# N13891: 1982 Mcdonnell Douglas DC-9-82(MD-82), registration cancelled 2003-05-12

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: May 12, 2003
- 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: 49102
- Year built: 1982
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: November 24, 1982
- Certificate issued: March 18, 1999
- Last registry action: March 26, 2002
- Mode S code: A09C96
- Owner when cancelled: [Castle Harbour-I LLC](https://openairdocs.org/faa-owner/CASTLE%20HARBOUR-I%20LLC)
- Location: Hamilton, Bermuda
- Owner type: Corporation
- The mark today: https://openairdocs.org/aircraft/N13891
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=13891
- Page: https://openairdocs.org/deregistered/N13891-2003-05-12

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 (59, newest 50)

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

- [SDR CALA0100877](https://openairdocs.org/sdr/CALA0100877), Sep 15, 2001: SUPPORT. CRACKED. INSPECTION FOUND A 1.52 INCH CRACK IN NR 1 PYLON UPPER SUPPORT ANGLE AT CANTED FRAME 1463, L17L. A REPAIR ANGLE WAS INSTALLED IAW ECRA 5410-01555.
- [SDR CALA0001524](https://openairdocs.org/sdr/CALA0001524), Oct 9, 2000: SKIN. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN WEB SKIN JUST FORWARD OF TRIM AT TAIL COMPARTMENT STA 1485, RT SIDE. THE AFT ACCESSORY VENT RT BOX WAS REMOVED IAW SRM 51-30-
- [SDR CALA0001523](https://openairdocs.org/sdr/CALA0001523), Oct 9, 2000: WEB. CORRODED. INSPECTION FOUND CUSP WEB CORRODED AT STA 195, LBL 22-LBL 44. THE CORRODED AREA WAS CUT OUT AND A DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 1 AND 51-30-2.
- [SDR CALA0001522](https://openairdocs.org/sdr/CALA0001522), Oct 9, 2000: BEAM. CORRODED. INSPECTION FOUND LEFT LAV I/B FORWARD AFT BEAM ON FLOOR BENT AND CORRODED AT FORWARD END. THE LAV BEAM WAS REMOVED AND A NEW BEAM WAS INSTALLED IAW 51-10-2, 51-
- [SDR CALA0001507](https://openairdocs.org/sdr/CALA0001507), Oct 6, 2000: SKIN. DENTED. INSPECTION FOUND THE LEFT FUSELAGE SKIN DENTED AT STA 389 - 436, LONGERON 22L. REPAIRED IAW ECRA 5331-01082 AND EA 9-5331-2-A0754.
- [SDR CALA0001492](https://openairdocs.org/sdr/CALA0001492), Oct 5, 2000: WEB. TORN. CUSP WEB TORN FS 214 AT RBL 10 TO RBL 14. CUT OUT DAMAGED AREA. FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER PER SRM 51-30-8.
- [SDR CALA0001491](https://openairdocs.org/sdr/CALA0001491), Oct 5, 2000: SEAT TRACK. CORRODED. RIGHT INBOARD SEAT TRACK CORRODED AT STATION 200 TO 266. REMOVED AND REPLACED SEAT TRACK SECTION PER SRM 51-30-1, 51-30-2, 51-30-5, 53-05 FIG 4F AND 51-10-4.
- [SDR CALA0001490](https://openairdocs.org/sdr/CALA0001490), Oct 5, 2000: SKIN. DENTED. EXTERIOR SKIN DENTED AT STATION 265 AT LONGERON 20R. REWORKED DENT. FABRICATED AND INSTALLED DOUBLER PER SRM 53-04 FIG 38 AND 51-30-2.
- [SDR CALA0001489](https://openairdocs.org/sdr/CALA0001489), Oct 5, 2000: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT CORRODED AT STATION 256 CENTER. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-30-5 AND 53-14-2 FIG 4 SHEET 1.
- [SDR CALA0001488](https://openairdocs.org/sdr/CALA0001488), Oct 5, 2000: SKIN. DENTED. AFT CARGO DOOR SKIN CENTER AFT IS DENTED. REMOVED DAMAGED AREA. REPAIRED SKIN PER SRM 51-50-1 FIG 1 AND 52-05 FIG 3.
- [SDR CALA0001487](https://openairdocs.org/sdr/CALA0001487), Oct 5, 2000: SKIN. DENTED. LEFT EXTERIOR SKIN DENTED AT STA 200 BETWEEN LONG 22L AND 23L. FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 53-04 AND 51-10-4.
- [SDR CALA0001486](https://openairdocs.org/sdr/CALA0001486), Oct 5, 2000: LONGERON. CRACKED. TAIL COMPARTMENT STA 1446 LONG 6R IS CRACKED 1 INCH. REMOVED CRACKED LONGERON. FABRICATED AND INSTALLED NEW LONGERON PER SRM 53-02, 51-10-4 AND 51-10-3.
- [SDR CALA0001485](https://openairdocs.org/sdr/CALA0001485), Oct 5, 2000: CARGO TRACK. CORRODED. MID PIT RT AFT TRACK SECTION FORWARD END OUTBOARD EDGE CORRODED. REMOVED DAMAGED SECTION. FABRICATED AND INSTALLED NEW SECTION OF TRACK PER SRM 51-10-3, 53-01, 
- [SDR CALA0001432](https://openairdocs.org/sdr/CALA0001432), Sep 26, 2000: FLOOR SUPPORT. CORRODED. STA 200 LBL 12 FLOOR SUPPORT IS CORRODED. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 1-30-5.
- [SDR CALA0001431](https://openairdocs.org/sdr/CALA0001431), Sep 26, 2000: FLOOR SUPPORT. CORRODED. STA 200 RBL 10 - RBL 46 FLOOR SUPPORT HAS ELONGATED HOLES AND CORROSION. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-30-5.
- [SDR CALA0001424](https://openairdocs.org/sdr/CALA0001424), Sep 21, 2000: WEB. PUNCTURED. INSPECTION FOUND SUB FLOOR PUNCTURED AT FS 170, RBL 15.5, 21, 26, 36, AND 41. THE PUNCTURED AREAS WERE CUT OUT IAW SRM 53-01, FIGURE 1. A DOUBLER WAS INSTALLED 
- [SDR CALA0001423](https://openairdocs.org/sdr/CALA0001423), Sep 21, 2000: WEB. CORRODED. INSPECTION FOUND CUSP WEB CORRODED AT FS 1076 - 1086, RBL 58. THE FASTENERS AND FRAME FITTINGS WERE REMOVED FROM AROUND THE CORRODED AREA AND THE CORRODED AREA 
- [SDR CALA0001422](https://openairdocs.org/sdr/CALA0001422), Sep 21, 2000: WEB. CRACKED. INSPECTION FOUND A 5 INCH CRACK IN CUSP WEB AT FS 886, LBL 50. THE CRACK WAS STOP DRILLED IAW SRM 53-01, FIGURE 2. A DOUBLER WAS INSTALLED IAW SRM 53-01, 51-10-
- [SDR CALA0001426](https://openairdocs.org/sdr/CALA0001426), Sep 18, 2000: STRUCTURE. DENTED. UPPER AFT EMERGENCY WALKWAY DENTED AT AFT SECTION AFT OF EXIT PAINT. CUT OUT DAMAGED SECTION PER SRM 53-01 FIG 2. VERIFIED NO CRACKS PAST CUTOUT AREA. FABRICATE
- [SDR CALA0001413](https://openairdocs.org/sdr/CALA0001413), Sep 18, 2000: CHANNEL. CORRODED. INSPECTION FOUND AFT VENTRAL DOOR THRESHOLD AREA UNDER FLOOR L-CHANNEL CORRODED AT FS 1338. SUPPORT ANGLES WERE REMOVED AND REPLACED IAW SRM 51-10-4 AND EA 9-53
- [SDR CALA0001401](https://openairdocs.org/sdr/CALA0001401), Sep 6, 2000: SKIN. GOUGED. INSPECTION FOUND LT WING NR 5 SLAT LOWER SKIN GOUGED AT I/B END. A DOUBLER WAS INSTALLED IAW SRM 57-03, FIGURE 4, 51-10-3, AND 51-30-8.
- [SDR CALA0001396](https://openairdocs.org/sdr/CALA0001396), Sep 5, 2000: FLOORBEAM. CORRODED. INSPECTION FOUND LT LAV FLOORBEAM BOLT HOLES CORRODED AT FS 1338. AN ANGLE REPAIR WAS INSTALLED IAW SRM 51-10-3, 51-30-05, 51-30-02, AND EA 9-5321-2-A0762.
- [SDR CALA0001395](https://openairdocs.org/sdr/CALA0001395), Sep 5, 2000: STOP. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN BOTH THE AFT AND FWD LOWER DOOR STOPS ON FWD CARGO DOOR. THE CRACKS WERE STOP DRILLED IAW SRM 52-03. DOUBLERS WERE INSTALLED 
- [SDR CALA0001394](https://openairdocs.org/sdr/CALA0001394), Sep 4, 2000: WEB. CRACKED. INSPECTION FOUND THREE .5 INCH CRACKS IN SUBFLOOR BETWEEN FS 150 AND 168, LBL 22. THE CRACKED AREA WAS REMOVED IAW SRM 53-01, FIGURE 1. A DOUBLER WAS INSTALLED 
- [SDR CALA0001463](https://openairdocs.org/sdr/CALA0001463), Aug 30, 2000: SUPPORT BRACKET. CHAFED. FORWARD FUSELAGE STATION 37 RIGHT HAND PAN SUPPORT HAS DEEP CHAFE. REMOVED AND REPLACED SUPPORT, FABRICATED AND INSTALLED DOUBLER PER SRM 53-01 FIG 1, 51-30-2, 
- [SDR CALA0001335](https://openairdocs.org/sdr/CALA0001335), Aug 28, 2000: SKIN. DAMAGED. INSPECTION FOUND LT FUSELAGE EXTERIOR SKIN CREASED AT STA 218 BETWEEN LONGERON 18L AND 19L. THE CREASED AREA WAS CUT OUT IAW SRM 53-04, FIGURE 25. A DOUBLER AND
- [SDR CALA0001459](https://openairdocs.org/sdr/CALA0001459), Aug 22, 2000: SEAT TRACK. CORRODED. RT HAND OUTBOARD SEAT TRACKS STA 1125 - 1200 IS CORRODED OUT OF LIMITS. REMOVED SECTION OF SEAT TRACK FROM STA 1125 - 1230 IAW SRM 53-05 FIG 4, RECEIVED SEAT TR
- [SDR CALA0001305](https://openairdocs.org/sdr/CALA0001305), Aug 22, 2000: WEB. CRACKED. INSPECTION FOUND A 6 INCH CRACK IN CUSP WEB AT FS 886, RBL 44 - 45. THE CRACKED AREA WAS CUT OUT AND A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-01, FIGURE 2A, 51
- [SDR CALA0001447](https://openairdocs.org/sdr/CALA0001447), Aug 18, 2000: WEB. PUNCTURED. SUB FLOOR PUNCTURED APPROX FS 170 - RBL 10. CUT OUT DAMAGED AREA IAW SRM 53-01 FIG 1. FABRICATED DOUBLER IAW SRM 53-14-1 FIG 4. LOCATED AND DRILLED IAW SRM 51-3
- [SDR CALA0001453](https://openairdocs.org/sdr/CALA0001453), Aug 17, 2000: WEB. CRACKED. RIGHT HAND CUSP WEB FS 245 AT RBL 44 CRACKED (.5 INCH) AND PUNCTURED. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER REPAIR PER SRM 53-01 FIG 2, 51-10-3, AND 51-30-
- [SDR CALA0001446](https://openairdocs.org/sdr/CALA0001446), Aug 17, 2000: WEB. CRACKED. RT SIDE CUSP WEB FS 245 APPROX RBL 44 CRACKED AND PUNCTURED. CUT OUT PUNCTURED PER SRM 53-01 FIG 2, FABBED REPAIR DOUBLER PER SRM 53-01 FIG 2, TREATED AND PRIME
- [SDR CALA0001458](https://openairdocs.org/sdr/CALA0001458), Aug 15, 2000: WEB. CORRODED. CUSP WEB HEAVILY CORRODED AT FS 224 APPROX LBL 58. FABRICATED CUSP WEB AT FAB SHOP ON TRAVELLER T9073. TREATED AND PRIMED IAW SRM 51-10-3, LOCATED AND TRIMMED A
- [SDR CALA0001457](https://openairdocs.org/sdr/CALA0001457), Aug 15, 2000: FLOOR SUPPORT. CORRODED. STA 160 - 195 LBL 54 FLOOR SUPPORT IN FWD ENTRY IS CORRODED BEYOND LIMITS. REMOVED FLOOR SUPPORT ON TRAVELLER T8983, FOUND CORROSION ON SUB FLOOR. REMOVED CORRO
- [SDR CALA0001456](https://openairdocs.org/sdr/CALA0001456), Aug 15, 2000: FLOOR SUPPORT. CORRODED. STA 148 - 200 RBL 54 FLOOR SUPPORT CORRODED BEYOND LIMITS (FWD ENTRY). REMOVED FLOOR SUPPORT IAW SRM 51-10-2, RECEIVED NEW FLOOR SUPPORT TRAVELLER T9012, TREATE
- [SDR CALA0001455](https://openairdocs.org/sdr/CALA0001455), Aug 15, 2000: WEB. CORRODED. CUSP WEB HEAVILY CORRODED AT FS 224 APPROX LBL 58. FABRICATED CUSP WEB AT FAB SHOP ON TRAVELLER T9073, TREATED AND PRIMED IAW SRM 51-10-3, LOCATED, TRIMMED AND 
- [SDR CALA0001454](https://openairdocs.org/sdr/CALA0001454), Aug 15, 2000: SKIN. GOUGED. RIGHT AILERON LOWER SURFACE SKIN IS GOUGED (.5 INCH) AT LEADING EDGE 18 INCHES OUTBOARD OF DAMPERS. REMOVED AILERON IAW MD-80 MM 27-10-01, REPAIRED AILERON IAW 
- [SDR CALA0001452](https://openairdocs.org/sdr/CALA0001452), Aug 15, 2000: FLOORBEAM. CORRODED. FLOORBEAM CORRODED AT STA 218 LBL 10 - RBL 10. REMOVED AND REPLACED FLOORBEAM PER SRM 51-30-2, 51-10-4, 51-10-3, AND 51-30-5.
- [SDR CALA0001451](https://openairdocs.org/sdr/CALA0001451), Aug 15, 2000: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT CORRODED IN FORWARD ENTRY AREA STA 160 - 195 LBL 54. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-30-2, AND 51-10-03.
- [SDR CALA0001450](https://openairdocs.org/sdr/CALA0001450), Aug 15, 2000: FLOORBEAM. CORRODED. FLOORBEAM CORRODED AT FORWARD ENTRY STA 168 RBL 9 - RBL 43. REPLACED FLOORBEAM PER SRM 51-10-04, 51-30-03, 51-30-2, AND 51-30-5.
- [SDR CALA0001449](https://openairdocs.org/sdr/CALA0001449), Aug 15, 2000: FLOORBEAM. CORRODED. FLOORBEAM ELONGATED HOLES AND CORROSION AT STA 160 LBL 5 - RBL 5. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED BEAM PER SRM 51-30-5, 51-10-4, AND 51-10-3.
- [SDR CALA0001448](https://openairdocs.org/sdr/CALA0001448), Aug 15, 2000: FLOOR SUPPORT. CORRODED. STA 148 - 200 RBL 7 FLOOR SUPPORT CORRODED OUT OF LIMITS FWD ENTRY. REMOVED FLOOR SUPPORT IAW SRM 51-10-2, RECEIVED NEW PART ON TRAVELLER T9013, LOCATE AND DRIL
- [SDR CALA0001445](https://openairdocs.org/sdr/CALA0001445), Aug 15, 2000: SKIN. GOUGED. RT AILERON LWR SURFACE SKIN IS GOUGED AT L/E APPROX 18 INCHES O/B OF DAMPERS. REMOVED AILERON IAW MD-80 MM 27-10-01. REPAIRED AILERON IAW MD-80 SRM 57-01 FIG 5 
- [SDR CALA0001444](https://openairdocs.org/sdr/CALA0001444), Aug 15, 2000: FLOORBEAM. CORRODED. STA 218 LBL 10 - RBL 10 FLOORBEAM OUT OF LIMITS FWD ENTRY. REMOVED FLOOR SUPPORT IAW SRM 51-30-2, RECEIVED NEW FLOORBEAM ON T9010, LOCATED AND DRLLED IAW SRM 51
- [SDR CALA0001443](https://openairdocs.org/sdr/CALA0001443), Aug 15, 2000: FLOOR SUPPORT. CORRODED. STA 195 - 200 LBL 17 FLOOR SUPPORT IS CORRODED OUT OF LIMIT (FWD ENTRY). REMOVED FLOOR SUPPORT IAW SRM 51-30-2, ROUTED TO FAB SHOP, RECEIVED NEW FLOOR SUPPORT O
- [SDR CALA0001442](https://openairdocs.org/sdr/CALA0001442), Aug 15, 2000: FLOORBEAM. CORRODED. STA 200 LBL 5- FLOORBEAM IS CORRODED OUT OF LIMITS FWD ENTRY. REMOVED BEAM FOUND TO BE OUT OF LIMITS, FAB NEW BEAM ON T8981, TREATED AND PRIMED IAW SRM 51-10-3,
- [SDR CALA0001441](https://openairdocs.org/sdr/CALA0001441), Aug 15, 2000: FLOOR SUPPORT. CORRODED. STA 148 - 200 LBL 7 FLOOR SUPPORT IS CORRODED BEYOND LIMITS FWD ENTRY. REMOVED FLOOR SUPPORT AND ROUTED TO FAB (REMOVAL PER SRM 51-30-2) RECEIVED FROM FAB-FABBE
- [SDR CALA0001440](https://openairdocs.org/sdr/CALA0001440), Aug 15, 2000: FLOORBEAM. CORRODED. STA 168 LBL 16-BLL 38 FLOORBEAM HAS CORROSION FWD ENTRY. REMOVED FLOORBEAM IAW SRM 51-30-2, SENT TO FAB SHOP FOR NEW FLOORBEAM, TREATED AND PRIMED IAW SRM 51-10
- [SDR CALA0001439](https://openairdocs.org/sdr/CALA0001439), Aug 15, 2000: FLOOR SUPPORT. CORRODED. STA 160 - 195 LBL 44 FLOOR SUPPORT IS CORRODED AND HAS ELONGATED HOLES FWD ENTRY. REMOVED FLOOR IAW SRM 51-30-2, FLOOR SUPPORT, FABBED ON TRAVELLER T-8979, DRIL
- [SDR CALA0001438](https://openairdocs.org/sdr/CALA0001438), Aug 15, 2000: FLOOR SUPPORT. CORRODED. STA 160 - 200 RBL 44 FLOOR SUPPORT OUT OF LIMITS FWD ENTRY. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-30-5, RECEIVED FLOOR SUPPORT FROM TRAVELER T9018, LOCA
- [SDR CALA9900123](https://openairdocs.org/sdr/CALA9900123), Feb 14, 1999: OIL SYST. OVERSERVICED. A MODERATE AMOUNT OF SMOKE APPEARED IN THE COCKPIT AND CABIN AFTER TAKEOFF FROM EWR WITH THE PNEUMATIC PRESSURE GAUGE READING 70 PSI. THE SMOKE SLOWLY DISSIPATE

All 59: https://openairdocs.org/deregistered/N13891-2003-05-12/reports.md

## FAA accident and incident reports (2)

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 19990206020739I](https://openairdocs.org/incident/19990206020739I), Feb 6, 1999: Doug DC982 (N13891), Cleveland, OH. Aircraft diverted to Cleveland without incident due to decreased oil pressure, #2 engine. Continental maintenance removed and replaced #2 eng.
- [Incident 19980920033059I](https://openairdocs.org/incident/19980920033059I), Sep 20, 1998: Doug DC982 (N13891), Chicago, IL. At 26,000 feet acft encountered ice. The engine anti-ice and airfoil ice protection system was activated. Within seconds the following lights came on and…

## Other aircraft with N13891

- [Cancelled 2012-05-01](https://openairdocs.org/deregistered/N13891-2012-05-01): Waco UKC, S/N 3845. Exported to Philippines. Owner: [Phillippine Aereal Taxi Co](https://openairdocs.org/faa-owner/PHILLIPPINE%20AEREAL%20TAXI%20CO), Manila

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