# N932DN: 1996 Mcdonnell Douglas MD-90-30, registration cancelled 2020-08-25

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: August 25, 2020
- Status when cancelled: Sale reported
- 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: 53457
- Year built: 1996
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: December 29, 2011
- Last registry action: August 25, 2020
- Mode S code: ACED6F
- Location: [Atlanta, GA](https://openairdocs.org/faa-place/GA/Atlanta)
- Owner type: Individual
- 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/N932DN
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=932DN
- Page: https://openairdocs.org/deregistered/N932DN-2020-08-25

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 (62, newest 50)

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

- [SDR DALA2017101107440](https://openairdocs.org/sdr/DALA2017101107440), Oct 5, 2017: LIGHT. INOPERATIVE. LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. R & R EMERGENCY LIGHT. OPS CHECKED GOOD.
- [SDR DALA2017020801054](https://openairdocs.org/sdr/DALA2017020801054), Feb 2, 2017: OIL COOLER. LEAKING. NR 2 ENGINE OIL QUANTITY LOW. DECREASED TO 0 ON ARRIVAL. TEMPERATURE AND PRESSURE NORMAL. FOUND OIL COOLER LEAKING. REMOVED AND REPLACED #2 FUEL/OIL COOLER PER 
- [SDR DALA2017020100923](https://openairdocs.org/sdr/DALA2017020100923), Feb 1, 2017: NOT REPORTED. NOT REPORTED. IN FLARE, RECEIVED A LANDING GEAR AUDIBLE WARNING. ALL 3 GEAR GREEN. GEAR DOOR OPEN LIGHT WAS EXTINGUISHED. WENT AROUND AND LANDED NORMALLY. REPLACED S1-412. AL
- [SDR DALA2017013000854](https://openairdocs.org/sdr/DALA2017013000854), Jan 28, 2017: WARNING MESSAGE. ILLUMINATED. AT CRUISE FL320 RECEIVED AN "SINGLE ELEV FEEL" FAULT OAP MESSAGE. AUTOPILOT REMAINED ENGAGED. DESCENDED TO FL 280. MAINTENANCE TROUBLESHOT. PERFORMED ACS RTS. R
- [SDR DALA2016122910187](https://openairdocs.org/sdr/DALA2016122910187), Dec 28, 2016: WEB. DAMAGED. HOLE IN FLOOR MEMBRANE JUST FORWARD OF BS 200, LBL 7. FOUND TO BE OUT OF LIMITS. REPAIRED WEB MEMBRANE IAW ERA 551879-14, REV O. (LP# 2825970)
- [SDR DALA2016122410118](https://openairdocs.org/sdr/DALA2016122410118), Dec 23, 2016: FLOOR SUPPORT. CORRODED. MAIN CABIN FORWARD WET AREA, BS 256, RBL 22 FLOOR SUPPORT CORRODED. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-30-05 AND DWG 59305
- [SDR DALA2016122410117](https://openairdocs.org/sdr/DALA2016122410117), Dec 23, 2016: SEAT TRACK. CORRODED. MAIN CABIN SEAT TRACK, BS 150 TO 200 RBL 7 IS CORRODED. ROUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-30-01 AND DWG 9936534, REV BW.
- [SDR DALA2016122410116](https://openairdocs.org/sdr/DALA2016122410116), Dec 23, 2016: SEAT TRACK. CORRODED. MAIN CABIN SEAT TRACK, BS 150 TO 200 LBL 7 CORRODED. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-30-01 AND DWG 9936534.
- [SDR DALA2016122310112](https://openairdocs.org/sdr/DALA2016122310112), Dec 22, 2016: FLOOR SUPPORT. CORRODED. GALLEY FLOOR SUPPORT IN FORWARD WET AREA, BS 160 RBL 19 CORRODED. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-30-05 AND DWG 9936534
- [SDR DALA2016122310111](https://openairdocs.org/sdr/DALA2016122310111), Dec 22, 2016: FLOOR SUPPORT. CORRODED. GALLEY FLOOR SUPPORT IN FORWARD WET AREA, BS 160, RBL 19 CORRODED. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-30-05 AND DWG 993653
- [SDR DALA2016122210110](https://openairdocs.org/sdr/DALA2016122210110), Dec 21, 2016: FLOOR SUPPORT. CORRODED. MAIN CABIN FLOOR SUPPORT CORRODED AT BS 200 LBL 8. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-30-02 AND DWG 9936534.
- [SDR DALA2016122210109](https://openairdocs.org/sdr/DALA2016122210109), Dec 21, 2016: FLOOR SUPPORT. CORRODED. MAIN CABIN FLOOR SUPPORT BS 212, RBL 12 CORRODED. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-30-02 AND DWG 9936535, REV CS.
- [SDR DALA2016122210108](https://openairdocs.org/sdr/DALA2016122210108), Dec 21, 2016: FLOORBEAM. CORRODED. MAIN CABIN FLOORBEAM CORRODED AT BS 200, RBL 7 TO LBL 7. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-30-02 AND DWG 9936534, REV BW.
- [SDR DALA2016122210107](https://openairdocs.org/sdr/DALA2016122210107), Dec 21, 2016: FLOORBEAM. CORRODED. MAIN CABIN FLOORBEAM BS 200 RBL 9 TO RBL 44 IS CORRODED. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-30-02 AND DWG 9936534, REV BW.
- [SDR DALA2016122210106](https://openairdocs.org/sdr/DALA2016122210106), Dec 21, 2016: FLOOR SUPPORT. CORRODED. MAIN CABIN FLOOR SUPPORT CORRODED BETWEEN BS 160 - 200, RBL 44. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-30-02 AND DWG 99365
- [SDR DALA2016122310115](https://openairdocs.org/sdr/DALA2016122310115), Dec 20, 2016: FLOOR SUPPORT. CORRODED. MAIN CABIN FORWARD WET AREA LBL 20 FLOOR SUPPORT INBOARD LOBES CORRODED AT BS 210. OUT OF LIMITS. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 53-10-01 AND DWG 29
- [SDR DALA2016122010008](https://openairdocs.org/sdr/DALA2016122010008), Dec 19, 2016: FLOOR SUPPORT. CORRODED. MAIN CABIN FLOOR SUPPORT, STA 160-200, LBL 43 CORRODED. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED SUPPORT IAW SRM 51-30-05 AND DWG 9936534.
- [SDR DALA2016121910006](https://openairdocs.org/sdr/DALA2016121910006), Dec 18, 2016: FLOOR SUPPORT. CORRODED. MAIN CABIN FLOOR SUPPORT, STA 160, RBL 50 CORRODED. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED SUPPORT IAW SRM 51-30-05 AND DWG 936534, REV BW.
- [SDR DALA2016121810005](https://openairdocs.org/sdr/DALA2016121810005), Dec 17, 2016: ATTACH ANGLE. CRACKED. LEFT HAND VERTICAL STABILIZER ATTACH ANGLE CRACKED. REMOVED AND REPLACED SAME IAW SRM 51-30-05 AND DWG 5912188, REV BD.
- [SDR DALA2016121810004](https://openairdocs.org/sdr/DALA2016121810004), Dec 17, 2016: FITTING. CORRODED. MAIN CABIN FORWARD WET AREA GIRT BAR SUBFLOOR FITTING, 2 EACH, CORRODED AT R1 DOOR CUTOUT. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED 2 EACH FITTINGS IAW S
- [SDR DALA2017010200057](https://openairdocs.org/sdr/DALA2017010200057), Dec 12, 2016: STIFFENER. CRACKED. NR 2 ENGINE NOSE COWLING FORWARD BULKHEAD HAS 1 VERTICAL STIFFENER CRACKED. REMOVED NR 2 ENGINE NOSE COWL IAW MM.
- [SDR DALA2017010200056](https://openairdocs.org/sdr/DALA2017010200056), Dec 12, 2016: STIFFENER. CRACKED. NR 1 ENGINE NOSE COWL FORWARD BULKHEAD HAS 4 VERTICAL STIFFENERS CRACKED. REMOVED AND REPLACED NOSE COWLING IAW MM.
- [SDR DALA2016120909736](https://openairdocs.org/sdr/DALA2016120909736), Dec 5, 2016: DOOR FRAME. CRACKED. FOUND CRACK ON FORWARD SIDE OF RIGHT MAIN LANDING GEAR DOOR CUT OUT. REMOVED CRACKED FRAME. INSTALLED NEW FRAME IAW DWG 5930584. (LP# 9389232)
- [SDR DALA2016120909735](https://openairdocs.org/sdr/DALA2016120909735), Dec 5, 2016: SKIN. CRACKED. CRACK ON LEFT FORWARD SIDE OF MAIN LANDING GEAR DOOR CUT OUT. REPLACED FRAME IAW DWG 5930584.
- [SDR DALA2015042302868](https://openairdocs.org/sdr/DALA2015042302868), Apr 23, 2015: PIN. DISENGAGED. PARACHUTE PIN IS DISENGAGED ON L1 DOOR SLIDE. R & R FWD ENTRY DOOR SLIDE IAW AMM AND JIC 2561-01358-02A.
- [SDR DALA2015011400304](https://openairdocs.org/sdr/DALA2015011400304), Jan 13, 2015: SLIDE. DAMAGED. TAILCONE SLIDE PACK UNRAVELING. R & R SLIDE IAW AMDS 2561-4643.
- [SDR DALA2015011400306](https://openairdocs.org/sdr/DALA2015011400306), Jan 12, 2015: FRAME. CRACKED. FRAME WEB, BS 1520, CRACKED. REPAIRED IAW ERA 531910-14, SECTION I.
- [SDR DALA2015011200291](https://openairdocs.org/sdr/DALA2015011200291), Jan 10, 2015: DOOR FRAME. CORRODED. CORROSION FOUND IN FASTENER HOLE ON THE AFT CARGO DOOR LOWER JAMB BEAM. ERA 531852-14 SECTION I WAS ACCOMPLISHED.
- [SDR DALA2015011200288](https://openairdocs.org/sdr/DALA2015011200288), Jan 10, 2015: SKIN. CRACKED. FUSELAGE EXTERIOR SKIN CRACKED AT BS 1531, 15" STAIRWAY CUTOUT, RT SIDE. REMOVED DAMAGE HFEC FOR CONTAINMENT. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER
- [SDR DALA2015011100283](https://openairdocs.org/sdr/DALA2015011100283), Jan 10, 2015: DOOR SILL. CORRODED. C3 LOWER SILL CORRODED. REPAIRED IAW PRI/ERA 531852-14, REV 3.
- [SDR DALA2015011100282](https://openairdocs.org/sdr/DALA2015011100282), Jan 10, 2015: BULKHEAD WEB. CRACKED. TAIL INTERIOR, LT VENT BOX, CANTED BS 1531 BULKHEAD WEB CRACKED. REPAIRED IAW PRI/ ERA 531910-14, REV O.
- [SDR DALA2015011100281](https://openairdocs.org/sdr/DALA2015011100281), Jan 10, 2015: LONGERON. CRACKED. FOUND CRACKED LONGERON 2R, AFT OF BS 1458. COMPLIED WITH PRI, FINAL ERA 531964-14, REV O.
- [SDR DALA2015011200293](https://openairdocs.org/sdr/DALA2015011200293), Jan 9, 2015: SKIN. DAMAGED. SKIN BS 1475. LONGERON 2L FOUND DAMAGED. REPAIRED IAW ERA 491741-14, REV A
- [SDR DALA2015011200292](https://openairdocs.org/sdr/DALA2015011200292), Jan 9, 2015: SKIN. CRACKED. CRACK FOUND ON SKIN COMMON TO LONGERON 2R JUST AFT OF BS 1475. ERA 531964-14, SECTION I WAS ACCOMPLISHED.
- [SDR DALA2015010800280](https://openairdocs.org/sdr/DALA2015010800280), Jan 7, 2015: SKIN. CRACKED. AFT FUSELAGE SKIN, BELOW RAM AIR INLET, CRACKED BS 1486, STRINGER 2L. REPAIRED IAW PRI 491741-14, REV A.
- [SDR DALA2015010800279](https://openairdocs.org/sdr/DALA2015010800279), Jan 7, 2015: SKATE ANGLE. CRACKED. FUSELAGE EXTERIOR VERTICAL STABILIZER SKATE ANGLE CRACKED AND RIVET POPPED, CANTED BS 1531, RT SIDE. COMPLIED WITH PRI 531878-14, REV O.
- [SDR DALA14035909232](https://openairdocs.org/sdr/DALA14035909232), Jun 13, 2014: WEB. DAMAGED. BS 101.55 CAPTAIN`S SIDE ELEVATOR CABLE FEED THROUGH AND WEB DAMAGED. REPAIRED IAW ERA 526158-14, REV O.
- [SDR DALA14033579232](https://openairdocs.org/sdr/DALA14033579232), Jun 3, 2014: OIL SYSTEM. LEAKING. PERFORMED AN IN FLIGHT SHUTDOWN AND AN AIR TURN BACK DUE TO LT ENGINE OIL QUANTITY LOSS WITH OIL QTY INDICATION AT ZERO. MAINTENANCE FOUND OIL IN COWLING AND ON
- [SDR DALA14028389232](https://openairdocs.org/sdr/DALA14028389232), May 4, 2014: PIN. PULLED. DURING SERVICE CHECK, FOUND L1 DOOR SLIDE PINS PULLED FROM SLIDE PACK COVER. R & R L1 DOOR SLIDE.
- [SDR DALA14003209232](https://openairdocs.org/sdr/DALA14003209232), Jan 11, 2014: RELEASE CABLE. PULLED. DURING SERVICE CHECK, COCKPIT DOOR RELEASE CABLES PULLED OUT OF DOOR HINGES. MAINTENANCE R & R UPPER AND LOWER COCKPIT DOOR HINGE CABLES IAW AMM. OPERATION CHEC
- [SDR DALA13059189232](https://openairdocs.org/sdr/DALA13059189232), Nov 3, 2013: BOTTLE. OUT OF TOLERANCE. DURING SERVICE CHECK, MAINTENANCE FOUND TAILCONE EVACUATION SLIDE DISCHARGE BOTTLE PRESSURE OUT OF RANGE. MAINTENANCE REMOVED AND REPLACED TAILCONE SLIDE.
- [SDR DALA13051179232](https://openairdocs.org/sdr/DALA13051179232), Sep 26, 2013: OVEN. CONTAMINATED. FIRST CLASS GALLEY OVEN STARTED SMOKING WHEN IT WAS TURNED ON. MX INSPECTED CONTENTS OF OVEN, NO SPILT FOOD OR SAUCE. FD TO MCO/PLAC IAW MEL 25-34-02. CIRCUIT B
- [SDR DALA13041389232](https://openairdocs.org/sdr/DALA13041389232), Aug 26, 2013: BALLAST. FAILED. AFT F/A WITNESSED SMOKE AND ELECTRICAL ODOR FROM OVERHEAD LAST ROW OF SEATS. MX FOUND CEILING LIGHT BALLAST FORWARD END AT 37CDE BURNED/SHORTED TO MOUNT SCREW. 
- [SDR DALA13033249232](https://openairdocs.org/sdr/DALA13033249232), Jun 27, 2013: OVEN. INOPERATIVE. FORWARD GALLEY OVEN, SMALL AMOUNT OF SMOKE OMITTED VERY HOT. OVEN OFF. INSPECTED FORWARD GALLEY OVEN AND CIRCUIT BREAKER PANEL. NO TROUBLE FOUND. PULLED FOWARD 
- [SDR DALA13021049232](https://openairdocs.org/sdr/DALA13021049232), May 3, 2013: SKIN. DAMAGED. FUSELAGE SKIN AFT OF L1 DOOR PUNCTURED BETWEEN L17L AND L18L. REMOVED DAMAGED SKIN IAW SRM 53-30-01. FABRICATED, TREATED, PRIMED AND INSTALLED DOUBLER AND FILLE
- [SDR DALA13021039232](https://openairdocs.org/sdr/DALA13021039232), May 3, 2013: SHEAR TIE. BENT. SHEAR TIE AT STA 237 BENT BETWEEN L17 AND L18. REMOVED SHEAR TIE. STRAIGHTENED HFEC INSPECTED FORMER. NO CRACKS. REPAIRED IAW ERA 514591-14. INSTALLED IAW DWG 9
- [SDR DALA13017609232](https://openairdocs.org/sdr/DALA13017609232), Apr 17, 2013: STRUCTURE. CRACKED. CEILING CLIP CRACKED AT 12 O'CLOCK POSITION AT BS 1475. REMOVED AND REPLACED CLIP IAW DWG PL 9964460.
- [SDR DALA13006749232](https://openairdocs.org/sdr/DALA13006749232), Feb 8, 2013: RELEASE MECH. OUT OF TOLERANCE. DURING TAILCONE FUNCTIONAL CHECK STEP 4 OF AMDS CARD 5352-7116, MX FOUND TAILCONE RELEASE OUT OF LIMITS. RELEASED TO HIGH. ADJUSTED CLIPS ON TEE PIN AND PULL HA
- [SDR DALA13006739232](https://openairdocs.org/sdr/DALA13006739232), Feb 7, 2013: WEB. CRACKED. CANTED FRAME BS 964 WEB AFT SIDE CRACKED. 6 INCHES ABOVE LT VENT BOX AT TOP FASTENER. VERIFIED WITH HFEC. REMOVED DAMAGE. CONTAINED. FABRICATED REPAIR DOUBLER, 
- [SDR DALA13006809232](https://openairdocs.org/sdr/DALA13006809232), Feb 6, 2013: D-RING. WORN. SLIDE D-RINGS ATTACHED AT AFT VENTRAL WALKWAY WORN-FRAYED. R & R SLIDE D-RINGS ATTACH STRAPS AT AFT VENTRAL STAIRWAY IAW AMM. OPS CHECKS GOOD.

All 62: https://openairdocs.org/deregistered/N932DN-2020-08-25/reports.md

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