# N72830: 1987 Mcdonnell Douglas DC-9-82(MD-82), registration cancelled 2005-06-24 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: June 24, 2005 - Exported to: Ukraine - 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: [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: 49490 - Year built: 1987 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: March 27, 1987 - Certificate issued: April 22, 1998 - Last registry action: November 13, 2002 - Mode S code: A9C41E - Owner when cancelled: [Wells Fargo Bank Northwest Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20BANK%20NORTHWEST%20NA%20TRUSTEE) - Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City) - Owner type: Corporation - Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N72830 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=72830 - Page: https://openairdocs.org/deregistered/N72830-2005-06-24 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 (71, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CALA0400059](https://openairdocs.org/sdr/CALA0400059), Jan 25, 2004: FLOOR SUPPORT. CORRODED. INSPECTION FOUND RT FLOOR SUPPORT ZEE ANGLE CORRODED IN MID BAGGAGE BIN AT STA 620. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-00-00. - [SDR CALA0200585](https://openairdocs.org/sdr/CALA0200585), Dec 13, 2002: BELTFRAME. CRACKED. INSPECTION FOUND A 1/2" CRACK IN BELTFRAME AT STA 1418, LONGERON 2L-2R. A REPAIR WAS INSTALLED IAW SRM 53-03, FIGURE 31 AND ECRA 5310-04301. - [SDR CALA0200583](https://openairdocs.org/sdr/CALA0200583), Dec 11, 2002: CABLE. FRAYED. THE TAILCONE RELEASE AT EXTERIOR AND INTERIOR HANDLES PULLED HIGH. THE UPPER L/H TAILCONE JETTISON CABLE WAS FOUND WORN AND FRAYED AT UPPER FORWARD PULLEY. REMO - [SDR CALA0200577](https://openairdocs.org/sdr/CALA0200577), Dec 9, 2002: LONGERON. CRACKED. INSPECTION FOUND A 2" CRACK IN LONGERON 2R AT STA 1418. A REPAIR WAS PERFORMED IAW ECRA 5311-01132. - [SDR CALA0200576](https://openairdocs.org/sdr/CALA0200576), Dec 9, 2002: INTERCOSTAL. CRACKED. NSPECTION FOUND A 3" CRACK IN INTERCOSTAL IN AFT BAGGAGE BIN BETWEEN STA 1271 AND 1287 AT CEILING RIGHT OF CENTERLINE. INSTALLED REPAIR IAW SRM 51-30. - [SDR CALA0200575](https://openairdocs.org/sdr/CALA0200575), Dec 8, 2002: INTERCOSTAL. CRACKED. INSPECTION FOUND A 3" CRACK IN INTERCOSTAL IN AFT BAGGAGE BIN AT CEILING BETWEEN STA 1287 AND 1309, JUST RIGHT OF CENTER. A REPAIR DOUBLER WAS INSTALLED IAW SRM - [SDR CALA0000732](https://openairdocs.org/sdr/CALA0000732), May 21, 2000: PANEL. CORRODED. INSPECTION FOUND TOP SURFACE OF REMOVEABLE BULKHEAD FLOOR TRANSITION PANEL IN AFT CARGO PIT AT STA 1320 CORRODED. THE PANEL WAS REMOVED AND REPLACED IAW SRM 51- - [SDR CALA0000728](https://openairdocs.org/sdr/CALA0000728), May 20, 2000: CARGO TRACK. CORRODED. INSPECTION FOUND RT CARGO TIE DOWN TRACK IN AFT CARGO PIT CORRODED ON UPPER AND LOWER SURFACE AT STA 1022 - 1155, RBL 24. THE TIE DOWN TRACK WAS REMOVED AND REP - [SDR CALA0000727](https://openairdocs.org/sdr/CALA0000727), May 20, 2000: FITTING. CRACKED. INSPECTION FOUND A 1.7 INCH CRACK IN FORWARD CARGO DOOR LOWER FITTING. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-30-6. - [SDR CALA0000712](https://openairdocs.org/sdr/CALA0000712), May 18, 2000: SKIN. DENTED. INSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AT FS 408 BETWEEN LONGERONS 29L AND 28R. A SKIN REPAIR DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 12B. - [SDR CALA0000696](https://openairdocs.org/sdr/CALA0000696), May 17, 2000: SKIN. WORN. INSPECTION FOUND THE FORWARD SERVICE DOOR SKIN WORN UNDER DOOR GUIDE. A DOUBLER WAS INSTALLED IAW ECRA 5240-01341. - [SDR CALA0000692](https://openairdocs.org/sdr/CALA0000692), May 17, 2000: SEAT TRACK. CORRODED. INSPECTION FOUND CENTER SEAT TRACK CORRODED AT STA 228, RBL 22.5. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-05, FIGURE 4F. - [SDR CALA0000691](https://openairdocs.org/sdr/CALA0000691), May 17, 2000: FRAME. GOUGED. INSPECTION FOUND FORWARD SIDE OF FRAME GOUGED AT PREVIOUS REPAIR IN AFT ACCESSORY AREA, FS 1380, L4L. THE REPAIR DOUBLER WAS REMOVED AND REPLACED IAW SRM 51-30- - [SDR CALA0000690](https://openairdocs.org/sdr/CALA0000690), May 17, 2000: LONGERON. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN LONGERON 2L AT FS 1438. THE LONGERON WAS REMOVED AND A NEW SECTION WAS SPLICED IN IAW SRM 53-02, FIGURE 18. - [SDR CALA0000689](https://openairdocs.org/sdr/CALA0000689), May 17, 2000: PAN. WORN. INSPECTION FOUND FORWARD CARGO DOOR AFT TO CENTER 3 DOOR STOPS WORN. REPAIRED IAW ECRA 5330-02819. - [SDR CALA0000688](https://openairdocs.org/sdr/CALA0000688), May 17, 2000: ATTACH FITTING. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN VERTICAL STABILIZER AFT SPAR LOWER CENTER ATTACH ANGLE, FS 1485. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-2. - [SDR CALA0000686](https://openairdocs.org/sdr/CALA0000686), May 16, 2000: SKIN. PUNCTURED. A PERMANENT REPAIR WAS INSTALLED WHERE A TEMPORARY REPAIR HAD PREVIOUSLY BEEN DONE FOR A 1 INCH HOLE IN THE FUSELAGE SKIN AT FS 324, L23L. THE TEMPORARY REPAIR - [SDR CALA0000685](https://openairdocs.org/sdr/CALA0000685), May 16, 2000: STRAP. CRACKED. INSPECTION FOUND FORWARD CARGO DOOR JAMB FLOOR PANEL SUPPORT STRAP FOR AFT SIDE OF JAMB CRACKED AT FS 427, L27R. THE CRACK WAS TWO INCHES LONG. THE SUPPORT STRA - [SDR CALA0000684](https://openairdocs.org/sdr/CALA0000684), May 16, 2000: PAN. WORN. INSPECTION FOUND FORWARD CARGO DOOR SECOND FROM TOP FORWARD STOP AND LOWER AFT STOP WORN. A DOUBLER WAS INSTALLED AT EACH LOCATION IAW ECRA 5330-02819 AND SRM 5 - [SDR CALA0000683](https://openairdocs.org/sdr/CALA0000683), May 16, 2000: ANGLE. CORRODED. INSPECTION FOUND AFT CARGO PIT RT FORWARD ANGLE CORRODED. THE ANGLE WAS REMOVED AND RERPLACED IAW SRM 51-30-1. - [SDR CALA0000681](https://openairdocs.org/sdr/CALA0000681), May 15, 2000: CARGO TRACK. CORRODED. INSPECTION FOUND FORWARD CARGO LT TIE DOWN TRACK CORRODED AROUND CLIP NUTS FROM FS 218 - 522. THE TRACK WAS REMOVED AND REPLACED IAW SRM 51-10-3 AND 51-30-1. - [SDR CALA0000680](https://openairdocs.org/sdr/CALA0000680), May 15, 2000: FLOORBOARD. CORRODED. INSPECTION FOUND AFT CARGO PIT REMOVABLE BULKHEAD FLOOR TRANSITION PANEL CORRODED ON TOP SURFACE AT STA 1320. THE PANEL WAS REMOVED AND REPLACED IAW SRM 51-30-2 - [SDR CALA0000679](https://openairdocs.org/sdr/CALA0000679), May 15, 2000: PAN. WORN. INSPECTION FOUND FORWARD CARGO DOOR THIRD FROM TOP FORWARD STOP WORN. THE AREA WAS REPAIRED IAW ECRA 5330-02819 AND A DOUBLER WAS INSTALLED IAW SRM 51-30-2. - [SDR CALA0000678](https://openairdocs.org/sdr/CALA0000678), May 15, 2000: DOOR FRAME. CORRODED. INSPECTION FOUND AFT CARGO PIT DOOR JAMB FORWARD FACE CORRODED AT STA 1155 - 1212. THE DOOR JAMB WAS REMOVED AND REPLACED IAW SRM 51-10-1 AND 51-10-2. - [SDR CALA0000677](https://openairdocs.org/sdr/CALA0000677), May 15, 2000: SKIN. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN AFT VENTRAL STAIR LOWER SKIN AT CENTER RT EDGE, FS 1479, L27R. THE CRACKED AREA WAS REMOVED AND FILLER AND DOUBLER WERE INSTA - [SDR CALA0000674](https://openairdocs.org/sdr/CALA0000674), May 11, 2000: BEAM. CRACKED. INSPECTION FOUND MID CARGO FORWARD WALL VERTICAL SUPPORT BEAM CRACKED AT FS 522, LBL 8. THE SUPPORT BEAM WAS REMOVED AND REPLACED IAW SRM 51-30-2. - [SDR CALA0000673](https://openairdocs.org/sdr/CALA0000673), May 11, 2000: PANEL. CRACKED. INSPECTION FOUND VERTICAL STABILIZER REAR SPAR LOWER ACCESS PANEL CRACKED IN SEVERAL PLACES. THE CRACKS WERE APPROXIMATELY .5 INCH LONG. THE CRACKS WERE STOP DR - [SDR CALA0000672](https://openairdocs.org/sdr/CALA0000672), May 11, 2000: BRACKET. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN LT MLG WHEEL WELL SUPPORT BRACKET AFT OF KEEL BOX WHERE KEEL AND AFT BULKHEAD CONNECT AT FS 1003, LONGERON 29L. THE SUPPORT B - [SDR CALA0000671](https://openairdocs.org/sdr/CALA0000671), May 11, 2000: PAN. CHAFED. INSPECTION FOUND FORWARD CARGO DOOR FORWARD TOP STOP CHAFED. A DOUBLER WAS INSTALLED IAW ECRA 5330-02819, SRM 51-10-4, AND 51-10-3. - [SDR CALA0000660](https://openairdocs.org/sdr/CALA0000660), May 10, 2000: CARGO TRACK. CORRODED. INSPECTION FOUND MID CARGO LT TIE DOWN TRACK CORRODED AT FS 674 - 788. THE TIE DOWN TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-1 AND 51-30-2. - [SDR CALA0000659](https://openairdocs.org/sdr/CALA0000659), May 10, 2000: PANEL. CORRODED. INSPECTION FOUND RT WING ACCESS PANEL NR1611A CORRODED AROUND FASTENER HOLES. THE ACCESS PANEL WAS REMOVED AND REPLACED IAW SRM 51-30-0. - [SDR CALA0000657](https://openairdocs.org/sdr/CALA0000657), May 10, 2000: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 160 - 200. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-2. - [SDR CALA0000656](https://openairdocs.org/sdr/CALA0000656), May 10, 2000: ATTACH ANGLE. CRACKED. INSPECTION FOUND DORSAL FIN LT INNER ATTACH ANGLE CRACKED. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-4 AND 51-30-2. - [SDR CALA0000655](https://openairdocs.org/sdr/CALA0000655), May 10, 2000: SKIN. DENTED. THE NR 4 LT FLAP T/E PANEL UPPER SKIN WAS DENTED WITH TWO INNER RIBS BENT. THE RIBS WERE REMOVED AND REPLACED AND REPAIR ANGLES WERE INSTALLED IAW SRM 51-30-2 A - [SDR CALA0000654](https://openairdocs.org/sdr/CALA0000654), May 10, 2000: SKIN. CHAFED. INSPECTION FOUND MID CARGO DOOR OUTER SKIN LOWER DOUBLER FWD AND AFT CHAFED AT THE EDGE. THE DOUBLER WAS REMOVED AND REPLACED IAW SRM 51-30-2. - [SDR CALA0000653](https://openairdocs.org/sdr/CALA0000653), May 10, 2000: SKIN. CRACKED. INSPECTION FOUND AFT CARGO DOOR SKIN BENT AT FORWARD LOWER SIDE WITH A .25 INCH CRACK AT DOOR LATCHING MECHANISM. THE CRACK WAS STOP DRILLED IAW SRM 52-05, FIGU - [SDR CALA0000652](https://openairdocs.org/sdr/CALA0000652), May 10, 2000: CARGO TRACK. CORRODED. INSPECTION FOUND AFT CARGO LT TIE DOWN TRACK CORRODED AT STA 1007 - 1211. THE TIE DOWN TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-1 AND 51-30-2. - [SDR CALA0000651](https://openairdocs.org/sdr/CALA0000651), May 10, 2000: SKIN. GOUGED. INSPECTION FOUND FORWARD CARGO DOOR INNER SKIN AT LOWER RADIUS CHAFED AND GOUGED FROM CORNER TO DOOR LOCK CAM. A DOUBLER REPAIR WAS INSTALLED SRM 52-01, FIGURE - [SDR CALA0000650](https://openairdocs.org/sdr/CALA0000650), May 10, 2000: PAN. WORN. INSPECTION FOUND AFT CARGO DOOR PAN WORN IN FOUR PLACES. A DOUBLER WAS INSTALLED AT EACH LOCATION IAW SRM 51-10-3, 51-30-2, AND ECRA 5330-02819. - [SDR CALA0000642](https://openairdocs.org/sdr/CALA0000642), May 8, 2000: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 1155, LBL 22 - 44. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-5. - [SDR CALA0000641](https://openairdocs.org/sdr/CALA0000641), May 8, 2000: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORTS CORRODED AT FS 180, BL 0 AND RBL 12 - 44. THE FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW SRM 51-30-5. - [SDR CALA0000640](https://openairdocs.org/sdr/CALA0000640), May 8, 2000: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 160 - 200, RBL 44. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-5. - [SDR CALA0000639](https://openairdocs.org/sdr/CALA0000639), May 8, 2000: CARGO TRACK. CORRODED. INSPECTION FOUND MID CARGO RT TIE DOWN TRACK CORRODED UNDER NUT PLATES AT FS 522 - 636, L27R. THE TIE DOWN TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-2. - [SDR CALA0000638](https://openairdocs.org/sdr/CALA0000638), May 8, 2000: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT ANGLE UNDER L-2 DOOR DRAIN PAN CORRODED. THE SUPPORT ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-4 AND 51-30-5. - [SDR CALA0000623](https://openairdocs.org/sdr/CALA0000623), May 4, 2000: WEB. CRACKED. OUTBOARD WEB CRACKED AT FS 250 LEFT (1.5 INCHES). STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER PER SRM 53-01 FIG 2, 51-10-3, AND 51-10-4. - [SDR CALA0000622](https://openairdocs.org/sdr/CALA0000622), May 4, 2000: SEAT TRACK. GOUGED. RIGHT SIDE INBOARD SEAT TRACK HAS GOUGES AT STA 332. REMOVED AND REPLACED SEAT TRACK PER SRM 53-05 FIG 4. - [SDR CALA0000621](https://openairdocs.org/sdr/CALA0000621), May 4, 2000: SEAT TRACK. GOUGED. SEAT TRACK HAS GOUGING AND A DAMAGED LOBE WHERE SEAT WAS MOUNTED AT FS 370 LEFT I/B TRACK. REMOVED AND REPLACED SEAT TRACK PER SRM 53-05 FIG 4. - [SDR CALA0000620](https://openairdocs.org/sdr/CALA0000620), May 4, 2000: GALLEY TRACK. CORRODED. G2 GALLEY SUPPORT MOUNT CORRODED AT FS 212 RBL 12. REMOVED AND REPLACED GALLEY SUPPORT PER SRM 51-30-5. - [SDR CALA0000619](https://openairdocs.org/sdr/CALA0000619), May 4, 2000: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT AT RBL 10 TO LBL 10 AT FS 200 BROKEN EAR AND CORRODED. REMOVED AND REPLACED SUPPORT PER SRM 51-10-4 AND 51-10-3. - [SDR CALA0000618](https://openairdocs.org/sdr/CALA0000618), May 4, 2000: SEAT TRACK. CORRODED. CENTER SEAT TRACK LBL 44 FS 1098 TO 1174 CORRODED AROUND NUT PLATE UPPER AND LOWER FLANGES. REPLACED SEAT TRACK PER SRM 53-05 FIG 4F SHEET 1. All 71: https://openairdocs.org/deregistered/N72830-2005-06-24/reports.md ## NTSB investigations (1) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB DEN88IA043](https://openairdocs.org/ntsb/DEN88IA043), Dec 27, 1987: Mcdonnell Douglas MD-80 (N72830), Denver, CO, incident, minor damage ## 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. - [Accident 19871227081359A](https://openairdocs.org/incident/19871227081359A), Dec 27, 1987: Doug DC982 (N72830), Denver, CO, Substantial damage. Collided with a taxiway marker on landing rollout. Due to blowing snow, visibility was zero. ## Other aircraft with N72830 - [Cancelled 1956-02-20](https://openairdocs.org/deregistered/N72830-1956-02-20): Cessna 140, S/N 10016. Owner: [Five Ace Club Inc](https://openairdocs.org/faa-owner/FIVE%20ACE%20CLUB%20INC) --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.