# N14871: 1983 Mcdonnell Douglas DC-9-82(MD-82), registration cancelled 2004-12-07

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: December 7, 2004
- Exported to: South Africa
- Status when cancelled: Triennial form not returned
- 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: 48022
- Year built: 1983
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: June 11, 1993
- Certificate issued: November 27, 1996
- Last registry action: December 17, 2002
- Mode S code: A0C3CF
- Owner when cancelled: [Aviation Assets 871 Inc](https://openairdocs.org/faa-owner/AVIATION%20ASSETS%20871%20INC)
- Location: [San Francisco, CA](https://openairdocs.org/faa-place/CA/San%20Francisco)
- Owner type: Corporation
- Owner's area on the map: 37.7984° N, 122.3992° W: Placed by OpenAirDocs at the center of ZIP code 94111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N14871
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=14871
- Page: https://openairdocs.org/deregistered/N14871-2004-12-07

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 (100, newest 50)

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

- [SDR CALA0400561](https://openairdocs.org/sdr/CALA0400561), Jul 2, 2004: PANEL. CRACKED. INSPECTION FOUND A 6 INCH CRACK IN RIGHT WING PANEL AT WING STA XFS 70-196. THE PANEL WAS REMOVED AND REPLACED IAW SRM 51-30-2.
- [SDR CALA0400572](https://openairdocs.org/sdr/CALA0400572), Jun 24, 2004: LONGERON. CRACKED. INSPECTION FOUND A SMALL CRACK IN LOWER EDGE OF THE VERTICAL LEG OF LONGERON 20L AT APPROXIMATELY STA 995. THE CRACK RAN FROM THE BOTTOM EDGE OF THE VERTICAL FL
- [SDR CALA0400542](https://openairdocs.org/sdr/CALA0400542), Jun 22, 2004: ANGLE. CORRODED. INSPECTION FOUND AFT CARGO DOOR FORWARD DOOR JAMB ANGLE CORRODED AT STA 1155, LONGERON 27R. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-5.
- [SDR CALA0400540](https://openairdocs.org/sdr/CALA0400540), Jun 18, 2004: STAND OFF. CORRODED. INSPECTION FOUND FLOOR STANDOFF CORRODED AT STA 200 CENTER OF FLOOR. THE FLOOR STANDOFF WAS REMOVED AND REPLACED IAW SRM 51-30-5-001.
- [SDR CALA0400539](https://openairdocs.org/sdr/CALA0400539), Jun 18, 2004: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT ANGLE CORRODED AT STA 200-230, LBL 15. THE FLOOR SUPPORT ANGLE WAS REPLACED IAW SRM 51-10-3.
- [SDR CALA0400538](https://openairdocs.org/sdr/CALA0400538), Jun 18, 2004: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT TRACK CORRODED AT STA 160-200, RBL 7. THE FLOOR SUPPORT TRACK WAS REPLACED IAW SRM 51-30-3.
- [SDR CALA0300111](https://openairdocs.org/sdr/CALA0300111), Mar 10, 2003: ANGLE. CORRODED. INSPECTION FOUND AFT PRESSURE BULKHEAD ANGLE CORRODED AT STA 1338, LONGERON 28R TO 30. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30.
- [SDR CALA0300109](https://openairdocs.org/sdr/CALA0300109), Mar 9, 2003: SKIN. GOUGED. INSPECTION FOUND LOWER FUSELAGE SKIN GOUGED AT JACK POINT, STA 1338. THE GOUGED AREA WAS REMOVED AND A DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 9.
- [SDR CALA0300114](https://openairdocs.org/sdr/CALA0300114), Mar 7, 2003: SKIN. DELAMINATED. MAINTENANCE FOUND THE L/H INBOARD FLAP OUTBOARD VANE UPPER SKIN DELAMINATED . THE FINAL TRIM OUT AREA MEASURED 4.7" X 5.6". THE SKIN WAS REPAIRED IAW ECRA 5750-
- [SDR CALA0300113](https://openairdocs.org/sdr/CALA0300113), Mar 7, 2003: SKIN. DELAMINATED. MAINTENANCE FOUND THE R/H INBOARD FLAP OUTBOARD VANE UPPER SKIN DELAMINATED. THE FINAL TRIM OUT AREA MEASURED 4.3" X 6.4". THE SKIN WAS REPAIRED IAW ECRA 5750-0
- [SDR CALA0300104](https://openairdocs.org/sdr/CALA0300104), Mar 7, 2003: SKIN. CRACKED. INSPECTION FOUND A 0.01" CRACK IN FUSELAGE SKIN AT STA 1338, LONGERON 10R. REPAIRED IAW ECRA 5330-03221 AND ECRA 5330-03220.
- [SDR CALA0300103](https://openairdocs.org/sdr/CALA0300103), Mar 7, 2003: SKIN. CRACKED. INSPECTION FOUND 0.01" CRACK IN FUSELAGE SKIN AT STA 1338 BELOW LONGERON 4R. REPAIRED IAW ECRA 5330-03221 AND ECRA 5330-03220.
- [SDR CALA0300096](https://openairdocs.org/sdr/CALA0300096), Mar 6, 2003: SKIN. CRACKED. INSPECTION FOUND A 1/4" CRACK IN MAIN CABIN DOOR EXTERIOR SKIN AT LOWER FORWARD CORNER. A REPAIR WAS INSTALLED IAW SRM 52-05.
- [SDR CALA0300092](https://openairdocs.org/sdr/CALA0300092), Mar 3, 2003: BELTFRAME. CRACKED. INSPECTION FOUND A 1/2" CRACK IN CANTED BELTFRAME AT STA 1416, LONGERON 4L TO 4R. INSTALLED NEW FRAME IAW SRM 51-00.
- [SDR CALA0300091](https://openairdocs.org/sdr/CALA0300091), Mar 3, 2003: CARGO TRACK. CORRODED. INSPECTION FOUND AFT BAGGAGE BIN RT TIE DOWN TRACK HOLES CORRODED AT STA 1136 - 1155. A NEW TIE DOWN TRACK WAS INSTALLED IAW SRM 53-23-00.
- [SDR CALA0300090](https://openairdocs.org/sdr/CALA0300090), Mar 3, 2003: BELTFRAME. CRACKED. INSPECTION FOUND A 1/2" CRACK IN CANTED BELTFRAME AT STA 1446, LONGERON 6R TO 5L. THE BELTFRAME WAS REMOVED AND REPLACED IAW SRM 51-10-2.
- [SDR CALA0300076](https://openairdocs.org/sdr/CALA0300076), Feb 28, 2003: CARGO TRACK. CORRODED. INSPECTION FOUND AFT BAGGAGE BIN LT TIE DOWN TRACK HOLES CORRODED BETWEEN STA 1231-1271. THE TIE DOWN TRACK WAS REPLACED IAW SRM 53-23-0.
- [SDR CALA0200023](https://openairdocs.org/sdr/CALA0200023), Jan 15, 2002: LINK. FAILED. WHEN THE GEAR WAS RAISED AFTER TAKEOFF, THE GEAR RETRACTED WITH ALL INDICATIONS NORMAL. THERE WAS A LOUD NOISE INDICATIVE OF THE NOSE GEAR DOOR HANGING DOWN AND
- [SDR CALA0101043](https://openairdocs.org/sdr/CALA0101043), Dec 29, 2001: SLIDE. FAILED. THE L-1 DOOR SLIDE FAILED EMERGENCY SLIDE LIGHT TEST. THE SLIDE WAS REMOVED AND REPLACED IAW WORK CARD 08-2560-1-4300.
- [SDR CALA0101042](https://openairdocs.org/sdr/CALA0101042), Dec 29, 2001: SLIDE. FAILED. THE R-1 DOOR SLIDE FAILED EMERGENCY SLIDE LIGHT TEST. THE SLIDE WAS REMOVED AND REPLACED IAW WORK CARD 08-2560-1-4300.
- [SDR CALA0100591](https://openairdocs.org/sdr/CALA0100591), Jun 24, 2001: BATTERY PACK. DISCHARGED. THE LT AND RT FORWARD OVERWING EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE DURING TEST. THE B5-103 BATTERY PACK WAS REMOVED AND REPLACED IAW MM 33-53-00.
- [SDR CALA0100039](https://openairdocs.org/sdr/CALA0100039), Jan 17, 2001: LIGHT. INOPERATIVE. INSPECTION FOUND FORWARD ENTRY PORTABLE EMERGENCY LIGHT INOPERATIVE. THE FORWARD ENTRY EMERGENCY LIGHT ASSEMBLY WAS REMOVED AND REPLACED IAW MM 33-53-00.
- [SDR CALA0001680](https://openairdocs.org/sdr/CALA0001680), Oct 30, 2000: FLOOR SUPPORT. CORRODED. INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT FS 200, RBL 41 - 55. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-2, 51-10-4, 51
- [SDR CALA0001678](https://openairdocs.org/sdr/CALA0001678), Oct 28, 2000: CARGO TRACK. CORRODED. INSPECTION FOUND FORWARD RT SIDE CARGO TRACK IN MID PIT CORRODED AT STA 541 - 636. THE TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-10-4, 51-30-1,
- [SDR CALA0001677](https://openairdocs.org/sdr/CALA0001677), Oct 28, 2000: STRAP. CORRODED. INSPECTION FOUND MID CARGO LOWER DOOR JAMB CORRODED AT FS 640 - 690. THE CORRODED STRAP WAS REMOVED AND A DOUBLER WAS INSTALLED IAW SRM 51-30-5, 51-30-7, AND 51
- [SDR CALA0001676](https://openairdocs.org/sdr/CALA0001676), Oct 28, 2000: WEB. CORRODED. INSPECTION FOUND RT CUSP WEB CORRODED UNDER FLOOR SUPPORT AT FS 1136 - 1155. A DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 2, SHEET 3.
- [SDR CALA0001675](https://openairdocs.org/sdr/CALA0001675), Oct 28, 2000: FLOOR SUPPORT. CORRODED. INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT FS 140 - 200, RBL 7. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-1, 51-10
- [SDR CALA0001674](https://openairdocs.org/sdr/CALA0001674), Oct 28, 2000: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORTS CORRODED AT FS 200, LBL 11 AND LBL 3 - RBL 3. THE FLOOR SUPPORTS WERE REMOVED AND NEW FLOOR SUPPORTS WERE INSTALLED IAW SRM 51-3
- [SDR CALA0001673](https://openairdocs.org/sdr/CALA0001673), Oct 28, 2000: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 160 - 200, LBL 43. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2, 51-10-3, A
- [SDR CALA0001672](https://openairdocs.org/sdr/CALA0001672), Oct 28, 2000: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORTS CORRODED AT FS 150 - 200, LBL 7 AND RBL 44. THE FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW SRM 51-10-4, 51-30-2, 51-30-5, AND 
- [SDR CALA0001671](https://openairdocs.org/sdr/CALA0001671), Oct 28, 2000: STRAP. CORRODED. INSPECTION FOUND AFT CARGO LOWER DOOR JAMB CORRODED AT FS 1155 - 1211. THE CORRODED STRAP WAS REMOVED AND REPLACED IAW SRM 51-10-3 AND ECRA 5310-03027.
- [SDR CALA0001670](https://openairdocs.org/sdr/CALA0001670), Oct 27, 2000: SKIN. DENTED. INSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AT FS 1251 - 1271 BETWEEN LONGERON 22R AND 23R. THE DENT WAS COLD WORKED IAW SRM 53-04, FIGURE 38. A DOUBLER WAS 
- [SDR CALA0001668](https://openairdocs.org/sdr/CALA0001668), Oct 27, 2000: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 200, RBL 24. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2 AND 51-10-3.
- [SDR CALA0001667](https://openairdocs.org/sdr/CALA0001667), Oct 27, 2000: SKIN. CRACKED. INSPECTION FOUND L-1 DOOR JAMB TORQUE BOX SKIN AFT LEG CRACKED AT FS 200. THE CRACKED AREA WAS CUT OUT AND A REPAIR DOUBLER AND FILLER WERE INSTALLED IAW EA 9-5
- [SDR CALA0001666](https://openairdocs.org/sdr/CALA0001666), Oct 27, 2000: SKIN. DENTED. INSPECTION FOUND RT EXTERNAL FUSELAGE SKIN DENTED AT FS 37 BETWEEN LONGERON 6R AND 18R. A REPAIR DOUBLER WAS INSTALLED IAW SRM 51-60, 53-01, FIGURE 7, 51-10-3, 
- [SDR CALA0001665](https://openairdocs.org/sdr/CALA0001665), Oct 27, 2000: FITTING. CRACKED. INSPECTION FOUND EXTERNAL FUSELAGE LOWER T-FITTING CRACKED AT FS 864, LONGERON 30. THE T-FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 51-30-5 AND
- [SDR CALA0001664](https://openairdocs.org/sdr/CALA0001664), Oct 27, 2000: FLOOR SUPPORT. PUNCTURED. INSPECTION FOUND FLOOR SUPPORT ANGLE PUNCTURED AT STA 541, L28R TO 28L. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2, 53-
- [SDR CALA0001663](https://openairdocs.org/sdr/CALA0001663), Oct 27, 2000: SKIN. DENTED. INSPECTION FOUND LT EXTERNAL FUSELAGE SKIN DENTED AND GOUGED AT FS 290 BETWEEN LONGERON 23L AND 24L. THE DENTED AREA WAS CUT OUT AND A DOUBLER WAS INSTALLED IAW
- [SDR CALA0001662](https://openairdocs.org/sdr/CALA0001662), Oct 27, 2000: WEB. CRACKED. INSPECTION FOUND THREE 2 INCH CRACKS IN LT SIDE VENT BOX AREA UPPER AFT CORNER WEB AT FORWARD SIDE OF FRAME STA 1485. THE CRACKS WERE STOP DRILLED IAW SRM 53-01
- [SDR CALA0001661](https://openairdocs.org/sdr/CALA0001661), Oct 26, 2000: PAN. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN RT MLG I/B DOOR FORWARD SIDE TOP CORNER. THE DOOR PAN WAS REMOVED AND A NEW PAN WAS INSTALLED IAW SRM 51-10-2, 51-10-4, 51-30
- [SDR CALA0001660](https://openairdocs.org/sdr/CALA0001660), Oct 26, 2000: FRAME. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN FORWARD FRAME SUPPORT ANGLE AT FS 229 - 256, LONGERON 1L. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-10-3
- [SDR CALA0001659](https://openairdocs.org/sdr/CALA0001659), Oct 26, 2000: WEB. CORRODED. INSPECTION FOUND CORROSION ON SUB FLOOR AND UNDER CUSP WEB AT FS 175, LBL 54. THE SUBFLOOR WAS REMOVED AND A NEW SUBFLOOR WAS INSTALLED IAW SRM 51-10-4, 53-14-1
- [SDR CALA0001648](https://openairdocs.org/sdr/CALA0001648), Oct 25, 2000: FRAME. CORRODED. INSPECTION FOUND CABIN WINDOW FRAME 41L CORRODED ON FORWARD AND AFT FLANGES AT STA 984 AND 1003. A REPAIR AND WINDOW DOUBLER WAS INSTALLED IAW EA 9-5330-2-A0794
- [SDR CALA0001647](https://openairdocs.org/sdr/CALA0001647), Oct 25, 2000: CARGO TRACK. CORRODED. INSPECTION FOUND MID CARGO LT TIE DOWN TRACK CORRODED AT FS 522 - 798. THE CORROSION WAS REMOVED IAW SRM 51-10-3. THE TRACK WAS TREATED AND PRIMED FROM FS 522 -
- [SDR CALA0001646](https://openairdocs.org/sdr/CALA0001646), Oct 25, 2000: FLOOR PANEL. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN LEFT O/B FLOOR PANEL EDGE AT FS 927 - 1003. THE CRACK WAS STOP DRILLED IAW SRM 51-10-4. A DOUBLER WAS INSTALLED IAW SRM 51-10
- [SDR CALA0001645](https://openairdocs.org/sdr/CALA0001645), Oct 24, 2000: WEB. CORRODED. INSPECTION FOUND SUBFLOOR WEB CORRODED AT FS 218, RBL 11 UPON REMOVAL OF GALLEY SUPPORT AND FITTING. A REPAIR WAS INSTALLED IAW SRM 53-01, FIGURE 4, 51-30-2, AN
- [SDR CALA0001644](https://openairdocs.org/sdr/CALA0001644), Oct 24, 2000: DOOR FRAME. DENTED. INSPECTION FOUND R-1 DOOR JAMB AT AFT CENTER AREA MAIN FRAME BEHIND ROLLER ASSEMBLY DENTED IN RADIUS. THE DOOR STOP WAS REMOVED IAW SRM 51-30-1. A REPAIR WAS IN
- [SDR CALA0001638](https://openairdocs.org/sdr/CALA0001638), Oct 23, 2000: SKIN. CORRODED. INSPECTION FOUND EXTERNAL FUSELAGE SKIN UNDER FWD WING TO BODY FAIRING CORRODED AT STA 769 BETWEEN STRINGERS 28R AND 27R. A DOUBLER WAS INSTALLED IAW SRM 53-04,
- [SDR CALA0001637](https://openairdocs.org/sdr/CALA0001637), Oct 23, 2000: SKIN. DENTED. INSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AT FS 170 BETWEEN LONGERONS 20R - 21R. THE DENTED AREA WAS REPAIRED WITH A DOUBLER IAW SRM 53-04, FIGURE 38G.
- [SDR CALA0001636](https://openairdocs.org/sdr/CALA0001636), Oct 23, 2000: FLOOR SUPPORT. CORRODED. INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT FS 168, RBL 24. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2, 51-10-4, 5

All 100: https://openairdocs.org/deregistered/N14871-2004-12-07/reports.md

## Other aircraft with N14871

- [Cancelled 1949-08-18](https://openairdocs.org/deregistered/N14871-1949-08-18): Howard DGA-11, S/N 72, built 1936. Owner: [Morris Emmett Robert](https://openairdocs.org/faa-owner/MORRIS%20EMMETT%20ROBERT), [De Witt, AR](https://openairdocs.org/faa-place/AR/De%20Witt)

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