DALA2015120907527), Dec 8, 2015: ACCESS PANEL. CORRODED. CORROSION ON SETTLEMENT AND COUNTERSINK AREA OF FUEL ACCESS PLATE 620JB. REAMED HOLES, FABRICATED AND INSTALLED BUSHINGS IAW SRM 51-10-03.
- [SDR DALA2015120807525](https://openairdocs.org/sdr/DALA2015120807525), Dec 7, 2015: CHANNEL. CRACKED. CRACK ON CHANNEL OF FLOOR PANEL BETWEEN BS 120-148. DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 54-02-04, 51-10-01, 53-20-03 AND 51-30-02.
- [SDR DALA2015120807524](https://openairdocs.org/sdr/DALA2015120807524), Dec 7, 2015: CHANNEL. CRACKED. CRACK ON LT MLG INBD DOOR AFT CHANNEL BETWEEN BS 1044.8 - 1052.813. R & R CHANNEL IAW SRM 51-30-02.
- [SDR DALA2015120807523](https://openairdocs.org/sdr/DALA2015120807523), Dec 7, 2015: ACCESS PANEL. CORRODED. CORROSION ON SETTLEMENT AND COUNTERSINK AREA OF FUEL ACCESS PANEL 620FT. BUSHINGS WERE REPLACED IAW SRM 57-00-04 AND 51-10-03.
- [SDR DALA2015120807522](https://openairdocs.org/sdr/DALA2015120807522), Dec 7, 2015: ACCESS PANEL. CORRODED. CORROSION ON CONTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PANEL 620FT. BUSHING FABRICATED AND INSTALLED IAW SRM 57-00-01.
- [SDR DALA2015120707448](https://openairdocs.org/sdr/DALA2015120707448), Dec 6, 2015: ACCESS PANEL. CORRODED. CORROSION ON SETTLEMENT AND COUNTERSINK AREA OF FUEL ACCESS PANEL NR 520EB. FOUND TO BE OUT OF LIMITS. REPLACED FUEL PANEL IAW SRM 57-00-04.
- [SDR DALA2015120407447](https://openairdocs.org/sdr/DALA2015120407447), Dec 3, 2015: CARGO TRACK. CORRODED. CORROSION ON RT CARGO TRACK BS 1136 TO 1212. R & R IAW SRM 53-20-01, 51-30-01, 51-30-02 AND 51-10-03.
- [SDR DALA2015120407446](https://openairdocs.org/sdr/DALA2015120407446), Dec 3, 2015: ATTACH ANGLE. CRACKED. CRACKS ON DORSAL FIN ATTACH INTERNAL ANGLES. R & R IAW SRM 51-30-05.
- [SDR DALA2015120407445](https://openairdocs.org/sdr/DALA2015120407445), Dec 3, 2015: INTERCOSTAL. CRACKED. CRACKS ON LOWER INTERCOSTAL, BS 1046 AT KEEL BEAM. REPLACED IAW SRM 51-30-02, 51-30-05 AND DWG 5936395, REV BF.
- [SDR DALA2015120307444](https://openairdocs.org/sdr/DALA2015120307444), Dec 2, 2015: STIFFENER. CRACKED. CRACKED STIFFNER, BS 1556 CANT BETWEEN 7 HRS AND 8 HRS POSITIONS AFT ACCESSORY COMPARTMENT. REPAIRED IAW SRM 53-10-03, FIG 17.
- [SDR DALA2015120307443](https://openairdocs.org/sdr/DALA2015120307443), Dec 2, 2015: BEAM. CORRODED. CORROSION ON RT BEAM OF VENTRAL STAIRWAY DOOR JAMB BS 1531 CANT TO 1542. X=-17.5. FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 53-00-01.
- [SDR DALA2015120207340](https://openairdocs.org/sdr/DALA2015120207340), Dec 1, 2015: RUB STRIP. CORRODED. CORROSION ON RUB STRIP AREAS AT BS 790-883 FROM LONGERON 26 TO 30 RT, BS 831, 827, 827.5, 832 AND 836 FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 53-30-01.
- [SDR DALA2015120207339](https://openairdocs.org/sdr/DALA2015120207339), Dec 1, 2015: ACCESS PANEL. CORRODED. CORROSION ON SETTLEMENT AND COUNTERSINK AREAS OF FUEL ACCESS PANEL 620AT. FOUND TO BE OUT OF LIMITS. REPLACED FUEL ACCESS PANEL IAW SRM 57-00-04.
- [SDR DALA2015120207338](https://openairdocs.org/sdr/DALA2015120207338), Dec 1, 2015: ACCESS PANEL. CORRODED. CORROSION ON SETTLEMENT AND COUNTERSINK AREA OF FUEL ACCESS PANEL 520JB. FOUND OUT OF LIMITS. REPLACED FUEL ACCESS PANEL IAW SRM 57-00-04.

All 126: https://openairdocs.org/deregistered/N936DN-2022-12-31/reports.md

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