# N17812: 1985 Mcdonnell Douglas DC-9-82(MD-82), registration cancelled 2004-04-01

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: April 1, 2004
- Exported to: Indonesia
- Status when cancelled: Second triennial mailing, no response
- 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: 49250
- Year built: 1985
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: March 11, 1985
- Certificate issued: December 29, 1994
- Last registry action: January 13, 2004
- Mode S code: A1397B
- Owner when cancelled: [Kuta-Two Aircraft Corporation](https://openairdocs.org/faa-owner/KUTA-TWO%20AIRCRAFT%20CORPORATION)
- Location: [Long Beach, CA](https://openairdocs.org/faa-place/CA/Long%20Beach)
- Owner type: Corporation
- Owner's area on the map: 33.8239° N, 118.1113° W: Placed by OpenAirDocs at the center of ZIP code 90808, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N17812
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=17812
- Page: https://openairdocs.org/deregistered/N17812-2004-04-01

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 (89, newest 50)

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

- [SDR CALA0300159](https://openairdocs.org/sdr/CALA0300159), Mar 11, 2003: SKIN. DENTED. MAINTENANCE FOUND A CREASE IN THE AFT UPPER CORNER OF THE OUTER SKIN OF THE AFT CARGO DOOR. THE CREASED AREA OF DOOR SKIN WAS REPAIRED IAW ECRA 5232-01023. A DI
- [SDR CALA0300108](https://openairdocs.org/sdr/CALA0300108), Mar 8, 2003: FRAME. CORRODED. INSPECTION FOUND BELTFRAME LOWER CHANNEL AND WEB CORRODED AT STA 1309 FROM LONGERON 28L TO 28R. REPAIRED IAW SRM 53-03, PAGE 04A, FIGURE 2A.
- [SDR CALA0300107](https://openairdocs.org/sdr/CALA0300107), Mar 8, 2003: CABLE. OUT OF RIG. THE TAILCONE FAILED TO DROP WITHIN SPECIFICATIONS AT ALL THREE POSITIONS DURING FUNCTIONAL TEST. THE PULL EXCEEDED 35 POUNDS. THE TAILCONE CABLES WERE ADJUSTED 
- [SDR CALA0300106](https://openairdocs.org/sdr/CALA0300106), Mar 8, 2003: LIGHT. INOPERATIVE. THE TAILCONE SLIDE LIGHT FAILED BATTERY TEST. THE SLIDE ASSEMBLY WAS REMOVED AND REPLACED IAW MM 25-62-01.
- [SDR CALA0300101](https://openairdocs.org/sdr/CALA0300101), Mar 7, 2003: FRAME. CRACKED. INSPECTION FOUND A 1" CRACK IN FRAME RADIUS AT STA 1418, LONGERON 2L AND 2R. REPAIRS WERE INSTALLED AT EACH LOCATION IAW ECRA 5310-04332.
- [SDR CALA0300100](https://openairdocs.org/sdr/CALA0300100), Mar 6, 2003: WEB. CORRODED. INSPECTION FOUND WEB AT STA 1338 AFT PRESSURE BULKHEAD T-CAP CORRODED. THE CORRODED SECTION OF WEB WAS CUT OUT AND A NEW SECTION WAS INSTALLED IAW SRM 51-70-4, 
- [SDR CALA0300093](https://openairdocs.org/sdr/CALA0300093), Mar 3, 2003: FRAME. CRACKED. INSPECTION FOUND A 3/4" CRACK IN FRAME AT STA 1418, LONGERON 1. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-03, FIGURE 4.
- [SDR CALA0300089](https://openairdocs.org/sdr/CALA0300089), Mar 3, 2003: CASTING. CRACKED. INSPECTION FOUND A 1/2" CRACK IN AFT ENTRY DOOR LEFT LOWER CASTING. THE CASTING WAS REMOVED AND A NEW CASTING WAS INSTALLED IAW SRM 51-30-0.
- [SDR CALA0100630](https://openairdocs.org/sdr/CALA0100630), Jul 2, 2001: BATTERY. DISCHARGED. THE EMERGENCY CEILING LIGHTS WERE FOUND INOPERATIVE AT ROW 15. THE BATTERIES WERE REMOVED AND REPLACED AND OPERATION CHECKED GOOD.
- [SDR CALA0000744](https://openairdocs.org/sdr/CALA0000744), May 25, 2000: SKIN. CRACKED. INSPECTION FOUND CABIN LT SUBFLOOR SKIN CRACKED AT FS 218. THE SUBFLOOR PANEL WAS REMOVED IAW SRM 51-30-2 AND 51-30-5. A NEW SUBFLOOR WAS INSTALLED IAW SRM 53-1
- [SDR CALA0000743](https://openairdocs.org/sdr/CALA0000743), May 25, 2000: CARGO TRACK. CORRODED. INSPECTION FOUND AFT CARGO LT TIE DOWN TRACK CORRODED FROM STA 1003 - 1212. THE TIE DOWN TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-1 AND 51-30-2.
- [SDR CALA0000304](https://openairdocs.org/sdr/CALA0000304), Mar 13, 2000: CLIP. CRACKED. INSPECTION FOUND A 2.3 INCH CRACK IN AFT CARGO FORWARD BULKHEAD FRAME CLIP AT STA 1003, LONGERON 28R. THE CLIP WAS REMOVED AND A NEW CLIP WAS INSTALLED IAW SRM 
- [SDR CALA0000303](https://openairdocs.org/sdr/CALA0000303), Mar 13, 2000: SKIN. CRACKED. INSPECTION FOUND A 4 INCH CRACK IN PREVIOUS DOUBLER REPAIR OF UPPER FORWARD CORNER RT MLG DOOR. THE DOUBLER WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-30-5
- [SDR CALA0000301](https://openairdocs.org/sdr/CALA0000301), Mar 11, 2000: FLOORBEAM. GOUGED. INSPECTION FOUND AFT CARGO CEILING FLOORBEAM GOUGED AT FS 1174, RBL 2. A DOUBLER AND SHIM WERE INSTALLED IAW SRM 53-05, FIGURE 86, 51-10-2, 51-10-3, AND 53-04, 
- [SDR CALA0000300](https://openairdocs.org/sdr/CALA0000300), Mar 11, 2000: CARGO TRACK. CORRODED. INSPECTION FOUND MID PIT RT CARGO TIE DOWN TRACK CORRODED FROM STA 427-636. THE TRACK WAS REMOVED AND NEW TRACK WAS INSTALLED IAW SRM 51-30-1 AND 51-30-2.
- [SDR CALA0000299](https://openairdocs.org/sdr/CALA0000299), Mar 11, 2000: SKIN. DENTED. INSPECTION FOUND RUDDER SKIN DENTED AT UPPER LEFT SIDE. THE DENTED AREA WAS REMOVED. A FILLER AND DOUBLER REPAIR WAS INSTALLED IAW SRM 55-03 AND 51-10-3.
- [SDR CALA0000298](https://openairdocs.org/sdr/CALA0000298), Mar 11, 2000: SKIN. DENTED. INSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AT FS 133 BETWEEN LONGERONS 18L AND 19L. THE DENT WAS COLD WORKED IAW SRM 53-04, FIGURE 38. A DOUBLER WAS INSTALL
- [SDR CALA0000297](https://openairdocs.org/sdr/CALA0000297), Mar 11, 2000: SKIN. DENTED. INSPECTION FOUND RIGHT EXTERNAL FUSELAGE SKIN DENTED AT STA 560 BETWEEN LONGERON 21R AND 22R. THE DOUBLER WAS REMOVED AND THE AREA WAS COLD WORKED IAW ECRA 5330
- [SDR CALA0000296](https://openairdocs.org/sdr/CALA0000296), Mar 11, 2000: STOP. GOUGED. INSPECTION FOUND FORWARD CARGO DOOR STOP GOUGED. A DOUBLER WAS INSTALLED IAW SRM 52-03, FIGURE 8, 51-10-2, 51-10-3, AND 51-30-2.
- [SDR CALA0000295](https://openairdocs.org/sdr/CALA0000295), Mar 11, 2000: SKIN. GOUGED. INSPECTION FOUND LEFT AILERON LOWER SURFACE SKIN GOUGED. THE AILERON WAS REPAIRED IAW ECRA 5750-03367.
- [SDR CALA0000294](https://openairdocs.org/sdr/CALA0000294), Mar 11, 2000: PAN. CRACKED. INSPECTION FOUND SEVERAL .125 INCH CRACKS AROUND DOOR SEAL RIVET HOLE AT AFT CARGO DOOR UPPER AFT CORNER. THE FASTENERS WERE REMOVED IAW SRM 52-03, FIGURE 8. DO
- [SDR CALA0000291](https://openairdocs.org/sdr/CALA0000291), Mar 10, 2000: BRACKET. CRACKED. INSPECTION FOUND NR 2 T/R UPPER DOOR I/B SIDE WING FAIRING SUPPORT BRACKET AND ANGLE CLIP CRACKED. THE CRACKS WERE 1 AND 1/8 LONG. THE I/B SIDE SUPPORT BRACKET 
- [SDR CALA0000290](https://openairdocs.org/sdr/CALA0000290), Mar 10, 2000: STOP. GOUGED. INSPECTION FOUND MID CARGO DOOR STOPS GOUGED IN TWO PLACES. DOUBLERS WERE INSTALLED IAW SRM 51-10-3, 51-30-2, AND 51-30-5, AND ECRA 5330-02819.
- [SDR CALA0000289](https://openairdocs.org/sdr/CALA0000289), Mar 10, 2000: CARGO TRACK. CORRODED. INSPECTION FOUND AFT CARGO TIE DOWN TRACK CORRODED FROM STA 1003 TO 1212. THE TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-1 AND 51-30-2.
- [SDR CALA0000288](https://openairdocs.org/sdr/CALA0000288), Mar 10, 2000: STOP. GOUGED. INSPECTION FOUND AFT CARGO DOOR STOPS GOUGED IN THREE PLACES. REPAIRS WERE INSTALLED IAW SRM 52-03, FIGURE 8, 51-10-3, AND ECRA 5330-02819.
- [SDR CALA0000287](https://openairdocs.org/sdr/CALA0000287), Mar 9, 2000: SKIN. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN FUSELAGE SKIN NEXT TO TOP RT RADOME HINGE. A DOUBLER AND FILLER WERE INSTALLED IAW SRM 51-10-3 AND 53-05, FIGURE 7.
- [SDR CALA0000286](https://openairdocs.org/sdr/CALA0000286), Mar 9, 2000: STOP. WORN. INSPECTION FOUND MID CARGO DOOR STOP WORN. A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-03, FIGURE 8, 51-10-3, AND 51-30-2.
- [SDR CALA0000285](https://openairdocs.org/sdr/CALA0000285), Mar 9, 2000: SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 200, LBL 12 TO LBL 15. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-4.
- [SDR CALA0000284](https://openairdocs.org/sdr/CALA0000284), Mar 9, 2000: SKIN. DENTED. INSPECTION FOUND EXTERNAL FUSELAGE SKIN SCRATCHED AND DENTED AT FS 280 BETWEEN LONGERONS 22L AND 23L. THE AREA WAS COLD WORKED AND DOUBLERS WERE INSTALLED IAW S
- [SDR CALA0000283](https://openairdocs.org/sdr/CALA0000283), Mar 9, 2000: CARGO TRACK. CORRODED. INSPECTION FOUND AFT CARGO AFT RT TIE DOWN TRACK CORRODED AROUND FASTENER HOLES. THE TIE DOWN TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-2.
- [SDR CALA0000282](https://openairdocs.org/sdr/CALA0000282), Mar 8, 2000: INTERCOSTAL. CORRODED. INSPECTION FOUND INTERCOSTAL CORRODED AT FS 1309-1331, LONGERON 29R. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-30-5.
- [SDR CALA0000281](https://openairdocs.org/sdr/CALA0000281), Mar 8, 2000: FLOOR PANEL. CORRODED. INSPECTION FOUND COCKPIT FLOOR SKIN CORRODED AT FS 160, LBL 6. THE CORROSION WAS REMOVED IAW SRM 53-01, FIGURE 2 AND 51-10-3. A REPAIR DOUBLER WAS INSTALLED IAW
- [SDR CALA0000280](https://openairdocs.org/sdr/CALA0000280), Mar 8, 2000: STOP. WORN. INSPECTION FOUND TWO MID CARGO DOOR STOPS WORN. REPAIRED STOPS IAW ECRA 5330-02819.
- [SDR CALA0000279](https://openairdocs.org/sdr/CALA0000279), Mar 8, 2000: STOP. WORN. INSPECTION FOUND TWO AFT CARGO DOOR STOPS WORN. THE AREAS WERE REPAIRED IAW SRM 52-03, FIGURE 8, 51-30-2, 52-30-7, 51-10-3, AND ECRA 5330-02819.
- [SDR CALA0000272](https://openairdocs.org/sdr/CALA0000272), Mar 6, 2000: STOP. GOUGED. INSPECTION FOUND MID CARGO DOOR STOP GOUGED.. THE DOOR STOP WAS REPAIRED IAW ECRA 5330-02819.
- [SDR CALA0000271](https://openairdocs.org/sdr/CALA0000271), Mar 6, 2000: ANGLE. CRACKED. INSPECTION FOUND FILLET PANEL SUPPORT ANGLE CRACKED AT STA 945, LONGERON 30. THE SUPPORT ANGLE WAS REMOVED AND A NEW SUPPORT ANGLE WAS INSTALLED IAW SRM 51-10-0
- [SDR CALA0000258](https://openairdocs.org/sdr/CALA0000258), Mar 3, 2000: STOP. GOUGED. INSPECTION FOUND FORWARD CARGO DOOR STOP GOUGED. THE DOOR STOP WAS REPAIRED IAW ECRA 5330-02819.
- [SDR CALA0000257](https://openairdocs.org/sdr/CALA0000257), Mar 3, 2000: FLANGE. CORRODED. INSPECTION FOUND ANTENNA FLANGE CORRODED IN MID PIT AT STA 600, LONGERON 29L TO 30. THE ANTENNA FLANGE WAS REMOVED AND A NEW FLANGE AND DOUBLER WERE INSTALLED I
- [SDR CALA0000256](https://openairdocs.org/sdr/CALA0000256), Mar 3, 2000: FLOORBEAM. CORRODED. INSPECTION FOUND L-1 DOOR THRESHOLD LOWER SUB FLOOR WEB CORRODED AND ATTACH ANGLE CRACKED. THE SUB FLOOR WEB WAS REMOVED IAW SRM 51-30-2. A NEW SUB FLOOR WEB WA
- [SDR CALA0000255](https://openairdocs.org/sdr/CALA0000255), Mar 3, 2000: WEB. CORRODED. INSPECTION FOUND LEFT CUSP WEB ON FORWARD SIDE OF FRAME AT STA 237, LONGERON 18L CORRODED. THE CORRODED AREA WAS CUT OUT IAW SRM 53-01, FIGURE 4. A DOUBLER, PLA
- [SDR CALA0000254](https://openairdocs.org/sdr/CALA0000254), Mar 3, 2000: WEB. CRACKED. INSPECTION FOUND A 3 INCH CRACK IN MAIN ENRTY DOOR AFT TORQUE BOX UPPER WEB TENSION LEG AT FS 208, LONGERON 11L. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-30-
- [SDR CALA0000253](https://openairdocs.org/sdr/CALA0000253), Mar 3, 2000: SEAT TRACK. CORRODED. INSPECTION FOUND LEFT O/B SEAT TRACK CORRODED AT FS 1174-1300. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-1.
- [SDR CALA0000252](https://openairdocs.org/sdr/CALA0000252), Mar 3, 2000: INTERCOSTAL. CRACKED. INSPECTION FOUND A 1.5 INCH CRACK IN FORWARD CARGO INTERCOSTAL AFT SUPPORT ANGLE AT STA 237 BETWEEN LONGERON 27R AND 28R. THE SUPPORT ANGLE WAS REMOVED AND REPL
- [SDR CALA0000251](https://openairdocs.org/sdr/CALA0000251), Mar 3, 2000: SKIN. DENTED. INSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED BETWEEN FS 465 AND 484 AT LONGERON 21R AND 22R. THE DENT WAS COLD WORKED IAW SRM 53-04, FIGURE 8, CONDITION 2. AN
- [SDR CALA0000250](https://openairdocs.org/sdr/CALA0000250), Mar 3, 2000: SEAT TRACK. CORRODED. INSPECTION FOUND LEFT I/B SET TRACK CORRODED AT FS 1030-1300. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-05, FIGURE 5F.
- [SDR CALA0000249](https://openairdocs.org/sdr/CALA0000249), Mar 3, 2000: FLOORBEAM. CRACKED. INSPECTION FOUND A 3 INCH CRACK IN R-1 DOOR THRESHOLD FLOOR SUPPORT WEB AT FORWARD EDGE OF DOOR CUTOUT. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED I
- [SDR CALA0000248](https://openairdocs.org/sdr/CALA0000248), Mar 3, 2000: ANGLE. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN LOWER RUDDER FAIRING AT STIFFENER ANGLE. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-4.
- [SDR CALA0000247](https://openairdocs.org/sdr/CALA0000247), Mar 3, 2000: ANGLE. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN LONGERON 30 FILLET PANEL SUPPORT ANGLE AT STA 970. THE SUPPORT ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-4.
- [SDR CALA0000246](https://openairdocs.org/sdr/CALA0000246), Mar 3, 2000: SEAT TRACK. CORRODED. INSPECTION FOUND LEFT CENTER SEAT TRACK CORRODED AT FS 1030-1100, LBL 22. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-1.
- [SDR CALA0000245](https://openairdocs.org/sdr/CALA0000245), Mar 3, 2000: STOP. WORN. INSPECTION FOUND FORWARD CARGO DOOR STOP WORN. REPAIRED IAW ECRA 5330-02819.

All 89: https://openairdocs.org/deregistered/N17812-2004-04-01/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 19940803035579I](https://openairdocs.org/incident/19940803035579I), Aug 3, 1994: Doug DC982 (N17812), Denver, CO, Minor damage. Noticed tailcone seal punctured prior departure. Maintenance signed repair off. Tailcone fell off. Landing at denve

## Other aircraft with N17812

- [Registered now](https://openairdocs.org/aircraft/N17812): Beech 200, S/N BB236

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