# N93875: 1982 Mcdonnell Douglas DC-9-82(MD-82), registration cancelled 2013-08-16

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: August 16, 2013
- Status when cancelled: Sale reported, canceled
- 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: 49125
- Year built: 1982
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard
- Airworthiness date: August 24, 1984
- Last registry action: March 21, 2005
- Mode S code: AD06CC
- Location: [Cedar Rapids, IA](https://openairdocs.org/faa-place/IA/Cedar%20Rapids)
- Owner type: Individual
- Owner's area on the map: 42.0232° N, 91.6596° W: Placed by OpenAirDocs at the center of ZIP code 52402, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N93875
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=93875
- Page: https://openairdocs.org/deregistered/N93875-2013-08-16

From the FAA registry file of October 29, 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 (96, newest 50)

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

- [SDR CALA0000003](https://openairdocs.org/sdr/CALA0000003), Jan 8, 2000: ACTUATOR. INOPERATIVE. THE LT AND RT MAIN GEAR RED UNSAFE LIGHTS REMAINED ILLUMINATED AFTER TAKEOFF FROM EWR. THE ABNORMAL CHECKLIST WAS FOLLOWED, BUT THE LIGHTS REMAINED ON. THE LIGH
- [SDR CALA9901422](https://openairdocs.org/sdr/CALA9901422), Oct 20, 1999: POWER SUPPLY. INOP. INSPECTION FOUND CABIN OVERHEAD EMERGENCY LIGHTS FORWARD OF OVERWING EXITS INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHTS POWER SUPPLY AND OPERATION CHE
- [SDR CALA9901337](https://openairdocs.org/sdr/CALA9901337), Oct 7, 1999: ACTUATOR. INOP. THE LT MLG SHOWED RED UNSAFE LIGHT WITH DOOR LIGHT OUT AFTER GEAR RETRACTION. THE GEAR WAS RECYCLED IAW CHECKLIST AND GEAR INDICATED NORMAL. THE LT GEAR ACTUATI
- [SDR CALA9901234](https://openairdocs.org/sdr/CALA9901234), Sep 15, 1999: SPAR CAP. CRACKED. INSPECTION FOUND A 3.5 INCH CRACK IN LT WING FLAP TRAILING EDGE CAP JUST O/B OF FLEX JOINT ASSEMBLY. REPAIRED IAW SRM 57-03, FIGURE 9 AND MM 51-00-00.
- [SDR CALA9901216](https://openairdocs.org/sdr/CALA9901216), Sep 14, 1999: PANEL. CRACKED. INSPECTION FOUND A 3 INCH CRACK IN RT WING TRAILING EDGE PANEL NR 1610. THE PANEL WAS REPAIRED IAW SRM 51-30-2.
- [SDR CALA9901215](https://openairdocs.org/sdr/CALA9901215), Sep 14, 1999: SUPPORT. BENT. INSPECTION FOUND AFT PIT FORWARD BULKHEAD CENTER VERTICAL SUPPORT BENT AT FS 1007, BL 0. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW 51-10-4, 51
- [SDR CALA9901214](https://openairdocs.org/sdr/CALA9901214), Sep 14, 1999: DOUBLER. CRACKED. INSPECTION FOUND A .75 INCH CRACK IN LT MLG DOOR LOWER LT CORNER DOUBLER. THE DOUBLER WAS REMOVED AND A NEW DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 28.
- [SDR CALA9901213](https://openairdocs.org/sdr/CALA9901213), Sep 14, 1999: SLAT. DENTED. INSPECTION FOUND RT WING 0 SLAT DENTED. REPAIRED SLAT IAW ECRA 5720-01170.
- [SDR CALA9901212](https://openairdocs.org/sdr/CALA9901212), Sep 14, 1999: PANEL. CRACKED. INSPECTION FOUND A 1.5 CRACK IN RT HORIZONTAL STABILIZER PANEL NR 3804 L/E. THE CRACKED AREA WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 51-30-2, 55-01, 51-3
- [SDR CALA9901211](https://openairdocs.org/sdr/CALA9901211), Sep 14, 1999: TIE STRAP. CORRODED. INSPECTION FOUND TIE STRAP CORRODED AT LEFT AFT SERVICE DOOR CUTOUT, FS 1136, LONGERON 27R. THE TIE STRAP WAS REMOVED AND A NEW TIE STRAP WAS INSTALLED IAW SRM 
- [SDR CALA9901210](https://openairdocs.org/sdr/CALA9901210), Sep 14, 1999: SKIN. DENTED. INPECTION FOUND LEFT WING 0 SLAT DENTED. THE SLAT WAS REPAIRED IAW ECRA 5720-01120.
- [SDR CALA9901209](https://openairdocs.org/sdr/CALA9901209), Sep 14, 1999: PAN. GOUGED. INSPECTION FOUND AFT CARGO DOOR GOUGED ON PAN AROUND DOOR STOPS. REPAIR DOUBLERS WERE INSTALLED IAW SRM 52-03, 51-10-4, 52-03, FIGURE 8 AND EA 5233-2-A0495.
- [SDR CALA9901204](https://openairdocs.org/sdr/CALA9901204), Sep 12, 1999: SKIN. DENTED. INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 140, LONGERON 19R. REPAIRED IAW SRM 53-04, FIGURE 38, SHEET 22, VIEW I.
- [SDR CALA9901203](https://openairdocs.org/sdr/CALA9901203), Sep 12, 1999: DOUBLER. CORRODED. INSPECTION FOUND LOWER FUSELAGE EXTERNAL CUTOUT FOR NR 2 AD ANTENNA CORRODED BETWEEN SKIN AND INTERNAL DOUBLER AND MATING SURFACE AT FS 484-503, LONGERON 29L AN
- [SDR CALA9901202](https://openairdocs.org/sdr/CALA9901202), Sep 12, 1999: PANEL. CORRODED. INSPECTION FOUND KEEL ACCESS PANEL BETWEEN BOTH MLG DOORS CORRODED ON ONE END AT FS 864-870. A NEW PANEL WAS INSTALLED IAW SRM 51-10-4, 51-10-3, AND 51-00-60.
- [SDR CALA9901201](https://openairdocs.org/sdr/CALA9901201), Sep 12, 1999: ANGLE. CRACKED. INSPECTION FOUND 3 CRACKS IN CENTER WING TO BODY FAIRING SUPPORT ANGLES(3) AT STA 875, BL 0. THE ANGLES WERE REMOVED AND NEW ANGLES WERE INSTALLED IAW SRM 51-10
- [SDR CALA9901200](https://openairdocs.org/sdr/CALA9901200), Sep 12, 1999: PANEL. CRACKED. INSPECTION FOUND CRACKS IN VERTICAL STABILIZER PANEL NR 6404. THE CRACKS WERE 1-2 INCHES LONG. THE PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLED IAW SRM 51-30
- [SDR CALA9901198](https://openairdocs.org/sdr/CALA9901198), Sep 12, 1999: TAB. DISBONDED. INSPECTION FOUND RUDDER TRIM TAB METAL TAB DISBONDED ON RT SIDE OF TAB. THE RUDDER TAB WAS REMOVED AND THE METAL TAB WAS REMOVED AND REPLACED. THE RUDDER TAB WA
- [SDR CALA9901197](https://openairdocs.org/sdr/CALA9901197), Sep 12, 1999: FITTING. CRACKED. INSPECTION FOUND A .25 INCH CRACK IN RT WING NR 5 SLAT O/B FITTING. THE FITTING WAS REMOVED, REPAIRED AND REINSTALLED IAW SRM 51-30-2, 51-30-8, AND ECRA 5750-03
- [SDR CALA9901196](https://openairdocs.org/sdr/CALA9901196), Sep 12, 1999: SKIN. CRACKED. INSPECTION FOUND A 2.2 INCH CRACK IN RT I/B SPOILER FIXED SUPPORT PANEL. THE CRACKED AREA OF SKIN WAS REMOVED AND A NEW PLATE WAS INSTALLED IAW SRM 51-30-1 AND 
- [SDR CALA9901195](https://openairdocs.org/sdr/CALA9901195), Sep 12, 1999: WEB. PUNCTURED. INSPECTION FOUND A SMALL HOLE PUNCTURED IN CUSP WEB AT FS 1050, RBL 59. THE PUNCTURED AREA WAS REMOVED AND A DOUBLER WAS INSTALLED IAW SRM 51-30-5, 51-10-2, AND
- [SDR CALA9901194](https://openairdocs.org/sdr/CALA9901194), Sep 12, 1999: ANGLE. CORRODED. INSPECTION FOUND FALSE BULKHEAD LOWER ATTACH ANGLE CORRODED AT FS 1333, LONGERON 28L-28R. THE ATTACH ANGLE WAS REMOVED AND A NEW ANGLE AND DOUBLER WERE INSTALLE
- [SDR CALA9901193](https://openairdocs.org/sdr/CALA9901193), Sep 12, 1999: FRAME. CORRODED. INSPECTION FOUND FRAME LOWER LOBE AND WEB CORRODED AT FS 1269, LONGERON 28L-28R. THE CORRODED AREA WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 51-10-2, 51-10
- [SDR CALA9901192](https://openairdocs.org/sdr/CALA9901192), Sep 12, 1999: WEB. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN SUBFLOOR CUSP WEB AT STA 195, RBL 9. THE SUBFLOOR CUSP WEB WAS REPAIRED IAW SRM 53-01, FIGURE 4, SHEET 3.
- [SDR CALA9901191](https://openairdocs.org/sdr/CALA9901191), Sep 12, 1999: LONGERON. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN LONGERON 27L AT FS 256. THE CRACKED SECTION OF LONGERON WAS REMOVED AND A NEW SPLICE AND LONGERON WERE INSTALLED IAW SRM 53-1
- [SDR CALA9901190](https://openairdocs.org/sdr/CALA9901190), Sep 12, 1999: SUPPORT. CORRODED. INSPECTION FOUND LT FLOOR SUPPORT CORRODED AT FS 1155, JUST O/B OF I/B SEAT TRACK. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-5
- [SDR CALA9901189](https://openairdocs.org/sdr/CALA9901189), Sep 12, 1999: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM WEB CORRODED AT STA 1338, RBL 54.5 AND RBL 35-45. THE CORRODED AREAS WERE CUT OUT AND REPAIRS WERE INSTALLED IAW SRM 53-01, FIGURE 4,
- [SDR CALA9901188](https://openairdocs.org/sdr/CALA9901188), Sep 12, 1999: FLOOR. CORRODED. INSPECTION FOUND CABIN LT FLOOR SKIN CORRODED AT FS 1138, LBL 42. INSTALLED NEW SKIN AND SUPPORTS IAW SRM 51-30-2, 51-30-3, AND 51-30-5.
- [SDR CALA9901187](https://openairdocs.org/sdr/CALA9901187), Sep 12, 1999: FLOOR. CORRODED. INSPECTION FOUND CABIN LT FLOOR SKIN CORRODED AT FS 1183, LBL 42. REMOVED FORWARD AND AFT FRAME FITTINGS TORQUE BOX DOUBLER AND VERTICAL STIFFENER IAW SRM 51-30
- [SDR CALA9901186](https://openairdocs.org/sdr/CALA9901186), Sep 12, 1999: SUPPORT. CORRODED. INSPECTION FOUND AFT LT SERVICE DOOR LOWER CUTOUT FLOOR LEVEL SUPPORT CORRODED AT FS 1330-1338, LBL 14. A NEW SUPPORT WAS INSTALLED IAW SRM 51-10-4, 51-10-3, AN
- [SDR CALA9901185](https://openairdocs.org/sdr/CALA9901185), Sep 12, 1999: FLOOR. CORRODED. INSPECTION FOUND COCKPIT RT FLOOR SKIN CORRODED AT FS 148, RBL 6. THE CORRODED AREA WAS CUT OUT, FILLER AND DOUBLER WERE INSTALLED IAW SRM 53-01, FIGURE 4, 51-1
- [SDR CALA9901183](https://openairdocs.org/sdr/CALA9901183), Sep 12, 1999: ANGLE. CORRODED. INSPECTION FOUND L-ANGLE ABOVE LONGERON 18R AT STA 148-160 CORRODED. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2, 51-10-4, AND 51-10-3.
- [SDR CALA9901182](https://openairdocs.org/sdr/CALA9901182), Sep 12, 1999: SUBFLOOR. CORRODED. INSPECTION FOUND SUBFLOOR CORRODED AT STA 218, LBL 42-44. THE SUBFLOOR WEB AND STIFFENERS WERE REMOVED AND A NEW WEB AND STIFFENERS WERE INSTALLED IAW SRM 53-10
- [SDR CALA9901181](https://openairdocs.org/sdr/CALA9901181), Sep 12, 1999: SUBFLOOR. CORRODED. INSPECTION FOUND SUBFLOOR CORRODED AT STA 200, LBL 40 AND LBL 18 TO RBL 30. THE SUBFLOOR AREAS WERE REPAIRED IAW SRM 51-30-2, 53-05, FIGURE 25, 51-30-5, AND 53-
- [SDR CALA9901180](https://openairdocs.org/sdr/CALA9901180), Sep 12, 1999: SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 200, BL 0 TO LBL 12 AND LBL 40. THE FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW SRM 51-30-2, 53-14-1, 51-10-3, 
- [SDR CALA9901179](https://openairdocs.org/sdr/CALA9901179), Sep 12, 1999: SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 157-200, BL 0 AND STA 200, BL 0 TO RBL 40. THE SUPPORTS WERE REMOVED AND REPLACED IAW SRM 53-14-1, FIGURE 11, 51
- [SDR CALA9901178](https://openairdocs.org/sdr/CALA9901178), Sep 12, 1999: SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 157-180, RBL 40. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-2, 51-30-5, AND 51-10-3.
- [SDR CALA9901177](https://openairdocs.org/sdr/CALA9901177), Sep 12, 1999: SEAT TRACK. CORRODED. INSPECTION FOUND AFT RIGHT O/B SEAT TRACK CORRODED AT STA 1022-1041, RBL 54.5 AND STA 1092-1243, RBL 54.5. THE CORRODED SECTIONS OF SEAT TRACK WERE REMOVED AND 
- [SDR CALA9901176](https://openairdocs.org/sdr/CALA9901176), Sep 12, 1999: SEAT TRACK. CRACKED. INSPECTION FOUND A 3 INCH CRACK IN LT CENTER SEAT TRACK AT FS 1309, LBL 22. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-1, 51-30-5, 51-10-3, AND 53-05
- [SDR CALA9901175](https://openairdocs.org/sdr/CALA9901175), Sep 12, 1999: DOUBLER. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN RT COCKPIT SLIDING WINDOW CUTOUT UPPER AFT CORNER INSIDE DOUBLER. THE DOUBLER WAS REMOVED AND A NEW DOUBLER WAS INSTALLED IAW
- [SDR CALA9901199](https://openairdocs.org/sdr/CALA9901199), Sep 10, 1999: SKIN. PUNCTURED. INSPECTION FOUND A HOLE THROUGH SKIN AND RIB OF VERTICAL STABILIZER AFT UPPER STRINGER TIP FAIRING. THE RIB AND SKIN WERE REPAIRED IAW SRM 55-01, FIGURES 2 & 4.
- [SDR CALA9901170](https://openairdocs.org/sdr/CALA9901170), Sep 10, 1999: POWER SUPPLY. INOP. INSPECTION FOUND EMERGENCY OVERWING AFT LIGHT INOPERATIVE. THE BATTERY POWER SUPPLY WAS REMOVED AND REPLACED IAW MM 33-50-22.
- [SDR CALA9901206](https://openairdocs.org/sdr/CALA9901206), Sep 9, 1999: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT STA 294, BL 0 TO RBL 50 AND STA 328, BL 0 TO RBL 50. NEW FLOORBEAM SECTIONS WERE INSTALLED IAW SRM 53-10-51.
- [SDR CALA9901167](https://openairdocs.org/sdr/CALA9901167), Sep 8, 1999: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM UPPER CHORD CORRODED AT STA 1332, LBL 34 TO 42.5. A REPAIR ANGLE WAS INSTALLED IAW SRM 51-10-3 AND 53-05, FIGURE 20A.
- [SDR CALA9901166](https://openairdocs.org/sdr/CALA9901166), Sep 8, 1999: SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 1155, LONGERON 28R-29R. A NEW SUPPORT WAS INSTALLED IAW SRM 51-10-2, 51-10-4, 51-10-3, AND 51-30-5.
- [SDR CALA9901165](https://openairdocs.org/sdr/CALA9901165), Sep 8, 1999: FITTING. CRACKED. INSPECTION FOUND A 1.5 INCH CRACK IN FLOORBEAM TO FRAME SUPPORT FITTING AT STA 1338, RBL 54.5. THE FITTING WAS REPLACED IAW SRM 51-10-4, 51-10-3, AND 51-30-5.
- [SDR CALA9901164](https://openairdocs.org/sdr/CALA9901164), Sep 8, 1999: SUPPORT. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN FLOORBEAM TO FRAME SUPPORT AT FS 446, LONGERON 23L. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-10-4, 
- [SDR CALA9901163](https://openairdocs.org/sdr/CALA9901163), Sep 8, 1999: SEAT TRACK. CORRODED. INSPECTION FOUND RT CENTER SEAT TRACK CORRODED AROUND CLIP NUTS AT STA 1009-1079. THE SEAT TRACK WAS REPLACED IAW ECRA 5310-03904.
- [SDR CALA9901162](https://openairdocs.org/sdr/CALA9901162), Sep 8, 1999: SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 218, LBL 6. A NEW SUPPORT WAS INSTALLED IAW SRM 53-14-1, FIGURE 11, 51-10-4, 51-10-3, AND 51-30-2.
- [SDR CALA9901161](https://openairdocs.org/sdr/CALA9901161), Sep 8, 1999: SKIN. CORRODED. INSPECTION FOUND FORWARD ENTRANCE DOOR CUTOUT CORRODED ON LOWER FORWARD CORNER AT FS 200, LONGERON 18L. A REPAIR DOUBLER AND FILLER WERE INSTALLED IAW ECRA 5310

All 96: https://openairdocs.org/deregistered/N93875-2013-08-16/reports.md

## 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.

- [Incident 20000402001949I](https://openairdocs.org/incident/20000402001949I), Apr 2, 2000: Doug DC982 (N93875), Tampa, FL, Minor damage. (-23) On April 2, 2000, at 2115 EST, a Mcdonnell Douglas, DC-9-82, N93875, operated by Continental airlines, flight 1671 from Tampa International Airport to…
- [Incident 19970523019429I](https://openairdocs.org/incident/19970523019429I), May 23, 1997: Doug DC982 (N93875), Cleveland, OH. Narrative: flight crew reported #2 engine surged twice. Aircraft diverted and landed at Cleveland without incident. Cala Cleveland maintenance replaced #2…
- [Incident 19920124005999I](https://openairdocs.org/incident/19920124005999I), Jan 24, 1992: Doug DC982 (N93875), Cleveland, OH, Minor damage. NR2 engine lost hydraulic pressure on climb. Returned. Found hydraulic pump had failed.

## Other aircraft with N93875

- [Cancelled 1970-09-08](https://openairdocs.org/deregistered/N93875-1970-09-08): Ercoupe 415-C, S/N 1198, built 1946. Owner: [Dynair Club Inc](https://openairdocs.org/faa-owner/DYNAIR%20CLUB%20INC), [Pomona, CA](https://openairdocs.org/faa-place/CA/Pomona)

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