# N35832: 1987 Mcdonnell Douglas DC-9-82(MD-82), registration cancelled 2006-04-17

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: April 17, 2006
- Status when cancelled: Valid registration
- Airframe: [Mcdonnell Douglas DC-9-82(MD-82)](https://openairdocs.org/model/mcdonnell-douglas-dc-9-82-md-82) (registry code 3022082)
- Engine: [Amateur-built UNKNOWN ENG](https://openairdocs.org/engine/amateur-built-unknown-eng) (registry code 99999)
- Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (OpenAirDocs)
- Serial number: 49492
- Year built: 1987
- Type of aircraft: Fixed wing multi engine
- Airworthiness: Standard, transport
- Airworthiness date: April 28, 1987
- Certificate issued: December 28, 1999
- Last registry action: March 8, 2005
- Mode S code: A40561
- Owner when cancelled: [Wachovia Bank Na Trustee](https://openairdocs.org/faa-owner/WACHOVIA%20BANK%20NA%20TRUSTEE)
- 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/N35832
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=35832
- Page: https://openairdocs.org/deregistered/N35832-2006-04-17

From the FAA registry file of October 31, 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 (119, newest 50)

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

- [SDR CALA0400143](https://openairdocs.org/sdr/CALA0400143), Feb 20, 2004: LONGERON. CORRODED. INSPECTION FOUND LONGERON 30 CORRODED FORWARD OF SPLICE IN FORWARD BAGGAGE BIN BETWEEN STA 484 AND 503. THE CORRODED SECTION OF LONGERON WAS REMOVED AND A SPLIC
- [SDR CALA0400130](https://openairdocs.org/sdr/CALA0400130), Feb 17, 2004: CABLE. OUT OF RIG. THE TAIL CONE WOULD NOT DEPLOY USING AFT ENTRY DOOR HANDLE. THE TAIL CONE CABLES WERE RIGGED IAW MM 53-53-00.
- [SDR CALA0300006](https://openairdocs.org/sdr/CALA0300006), Jan 9, 2003: LONGERON. CRACKED. INSPECTION FOUND A 1" CRACK IN LONGERON 2L AT AFT SIDE OF BELTFRAME, STA 1415. A LONGERON SPLICE WAS INSTALLED IAW SRM 53-02.
- [SDR CALA0100990](https://openairdocs.org/sdr/CALA0100990), Oct 30, 2001: INTERCOSTAL. CORRODED. INSPECTION FOUND INTERCOSTAL CORRODED AT LOWER SECTION OF AFT BAGGAGE BIN DOOR CUTOUT, STA 1174. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 53-01, FIGURE 
- [SDR CALA0100985](https://openairdocs.org/sdr/CALA0100985), Oct 29, 2001: SKIN. CRACKED. INSPECTION FOUND A 1.5" CRACK IN R/H WING UPPER L/E SKIN BETWEEN #2 & #3 SLAT PANELS AT WS XOS 286. A SKIN DOUBLER REPAIR WAS INSTALLED IAW ECRA 5720-01731.
- [SDR CALA0001406](https://openairdocs.org/sdr/CALA0001406), Sep 8, 2000: CHANNEL. CORRODED. INSPECTION FOUND DOME NUT GANG CHANNEL AND OUTER SHIM OF LT WING LOWER FUEL TANK OPENING (PANEL 1371C) CORRODED. THE RUB STRIP AND GANG CHANNEL WERE REMOVED AND
- [SDR CALA0001405](https://openairdocs.org/sdr/CALA0001405), Sep 8, 2000: ACCESS PANEL. CRACKED. INSPECTION FOUND A .5 INCH CRACK AT LAST RIVET HOLE IN THE FIXED SECTION ON O/B SIDE OF RT HORIZONTAL STABILIZER ELEVATOR ACCESS TO ELEVATOR GEAR TAB MECHANISM 
- [SDR CALA0001404](https://openairdocs.org/sdr/CALA0001404), Sep 8, 2000: SKIN. DENTED. INSPECTION FOUND THE LT NR 5 SLAT LEADING EDGE DENTED. THE SLAT WAS REMOVED, REPAIRED, AND REINSTALLED IAW MM 27-80-01, SRM 57-06, FIGURE 1, AND 51-30-2.
- [SDR CALA0001393](https://openairdocs.org/sdr/CALA0001393), Sep 4, 2000: FLOOR PANEL. CORRODED. INSPECTION FOUND R-1 ENTRYWAY FLOOR PANEL CORRODED AT FS 148 - 200. THE CORRODED FLOOR PANEL AREA WAS REPAIRED IAW SRM 53-24-0, FIGURE 3, 51-10-3, AND ECRA 5100
- [SDR CALA0001391](https://openairdocs.org/sdr/CALA0001391), Sep 3, 2000: ACCESS PANEL. CORRODED. INSPECTION FOUND LT WING FUEL ACCESS PANELS 1303C, 1355C, AND 1363C CORRODED AND GOUGED. THE FUEL PANELS WERE REMOVED AND REPLACED IAW ECRA 5730-01688.
- [SDR CALA0001390](https://openairdocs.org/sdr/CALA0001390), Sep 3, 2000: ACCESS PANEL. CORRODED. INSPECTION FOUND RT WING FUEL ACCESS PANELS 1410C, 1409C, AND 1436C CORRODED AND GOUGED. THE FUEL PANELS WERE REMOVED AND REPLACED IAW ECRA 5730-01688.
- [SDR CALA0001368](https://openairdocs.org/sdr/CALA0001368), Sep 2, 2000: SLAT TRACK. GOUGED. INSPECTION FOUND RT WING NR 5 SLAT TRACK GOUGED. THE SLAT TRACK WAS REMOVED AND REPLACED IAW MM 27-80-01.
- [SDR CALA0001362](https://openairdocs.org/sdr/CALA0001362), Sep 1, 2000: PANEL. GOUGED. INSPECTION FOUND LT WING LOWER SURFACE FUEL ACCESS PANEL NR 2 GOUGED. THE PANEL WAS REPAIRED IAW SRM 5730-01688 AND SRM 51-30-2.
- [SDR CALA0001358](https://openairdocs.org/sdr/CALA0001358), Sep 1, 2000: FITTING. CORRODED. INSPECTION FOUND LEFT O/B FLIGHT SPOILER CENTER FITTING CORRODED. THE SPOILER WAS REMOVED IAW MM 27-62-01. THE HINGE FITTING WAS REMOVED AND REPLACED IAW OHM 27
- [SDR CALA0001357](https://openairdocs.org/sdr/CALA0001357), Sep 1, 2000: ACCESS PANEL. GOUGED. INSPECTION FOUND FUEL ACCESS PANELS NR 1, 6 AND 7 GOUGED AND CORRODED ON RT WING LOWER SURFACE. THE PANELS WERE REPAIRED IAW ECRA 5730-01688 AND SRM 51-30-2.
- [SDR CALA0001356](https://openairdocs.org/sdr/CALA0001356), Sep 1, 2000: FITTING. CRACKED. INSPECTION FOUND TWO 1 INCH CRACKS AT FASTENER HOLE OF RT WING NR 5 SLAT END FITTING. THE SEAL AND RETAINER ON END FITTING WERE REMOVED IAW SRM 51-30-3. THE CRA
- [SDR CALA0001355](https://openairdocs.org/sdr/CALA0001355), Sep 1, 2000: FLOOR PANEL. CORRODED. INSPECTION FOUND AFT CARGO FLOOR PANEL CORRODED AND DENTED AT STA 1211 - 1231. THE FLOOR PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLED IAW SRM 53-24-0, FIGURE
- [SDR CALA0001350](https://openairdocs.org/sdr/CALA0001350), Aug 30, 2000: FLOOR PANEL. CORRODED. INSPECTION FOUND AFT CARGO FLOOR PANEL CORRODED AT FS 1211 - 1231. THE FLOOR PANEL WAS REPLACED IAW SRM 53-24-0, FIGURE 11A, 51-10-2, AND 51-60-0, PAGE 5.
- [SDR CALA0001349](https://openairdocs.org/sdr/CALA0001349), Aug 30, 2000: FITTING. CORRODED. INSPECTION FOUND NR 4 GALLEY ATTACH MOUNT FITTINGS (2) CORRODED. THE FITTINGS WERE REMOVED AND REPLACED IAW ECRA 2530-01257.
- [SDR CALA0001342](https://openairdocs.org/sdr/CALA0001342), Aug 28, 2000: FLOOR SUPPORT. CRACKED. INSPECTION FOUND A 6 INCH CRACK IN MID CARGO BAY FIBERGLASS FLOOR SUPPORT ANGLE AT STA 617, LONGERON 26R TO 27R. THE FLOOR SUPPORT ANGLE WAS REMOVED, REPAIRED W
- [SDR CALA0001341](https://openairdocs.org/sdr/CALA0001341), Aug 28, 2000: WEB. CRACKED. INSPECTION FOUND A 4.5 INCH CRACK IN AFT AIRSTAIR LT SIDE WEB. THE CRACKED AREA WAS CUT OUT IAW SRM 52-01, FIGURE 2. A DOUBLER AND FILLER REPAIR WAS INSTALLED I
- [SDR CALA0001334](https://openairdocs.org/sdr/CALA0001334), Aug 27, 2000: FAIRING. GOUGED. INSPECTION FOUND RT WING NR 3 AFT LOWER FLAP HINGE FAIRING GOUGED. A SPLICE REPAIR WAS INSTALLED IAW SRM 51-30-2 AND 57-50-14, FIGURE 4.
- [SDR CALA0001333](https://openairdocs.org/sdr/CALA0001333), Aug 27, 2000: FAIRING. CRACKED. INSPECTION FOUND A 4 INCH CRACK IN RT WING O/B FLAP HINGE FAIRING LOWER HALF. A DOUBLER REPAIR WAS INSTALLED IAW SRM 57-50-14 AND 51-30-2.
- [SDR CALA0001327](https://openairdocs.org/sdr/CALA0001327), Aug 25, 2000: CARGO TRACK. CORRODED. INSPECTION FOUND AFT CARGO TRACK CORRODED AT NUT CLIP HOLES. THE CARGO TRACK WAS REMOVED AND A NEW CARGO TRACK WAS INSTALLED IAW SRM 51-30-1 AND 53-24-0, FIGURE
- [SDR CALA0001326](https://openairdocs.org/sdr/CALA0001326), Aug 25, 2000: FRAME. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN FORWARD END OF FRAME OF THE FORWARD LAV TOILET SERVICING UNIT AT STA 240, LT SIDE. A DOUBLER WAS INSTALLED IAW SRM 53-01, FIG
- [SDR CALA0001325](https://openairdocs.org/sdr/CALA0001325), Aug 25, 2000: FLAP TRACK. CORRODED. INSPECTION FOUND RIGHT I/B FLAP TRACK UPPER ROLLER SURFACE CORRODED. THE RIGHT I/B FLAP TRACK WAS REMOVED AND REPLACED IAW MM 27-51-01.
- [SDR CALA0001324](https://openairdocs.org/sdr/CALA0001324), Aug 25, 2000: VANE. GOUGED. INSPECTION FOUND RIGHT I/B FLAP MOVEABLE VANE GOUGED. THE GOUGED AREA OF SKIN WAS REMOVED AND REPAIR PARTS WERE INSTALLED IAW SRM 51-70-2, FIGURE 72 AND PARAGRA
- [SDR CALA0001323](https://openairdocs.org/sdr/CALA0001323), Aug 25, 2000: ANGLE. CRACKED. INSPECTION FOUND FOUR INCH CRACKS IN TWO ANGLES ON I/B FAIRING OF NR 2 ENGINE UPPER T/R BUCKET. THE ANGLES WERE REMOVED AND NEW ANGLES WERE INSTALLED IAW SRM 51
- [SDR CALA0001322](https://openairdocs.org/sdr/CALA0001322), Aug 25, 2000: FLAP TRACK. CORRODED. INSPECTION FOUND LEFT I/B FLAP TRACK UPPER ROLLER SURFACE CORRODED. THE LEFT I/B FLAP TRACK WAS REMOVED AND REPLACED IAW MM 27-51-01.
- [SDR CALA0001319](https://openairdocs.org/sdr/CALA0001319), Aug 25, 2000: PANEL. CORRODED. INSPECTION FOUND RT WING FUEL PANEL 1414C CORRODED. THE PANEL WAS REMOVED AND REPLACED IAW SRM 51-30-2.
- [SDR CALA0001318](https://openairdocs.org/sdr/CALA0001318), Aug 25, 2000: GALLEY TRACK. CORRODED. INSPECTION FOUND FORWARD GALLEY I/B LOWER MOUNT FITTING CORRODED. A REPLACEMENT MOUNT FITTING WAS INSTALLED IAW ECRA 2530-01257.
- [SDR CALA0001317](https://openairdocs.org/sdr/CALA0001317), Aug 25, 2000: ANGLE. CRACKED. INSPECTION FOUND CRACKS IN FIRST AND THIRD ANGLES ON INBOARD T/R FAIRING ON UPPER BUCKET OF NR 1 ENGINE. THE CRACKS WERE APPROXIMATELY 3 INCHES LONG. THE ANGLES
- [SDR CALA0001316](https://openairdocs.org/sdr/CALA0001316), Aug 25, 2000: FITTING. CORRODED. INSPECTION FOUND FORWARD ENTRY FLOOR SUPPORT FITTING CORRODED AT STA 160 - 196, LBL 55. THE FLOOR SUPPORT FITTING WAS REMOVED AND A NEW SUPPORT FITTING WAS INST
- [SDR CALA0001315](https://openairdocs.org/sdr/CALA0001315), Aug 25, 2000: ATTACH ANGLE. CRACKED. INSPECTION FOUND A 3 INCH CRACK IN MID CARGO LT SIDEWALL FORWARD ATTACH ANGLE AT STA 524. THE ATTACH ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-
- [SDR CALA0001314](https://openairdocs.org/sdr/CALA0001314), Aug 25, 2000: SKIN. DENTED. INSPECTION FOUND THREE DENTS IN NR 1 SLAT T/E BETWEEN XOS 166 AND XOS 147. THE DENTED AREA WAS REMOVED AND A REPAIR WAS INSTALLED IAW ECRA 5750-03426.
- [SDR CALA0001312](https://openairdocs.org/sdr/CALA0001312), Aug 25, 2000: WEB. CRACKED. INSPECTION FOUND A 6 INCH CRACK IN SUBFLOOR WEB AT STA 1170, LBL 56. THE CRACKED AREA OF WEB WAS REMOVED AND FILLER AND DOUBLER WERE INSTALLED IAW SRM 53-01, FI
- [SDR CALA0001311](https://openairdocs.org/sdr/CALA0001311), Aug 25, 2000: PANEL. CORRODED. INSPECTION FOUND LT WING FUEL PANELS 1311C AND 1307C CORRODED. THE FUEL PANELS WERE REMOVED AND REPLACED IAW ECRA 5730-01688.
- [SDR CALA0001310](https://openairdocs.org/sdr/CALA0001310), Aug 25, 2000: PANEL. GOUGED. INSPECTION FOUND RT WING FUEL PANEL 1472C GOUGED. THE FUEL PANEL WAS REMOVED AND REPLACED IAW ECRA 5730-01688.
- [SDR CALA0001291](https://openairdocs.org/sdr/CALA0001291), Aug 21, 2000: SHIM. CORRODED. INSPECTION FOUND SHIMS UNDER STRAPS OF DOOR STOP NUMBER 11 & 12 OF AFT CARGO DOOR CORRODED. THE SHIMS WERE REMOVED AND REPLACEMENT SHIMS WERE INSTALLED. THE STR
- [SDR CALA0001290](https://openairdocs.org/sdr/CALA0001290), Aug 21, 2000: CARGO TRACK. CORRODED. INSPECTION FOUND THE UPPER FLANGE OF THE RIGHT CARGO TIE DOWN TRACK IN THE MID CARGO PIT CORRODED AROUND FASTENER HOLES ON UPPER AND LOWER SURFACES AT STA 579 -
- [SDR CALA0001289](https://openairdocs.org/sdr/CALA0001289), Aug 21, 2000: VANE. DENTED. INSPECTION FOUND LT WING O/B FLAP O/B NR 2 FIXED VANE DENTED ON LEADING EDGE. THE DENTED AREA WAS REMOVED AND REPAIR DOUBLERS WERE INSTALLED IAW SRM 57-50-14 AN
- [SDR CALA0001288](https://openairdocs.org/sdr/CALA0001288), Aug 21, 2000: FLOOR PANEL. CORRODED. INSPECTION FOUND FORWARD ENTRY FLOOR CORRODED AT STA 170 - 184, LBL 55. THE CORRODED AREA WAS CUT OUT IAW SRM 53-01. DOUBLER AND FILLER WERE INSTALLED IAW SRM 5
- [SDR CALA0001287](https://openairdocs.org/sdr/CALA0001287), Aug 21, 2000: SKIN. BULGED. INSPECTION FOUND LOWER FUSELAGE SKIN BULGED AT STA 389, LONGERON 16L-17L. THE EXISTING REPAIR WAS REMOVED IAW SRM 51-30-2. AN EXTERNAL AND INTERNAL DOUBLER AND 
- [SDR CALA0001281](https://openairdocs.org/sdr/CALA0001281), Aug 20, 2000: PANEL. GOUGED. INSPECTION FOUND RT WING LOWER PANEL NR 1222C GOUGED. THE PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLED IAW SRM 57-30-3, FIGURE 3 AND 51-10-3.
- [SDR CALA0001280](https://openairdocs.org/sdr/CALA0001280), Aug 20, 2000: FITTING. BENT. INSPECTION FOUND MID CARGO DOOR FRAME LOWER BEAM TEE FITTING BENT. THE TEE FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 51-10-1, 51-30-5, AND 51-
- [SDR CALA0001279](https://openairdocs.org/sdr/CALA0001279), Aug 20, 2000: PANEL. GOUGED. INSPECTION FOUND RT WING LOWER FUEL PANEL NR 1244C GOUGED. A DOUBLER WAS INSTALLED IAW SRM 57-01, FIGURE 3, SHEET 2, 51-10-3, 51-30-2, AND DRAWING 9937483.
- [SDR CALA0001278](https://openairdocs.org/sdr/CALA0001278), Aug 19, 2000: DOOR FRAME. CORRODED. INSPECTION FOUND AFT CARGO DOOR JAMB CENTER LOWER SECTION CORRODED. THE DOOR JAMB CENTER LOWER SECTION WAS REMOVED AND A NEW PART WAS INSTALLED IAW SRM 51-30-5,
- [SDR CALA0001277](https://openairdocs.org/sdr/CALA0001277), Aug 19, 2000: FLOOR SUPPORT. CORRODED. INSPECTION FOUND AFT CARGO DOOR JAMB FLOOR SUPPORT CORRODED AT STA 1155 - 1211, RBL 24. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW 
- [SDR CALA0001276](https://openairdocs.org/sdr/CALA0001276), Aug 19, 2000: WEB. CORRODED. INSPECTION FOUND FORWARD CARGO PIT FORWARD DOOR FRAME TORQUE BOX WEB CORRODED. A DOUBLER AND CONICAL WASHERS WERE INSTALLED IAW SRM 53-01, FIGURE 2, 51-30-1, 51
- [SDR CALA0001275](https://openairdocs.org/sdr/CALA0001275), Aug 19, 2000: FLOOR SUPPORT. CRACKED. INSPECTION FOUND SUPPORT SPLICE UNDER CABIN FLOOR HAD 7 CRACKS AT STA 826 - 886. THE CRACKS WERE 4 - 6 INCHES LONG. THE FLOOR SUPPORT WAS REMOVED AND REPLACED I

All 119: https://openairdocs.org/deregistered/N35832-2006-04-17/reports.md

## FAA accident and incident reports (1)

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 19970308008749I](https://openairdocs.org/incident/19970308008749I), Mar 8, 1997: Doug DC982 (N35832), Albuquerque, NM. Narrative: summary of findings; received an air carrier incident report from the abq ARTCC on March 9, 1997. The report identified Continental airlines flight…

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