# N918DH: 1996 Mcdonnell Douglas MD-90-30, registration cancelled 2022-11-30

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: November 30, 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: 53553
- Year built: 1996
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: July 20, 2010
- Certificate issued: February 8, 2010
- Last registry action: July 19, 2022
- Mode S code: ACB4B6
- 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/N918DH
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=918DH
- Page: https://openairdocs.org/deregistered/N918DH-2022-11-30

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 (102, newest 50)

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

- [SDR DALA2019081304741](https://openairdocs.org/sdr/DALA2019081304741), Aug 13, 2019: INLET. CONTAMINATED. ON ARRIVING AT AIRCRAFT FO & CAPTAIN SMELLED A BURNING ODOR COMING FROM AC VENT OVER GALLEY WITH MINUITES APU AUTO SHUTDOWN WITH FAULT. CONFIRMED APU INLET OIL 
- [SDR DALA201902110881](https://openairdocs.org/sdr/DALA201902110881), Feb 9, 2019: SKIN. CRACKED. CRACKS 2(E/A) ON VERTICAL STABILIZER SKIN STA ZFS= 23.500 APROX. (EHV) PERMANENT REPAIR SECTION I WAS PERFORMED ON VERTICAL STABILIZER SKIN STA ZFS= 23.500 APRO
- [SDR DALA2019021190880](https://openairdocs.org/sdr/DALA2019021190880), Feb 8, 2019: SKIN. CRACKED. CRACKS ON VERTICAL STABILIZER SKIN STA ZFS=-26.8 APROX. BELOW LL RAM AIR PER ER/A 575309-14AD REV. ORIGINAL AND ETI-90-19-006 REV. ORIGINAL REPAIR APPROVAL IS L
- [SDR DALA2019020540753](https://openairdocs.org/sdr/DALA2019020540753), Feb 3, 2019: ATTACH ANGLE. CRACKED. INITIAL INSPECTION: CRACKED VERTICAL ATTACH ANGLE P/N: 5912188-50 RH (EHV). SUMMARY: OF NRC.00120 VERTICAL ATTACH ANGLE P/N: 5912188-50 RH WAS REPLACED PER MD-9
- [SDR DALA2019020540752](https://openairdocs.org/sdr/DALA2019020540752), Feb 3, 2019: ATTACH ANGLE. CRACKED. INITIAL INSPECTION: CRACKED VERTICAL ATTACH ANGLE P/N: 5912188-49 LH (EHV). SUMMARY OF NRC. 00118 VERTICAL ATTACH ANGLE P/N: 5912188-49 LH WAS REPLACED PER MD-9
- [SDR DALA2018090705472](https://openairdocs.org/sdr/DALA2018090705472), Sep 5, 2018: BATTERY PACK. DISCHARGED. SEVERAL CABIN EMERGENCY LIGHT FAIL TEST. R&R EMERGENCY LIGHT BATTERY PACKS B5-235 AND B--236 IAW MDPO AMM 33-51, OPS CK GOOD.
- [SDR DALA2018051503057](https://openairdocs.org/sdr/DALA2018051503057), May 3, 2018: POWER SUPPLY. INOPERATIVE. EMERGENCY EXIT LIGHT AT SEAT 30 ABC INOPERATIVE. REPLACED THE POWER SUPPLY. OPS CHECKED GOOD IAW AMM 33-51.
- [SDR DALA2017112008276](https://openairdocs.org/sdr/DALA2017112008276), Nov 20, 2017: POWER SUPPLY. INOPERATIVE. EMERGENCY POWER SUPPLY INOPERATIVE AT THE AFT EMERGENCY EXIT DOOR. REMOVED AND REPLACED THE POWER SUPPLY .
- [SDR DALA2017031302010](https://openairdocs.org/sdr/DALA2017031302010), Mar 9, 2017: SLIDE. LOOSE. TAIL CONE COMPARTMENT SLIDE LOOSE. REPLACED THE SLIDE.
- [SDR DALA2017012300615](https://openairdocs.org/sdr/DALA2017012300615), Jan 21, 2017: PROBE. DAMAGED. LIGHTNING STRIKE ON CLIMB OUT FROM ATL. INSPECTED. FOUND DAMAGE TO AUXILIARY PITOT PROBE, LEFT WING NAV LIGHT AND RIVETS ON CROWN OF FUSELAGE. NON- ROUTINES WRI
- [SDR DALA2016110908717](https://openairdocs.org/sdr/DALA2016110908717), Nov 7, 2016: HOUSING. DAMAGED. R1 EMERGENCY EXIT LIGHT LENS MISSING AND COVER MOUNT DAMAGED. REPLACED LIGHT BASE AND COVER IAW MM. OPERATION CHECKS GOOD. (LP# 9167692)
- [SDR DALA2016061604797](https://openairdocs.org/sdr/DALA2016061604797), Jun 12, 2016: RECEPTACLE. DAMAGED. EMERGENCY LIGHT BATTERY PACK B5-234 RECEPTACLE DAMAGED. R & R SAME. OPERATION CHECKS GOOD.
- [SDR DALA2016022101278](https://openairdocs.org/sdr/DALA2016022101278), Feb 18, 2016: LOCK PIN. WORN. TAILCONE RELEASE LOCK PIN AND RECEPTICAL WORN, LEFT UPPER. REPLACED THE LT UPPER TAILCONE LOCKPINE AND RECEPTICAL IAW MM. OPS CHECK OK.
- [SDR DALA2015080204789](https://openairdocs.org/sdr/DALA2015080204789), Aug 2, 2015: SLIDE. NO TEST. TAIL CONE DROPPED AS REQUIRED, SLIDE DID NOT DEPLOY, FOUND EVIDENCE OF SLIDE EXPANSION INSIDE OF CONTAINER. REPLACED SLIDE.
- [SDR DALA2015032802556](https://openairdocs.org/sdr/DALA2015032802556), Mar 27, 2015: FUEL TANK. CORRODED. CORROSION ON CENTER TANK UPPER SKIN LT SIDE STR 5 BETWEEN BS XCW42.00 AND 58.688. REPAIRED IAW ERA, REV O.
- [SDR DALA2015032802555](https://openairdocs.org/sdr/DALA2015032802555), Mar 27, 2015: FUEL TANK. CORRODED. CORROSION ON CENTER FUEL TANK UPPER SKIN RT SIDE ON STR 9, BETWEEN XCW 58.688 AND XCW 42.00. COMPLIED WITH ERA 533302-14AD, REV O.
- [SDR DALA2015032702553](https://openairdocs.org/sdr/DALA2015032702553), Mar 26, 2015: FUEL TANK. CORRODED. CORROSION ON CENTER FUEL TANK UPPER SKIN RT SIDE ON FRONT SPAR BETWEEN XCW 58.688 AND XCW 42.000. CORROSION COMPLIED WITH ERA 533301-14 AD, REV O.
- [SDR DALA2015032702552](https://openairdocs.org/sdr/DALA2015032702552), Mar 26, 2015: FUEL TANK. CORRODED. CORROSION ON CENTER FUEL TANK UPPER SKIN RT SIDE ON STRINGER 5, BETWEEN XCW 58.688 AND SCW 42.000. REPAIRED IAW ERA 533304-14, REV O.
- [SDR DALA2015032702551](https://openairdocs.org/sdr/DALA2015032702551), Mar 26, 2015: FUEL TANK. CORRODED. CORROSION ON CENTER FUEL TANK UPPER SKIN RT SIDE ON STR 3, BETWEEN SCW 58.688 AND XCW 42.000. REPAIRED ERA 53305-14AD, REV O.
- [SDR DALA2015031902284](https://openairdocs.org/sdr/DALA2015031902284), Mar 18, 2015: INTERCOSTAL. CRACKED. SEVERAL CRACKS ON INTERCOSTAL BETWEEN FLOOR BEAMS STA 1344 TO 1364. REPLACED INTERCOSTAL IAW ERA 533320-14, REV O.
- [SDR DALA2015031702404](https://openairdocs.org/sdr/DALA2015031702404), Mar 16, 2015: FRAME. CRACKED. CRACK ON FRAME STA 1231, LONGERON 6L. R & R FRAME IAW ERA 495237-14, REV B.
- [SDR DALA2015031602275](https://openairdocs.org/sdr/DALA2015031602275), Mar 15, 2015: CARGO TRACK. CORRODED. CORROSION ON LT TIE TRACK BETWEEN, STA 1091 AND 1277. REPLACED TIE TRACK IAW SRM 51-30-01, 51-30-02, AND 51-10-05.
- [SDR DALA2015031702209](https://openairdocs.org/sdr/DALA2015031702209), Mar 13, 2015: DOUBLER. CRACKED. CRACKED INTERNAL DOUBLER ON VERTICAL STABILIZER ACCESS PLATE 370 BL CUTOUT. REPAIRED CRACK IAW SRM 5330-05, FIG 3.
- [SDR DALA2015031402204](https://openairdocs.org/sdr/DALA2015031402204), Mar 13, 2015: INTERCOSTAL. CRACKED. CRACKED INTERCOSTAL BETWEEN RT X=-4 TO X=-6, STA 994 TO 997 AT KEEL BEAM AREA. REMOVED, FABRICATED AND INSTALLED INTERCOSTAL IAW SRM 51-30-05, DWG 9936368, REV 
- [SDR DALA2015031702207](https://openairdocs.org/sdr/DALA2015031702207), Mar 12, 2015: INTERCOSTAL. CRACKED. CRACKS ON INTERCOSTAL BETWEEN FLOORBEAMS, STA 1344 TO 1364, X=0. REMOVED, FABRICATED AND INSTALLED INTERCOSTAL IAW SRM 51-30-02 AND SRM 51-30-05.
- [SDR DALA2015031302203](https://openairdocs.org/sdr/DALA2015031302203), Mar 12, 2015: BEAM. CRACKED. CRACK ON BEAM, NR 1 AT STA 163 AND STA 197 ON FORWARD PASSENGER DOOR STRUCTURE. R & R BEAM IAW SRM 51-30-00, 51-10-03, 51-10-04 AND ERA 533300-14, REV O.
- [SDR DALA2015031302202](https://openairdocs.org/sdr/DALA2015031302202), Mar 12, 2015: STRUCTURE. BENT. BENT ON PREVIOUSLY REPAIRED DOUBLER ON FORWARD PASSENGER ENTRANCE DOOR ON FORWARD LOWER CORNER. R & R DOUBLER IAW SRM 52-10-01, 51-30-00 AND 51-10-03.
- [SDR DALA2016102607791](https://openairdocs.org/sdr/DALA2016102607791), Mar 11, 2015: SKIN. CORRODED. CORROSION ON UPPER AND LOWER ELEVATOR. REPLACED ELEVATOR.
- [SDR DALA2015031202239](https://openairdocs.org/sdr/DALA2015031202239), Mar 11, 2015: BAR. CORRODED. CORROSION ON LT FLAP FLEX JOINTS LOWER BAR AND LINK. TASK 57-051-03. REPLACED IAW AMM 27-51-07-420.
- [SDR DALA2015031202238](https://openairdocs.org/sdr/DALA2015031202238), Mar 11, 2015: FRAME. CRACKED. CRACK ON RT WHEEL WELL FORWARD FRAME, 6" OF INBD BELOW HD SERVICE PANEL. R & R CHANNEL IAW SRM 51-30-02 AND 51-30-05.
- [SDR DALA2015031202237](https://openairdocs.org/sdr/DALA2015031202237), Mar 11, 2015: SKIN. CORRODED. CORROSION ON SETTLEMENT ARE OF FUEL ACCESS DOOR CUTOUTS. COMPLIED WITH WORK ON NRC 61, ZONE 500.
- [SDR DALA2015031202201](https://openairdocs.org/sdr/DALA2015031202201), Mar 11, 2015: SEAT TRACK. CORRODED. CORROSION ON SEAT TRACK FROM STA 207 - 243, X=-43, X=-44 AND X=-45. TASK 53-211-01. R & R SEAT TRACK IAW SRM 53-40-01 AND ERA 533308-14MA, REV O.
- [SDR DALA2015031202200](https://openairdocs.org/sdr/DALA2015031202200), Mar 11, 2015: SEAT TRACK. CORRODED. CORROSION ON SEAT TRACK, STA 207 TO 237, X=- 21, X=-22, X=-23. TASK 53-211-01. R & R SEAT TRACK, STA 200 - 260 IAW SRM 51-30-01, 51-30-02 AND 51-30-05 AND ERA 5
- [SDR DALA2015031202199](https://openairdocs.org/sdr/DALA2015031202199), Mar 11, 2015: SEAT TRACK. CORRODED. CORROSION ON SEAT TRACK, X=22, BS 200-220. TASK 53-211-01. R & R SEAT TRACK, STA 200 TO STA 230 IAW SRM 53-40-01, RIG 6 AND ERA 533308-14MA, REV O.
- [SDR DALA2015031002111](https://openairdocs.org/sdr/DALA2015031002111), Mar 10, 2015: BAR. CORRODED. CORROSION ON LOWER BAR AT RT FLAP FLEX JOINT. TASK 27-05-03. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. NEW BAR INSTALLED.
- [SDR DALA2015031002110](https://openairdocs.org/sdr/DALA2015031002110), Mar 9, 2015: SKIN. CORRODED. PREVIOUS BLEND OUT ON RT WING UPPER SKIN, STA 988 - 953, X=61, 67 AND 70. REMOVED CORROSION. FLAP PENNING IAW 95900-4. AREA TREATED AND PAINTED. FASTENER INSTAL
- [SDR DALA2015030902003](https://openairdocs.org/sdr/DALA2015030902003), Mar 8, 2015: CARGO TRACK. CORRODED. CORROSION ON RIGHT TIE TRACK BETWEEN, STA 1155-1212 AT C3. TASK 20-010-12. R & R TIE TRACK IAW SRM 51-30-02, 51-30-01, 51-10-05, AND 51-10-03. LP 1853329.
- [SDR DALA2015030902004](https://openairdocs.org/sdr/DALA2015030902004), Mar 7, 2015: ANGLE. CORRODED. CORROSION ON ANGLES BETWEEN RT LONGERON 28 AND 27, STA 1212-1210 AND 1268-1271, DOOR JAMB. TASK 53-123-02. ANGLES REPLACE IAW SRM 51-30-02. LP 1853601.
- [SDR DALA2015030601950](https://openairdocs.org/sdr/DALA2015030601950), Mar 5, 2015: SKIN. DENTED. DENT ON FUSELAGE SKIN BETWEEN STA 617-636, LONGERON 24R-25R. EVALUATED AND FOUND DENT CONDITION 1B.
- [SDR DALA2016102607688](https://openairdocs.org/sdr/DALA2016102607688), Mar 4, 2015: SKIN. CORRODED. CORROSION ON LEFT HAND ELEVATOR UPPER AND LOWER SKIN TASK 53-300-03. REPLACED ELEVATOR ON CARD 2730-4139LH.
- [SDR DALA2015030501949](https://openairdocs.org/sdr/DALA2015030501949), Mar 4, 2015: CHANNEL. CRACKED. RT CHANNELS CRACKED. REPAIRED IAW SRM 53-20-03.
- [SDR DALA2015030501946](https://openairdocs.org/sdr/DALA2015030501946), Mar 4, 2015: STRUCTURE. CORRODED. CORROSION ON BARREL NUT NR 21, XH=27 AT LT HORIZONTAL STABILIZER. FABRICATED AND INSTALLED BUSHING IAW SRM 55-10-03 AND DWG 5922576, REV 2.
- [SDR DALA2015030401944](https://openairdocs.org/sdr/DALA2015030401944), Mar 3, 2015: WEB. CRACKED. CRACKED WEB, STA 1542, LONGERON 5R. REMOVED WEB. FABRICATED AND INSTALLED DOUBLER IAW SRM 51-10-03, PARA 14 AND 21, AND 53-00-01.
- [SDR DALA2015030401941](https://openairdocs.org/sdr/DALA2015030401941), Mar 3, 2015: BULKHEAD WEB. CRACKED. CRACKED WEB, AFT BULKHEAD DOOR AT LT EDGE FORWARD MID SECTION. REPAIRED IAW SRM 52-00-01.
- [SDR DALA2015030401940](https://openairdocs.org/sdr/DALA2015030401940), Mar 3, 2015: CHANNEL. WORN. WORN SPLICE ON AFT CHANNEL AT RT INBD MLG DOOR. REMOVED DAMAGE. FABRICATED AND INSTALLED REPAIR ANGLE IAW EA 469617-14, REV AFC.
- [SDR DALA2015030401939](https://openairdocs.org/sdr/DALA2015030401939), Mar 3, 2015: CUSP WEB. CORRODED. CORROSION ON LT CUSP MEMBRANE UPPER AND LOWER SURFACE, BS 512 AND X=59, TASK 53-211-01. REMOVED CORROSION. FABRICATED AND INSTALLED NEW REPAIR PARTS IAW SRM 53-
- [SDR DALA2015030401938](https://openairdocs.org/sdr/DALA2015030401938), Mar 3, 2015: CUSP WEB. CORRODED. CORROSION ON LT CUSP WEB MEMBRANE UPPER AND LOWER SURFACE, BS 512, X=59, TASK 53-211-01. REPAIRED IAW SRM 53-20-02, FIG 11.
- [SDR DALA2015030401937](https://openairdocs.org/sdr/DALA2015030401937), Mar 3, 2015: SEAT TRACK. CORRODED. CORROSION OUT OF LIMITS ON RT SEAT TRACK, X=-22, BS 424 TO 427, TASK 53-211-02. REMOVED DAMAGE. REPAIR PARTS INSTALLED IAW SRM 53-40-01, FIG 2.
- [SDR DALA2015030401936](https://openairdocs.org/sdr/DALA2015030401936), Mar 3, 2015: CUSP WEB. CORRODED. CORROSION ON LT CUSP MEMBRANE, STA 769-788, X=55/60, TASK 53-211-01. DAMAGE REMOVED. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-20-02, FIG 12, 51-10-03 AN
- [SDR DALA2016102607681](https://openairdocs.org/sdr/DALA2016102607681), Mar 2, 2015: CUSP WEB. CORRODED. CORROSION ON LEFT HAND CUSP WEB AND CRACK ON WEB AND REPAIR DOUBLER. REMOVED CORROSION AND REPAIRED IAW SRM 53-20-02.

All 102: https://openairdocs.org/deregistered/N918DH-2022-11-30/reports.md

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