# N932RD: 1985 Mcdonnell Douglas DC-9-82(MD-82), registration cancelled 2018-08-21

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: August 21, 2018
- Status when cancelled: Registration expired, pending cancellation
- Airframe: [Mcdonnell Douglas DC-9-82(MD-82)](https://openairdocs.org/model/mcdonnell-douglas-dc-9-82-md-82) (registry code 3022082)
- 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: 49233
- Year built: 1985
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: May 23, 1985
- Certificate issued: April 1, 2015
- Last registry action: April 1, 2015
- Mode S code: ACEE92
- Owner when cancelled: [Jet Midwest Group LLC](https://openairdocs.org/faa-owner/JET%20MIDWEST%20GROUP%20LLC)
- Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington)
- Owner type: Corporation
- Owner's area on the map: 39.7236° N, 75.5412° W: Placed by OpenAirDocs at the center of ZIP code 19801, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N932RD
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=932RD
- Page: https://openairdocs.org/deregistered/N932RD-2018-08-21

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 DC-9-82(MD-82): https://openairdocs.org/model/mcdonnell-douglas-dc-9-82-md-82.md

## Service difficulty reports (27)

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

- [SDR RYNA201204240019](https://openairdocs.org/sdr/RYNA201204240019), Apr 24, 2012: SLIDE. LOW PRESSURE. R1 DOOR SLIDE PRESSURE NEEDLE OUT OF GREEN BAND. REPLACED R1 DOOR SLIDE IAW AMM 25-62-00.
- [SDR RYNA201202160011](https://openairdocs.org/sdr/RYNA201202160011), Feb 16, 2012: CONNECTOR. LOOSE. F/O AIRSPEED INDICATOR NOT WORKING ON TAKEOFF ROLL, RTO AT 80 KTS. FOUND LOOSE PITOT CONNECTOR ON NR 2 ADC. SECURED CONNECTOR. PERFORMED PITOT STATIC TEST OF NR
- [SDR RYNA201201160004](https://openairdocs.org/sdr/RYNA201201160004), Jan 16, 2012: BATTERY. DEFECTIVE. DURING ACCOMPLISHMENT OF FCD 33-08, FOUND NUMEROUS UPPER EMERGENCY FLOOR TRACK SECTIONS WITH WARPED, CRACKED AND BROKEN AREAS. EMERGENCY FLOOR TRACK LIGHTING SY
- [SDR RYNA2011123000023](https://openairdocs.org/sdr/RYNA2011123000023), Dec 30, 2011: WIRE HARNESS. DEFECTIVE. AIR TURNBACK - CENTER FUEL PUMP CIRCUIT BREAKER POPPED AND CREW WAS UNABLE TO GET FUEL OUT OF THE CENTER TANK. TROUBLESHOT AND FOUND DEFECTIVE FUEL HARNESS. IN 
- [SDR RYNA2011091700021](https://openairdocs.org/sdr/RYNA2011091700021), Sep 17, 2011: SKIN. PUNCTURED. AFT LOWER FUSELAGE HAS PUNCTURE AT FS 1155 APPROXIMATELY 1 INCH LONG, 7 INCHES WIDE THROUGH PRESSURIZED AREA. PERFORMED REPAIR PER SRM 53-04-3 FIGURE 5 SHEET 1.
- [SDR RYNA2011020900005](https://openairdocs.org/sdr/RYNA2011020900005), Feb 9, 2011: SLIDE. UNWANTED DEPLOY. AC 932 SLIDE INADVERTENTLY DEPLOYED. RE-PACKED TAIL CONE SLIDE, RE-INSTALLED SLIDE AND TAIL CONE.
- [SDR RYNA2010009020028](https://openairdocs.org/sdr/RYNA2010009020028), Sep 1, 2010: WARNING SYSTEM. MALFUNCTIONED. UPON TAXI OUT HAD ELEVATOR POWER ON ON LIGHT REMAIN ON. PLACE LIGHT INOP PER MEL 27-14 CAT C DDD 9/11/10 DMI 1165 ISSUED BY MXC.
- [SDR RYNA2010007020027](https://openairdocs.org/sdr/RYNA2010007020027), Jul 25, 2010: LIGHT. UNSECURE. ONE FOOT SECTION OF EMERGENCY FLOOR TRACK LIGHTING NOT SECURED TO FLOOR. RE-SECURED EMERGENCY FLOOR TRACK LIGHTING. REFERENCE MD80 MM 33-53-01. OPERATIONAL CHEC
- [SDR RYNA2010007020021](https://openairdocs.org/sdr/RYNA2010007020021), Jul 13, 2010: UNKNOWN. MALFUNCTIONED. ELEVATOR POWER LIGHT CAME ON DURING TAXI. INSPECTED CONTROL SURFACE OPERATION, NO DEFECT. PULLED AND RESET C/B P-27. OPERATIONAL CHECK SYSTEM PER MM 27-30-12 AN
- [SDR RYNA2010006020014](https://openairdocs.org/sdr/RYNA2010006020014), May 26, 2010: LIGHT. MISSING. DURING INSPECTION FOUND ONE FLOOR EMERGENCY TRACK LIGHT MISSING AT 31D AND F. REPLACED EMERGENCY FLOOR TRACK LIGHTING PER AMM 33-51-00, OPS CHECK GOOD.
- [SDR RYNA2010002170004](https://openairdocs.org/sdr/RYNA2010002170004), Feb 15, 2010: FAN BLADE. BENT. RIGHT ENGINE HAD 3 COMPRESSOR STALLS DURING CLIMB THROUGH 16,000 TO 17,000 FT. DURING TROUBLESHOOTING FOR COMPRESSOR STALL FOUND DAMAGED 1ST STAGE FAN BLADE. PE
- [SDR EE4Y090210](https://openairdocs.org/sdr/EE4Y090210), Aug 5, 2009: SUPPORT ANGLE. CRACKED. FWD CARGO COMPARTMENT DOOR AT STA Y389, BTWN BEAM NR 1 AND PAN INTERNAL WITH SUPPORT ANGLE CRACKED.
- [SDR RYNA200903200004](https://openairdocs.org/sdr/RYNA200903200004), Mar 18, 2009: PROXIMITY SENSOR. OUT OF ADJUST. ON DEPARTURE FROM SAP DURING INITIAL GEAR RETRACTION THE RED NOSE LANDING GEAR UNSAFE LIGHT REMAINED ON. RECYCLED GEAR OPS CHECK NORMAL NO FURTHER PROBLEMS WERE
- [SDR RYNA2009013100003](https://openairdocs.org/sdr/RYNA2009013100003), Jan 31, 2009: LIGHT. ILLUMINATED. FORWARD CARGO DOOR LIGHT ON AFTER TAKEOFF. FUNCTIONALLY CHECKED CARGO DOOR PROXIMITY SWITCH AS PER AMM 52-70-02. OPS CHECK NORMAL.
- [SDR RYNA2009012900002](https://openairdocs.org/sdr/RYNA2009012900002), Jan 29, 2009: PUMP. MALFUNCTIONED. ON DESCENT WITH TRANSFER PUMP & AUX PUMPS ON AND BOTH HYD PUMPS SET IN HIGH POSITION. RT HYD PUMP PRESS LOW AT APPROX 2000 PSI (LEFT PRESS NORMAL). ON FINAL APP
- [SDR RYNA2008122300047](https://openairdocs.org/sdr/RYNA2008122300047), Dec 23, 2008: LANDING GEAR. LACK OF LUBE. DURING LANDING NLG FAILED TO EXTEND, MLG INDICATION GREEN, NLG INDICATION LIGHT RED, GEAR WARNING HORN SOUNDED NLG PEDESTAL PIN WAS FLUSH. RECYCLED GEAR HANDLE 
- [SDR RYNA2008122200046](https://openairdocs.org/sdr/RYNA2008122200046), Dec 19, 2008: BUNGEE CYLINDER. DEFECTIVE. DURING LANDING NLG FAILED TO EXTEND CHECKED TILLER ALIGNMENT MLG INDICATION WAS GREEN NLG INDICATION RED NLG PEDESTAL PIN WAS FLUSH. REACCOMPLISHED GEAR EXTENSI
- [SDR RYNA200800017](https://openairdocs.org/sdr/RYNA200800017), Apr 17, 2008: SEAT TRACK. CORRODED. PASSENGER CABIN RIGHT INBOARD SEAT TRACK IS CORRODED AT BS 448. REPAIRED CORRODED AREA IAW MD-80 SRM 51-10-03.
- [SDR RYNA200800018](https://openairdocs.org/sdr/RYNA200800018), Apr 17, 2008: SEAT TRACK. CORRODED. PASSENGER CABIN LEFT INBOARD SEAT TRACK IS CORRODED AT BS 731. REPAIRED CORRODED AREA IAW MD-80 SRM 51-10-03.
- [SDR RYNA200800022](https://openairdocs.org/sdr/RYNA200800022), Apr 17, 2008: FAIRING. CRACKED. RIGHT WING OUTBOARD AILERON TAB, OUTBOARD FAIRING IS CRACKED AT THE TOP. REPAIRED CRACKED AILERON IAW MD-80 SRM 51-70-4.
- [SDR RYNA200800019](https://openairdocs.org/sdr/RYNA200800019), Apr 17, 2008: SEAT TRACK. CORRODED. PASSENGER CABIN LEFT INBOARD SEAT TRACK IS CORRODED AT BS 693. REPAIRED CORRODED AREA IAW MD-80 SRM 51-10-03.
- [SDR RYNA200800021](https://openairdocs.org/sdr/RYNA200800021), Apr 17, 2008: SEAT TRACK. CORRODED. PASSENGER CABIN LEFT INBOARD SEAT TRACK IS CORRODED AT BS 1212 - 1287. REPAIRED CORRODED AREA IAW MD-80 SRM 51-10-03.
- [SDR RYNA200800020](https://openairdocs.org/sdr/RYNA200800020), Apr 17, 2008: SEAT TRACK. CORRODED. PASSENGER CABIN RIGHT INBOARD SEAT TRACK IS CORRODED AT BS 1078. REPAIRED CORRODED AREA IAW MD-80 SRM 51-10-03.
- [SDR RYNA200800015](https://openairdocs.org/sdr/RYNA200800015), Apr 17, 2008: SEAT TRACK. CORRODED. PASSENGER CABIN RIGHT INBOARD SEAT TRACK IS CORRODED AT BS 1022-1060. REPAIRED CORRODED ARE IAW SRM 51-10-03.
- [SDR RYNA200800016](https://openairdocs.org/sdr/RYNA200800016), Apr 17, 2008: SEAT TRACK. CORRODED. PASSENGER CABIN RIGHT INBOARD SEAT TRACK IS CORRODED AT BS 579. REPAIRED CORRODED ARE IAW MD-80 SRM 51-10-03.
- [SDR RYNA200800023](https://openairdocs.org/sdr/RYNA200800023), Apr 11, 2008: BRACE. CRACKED. FUSELAGE TO LEFT WING FAIRING SUPPORT BRACES ARE CRACKED AT BS 807 NEAR WING LEADING EDGE AREA. REPLACED CRACKED SUPPORT BRACES PER MD-80 SRM 51-10-2.
- [SDR RYNA200500023](https://openairdocs.org/sdr/RYNA200500023), Jul 20, 2005: GASKET. FAILED. TAIL COMPARTMENT TEMPATURE HIGH LIGHT ILLUMINATED DURING CLIMB. REMOVED AND REPLACED TWO GASKETS ON THE PNEUMATIC ICE CONTROL ANTICIPATOR AND BLEED AIR SUPPLY H

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