# N16804: 1984 Mcdonnell Douglas DC-9-82(MD-82), registration cancelled 2006-05-16

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: May 16, 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: [Pratt & Whitney JT9D-3A](https://openairdocs.org/engine/pratt-whitney-jt9d-3a) (registry code 52050)
- Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE), [TCDS E20EA](https://openairdocs.org/tcds/E20EA) (OpenAirDocs)
- Serial number: 49246
- Year built: 1984
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 13, 1984
- Certificate issued: October 21, 2003
- Last registry action: December 15, 2004
- Mode S code: A111DB
- Owner when cancelled: [Aeroturbine Inc](https://openairdocs.org/faa-owner/AEROTURBINE%20INC)
- Location: [Miami, FL](https://openairdocs.org/faa-place/FL/Miami)
- Owner type: Corporation
- Owner's area on the map: 25.8050° N, 80.3151° W: Placed by OpenAirDocs at the center of ZIP code 33122, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N16804
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=16804
- Page: https://openairdocs.org/deregistered/N16804-2006-05-16

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 (96, newest 50)

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

- [SDR CALA0000554](https://openairdocs.org/sdr/CALA0000554), Apr 25, 2000: ANGLE. CRACKED. VERTICAL AND HORIZONTAL SUPPORT ANGLES AT CFS 1485 VENT BOX ARE CRACKED (2). REMOVED AND REPLACED SUPPORT ANGLES PER SRM 51-30-5.
- [SDR CALA0000553](https://openairdocs.org/sdr/CALA0000553), Apr 25, 2000: BRACKET. CRACKED. LEFT SIDE HEAT EXCHANGER SUPPORT BRACKET CRACKEDAT FS 1429 LONG. 4L (8). REMOVED AND REPLACED BRACKET PER SRM 51-30-1.
- [SDR CALA0000507](https://openairdocs.org/sdr/CALA0000507), Apr 20, 2000: DOOR FRAME. CORRODED. INSPECTION FOUND AFT CARGO DOOR LOWER DOOR JAMB CORRODED BETWEEN STA 1156 AND 1212. A DOUBLER AND SPACER WERE INSTALLED IAW ECRA 5310-03027.
- [SDR CALA0000506](https://openairdocs.org/sdr/CALA0000506), Apr 19, 2000: FRAME. CORRODED. INSPECTION FOUND AFT CARGO PIT MAIN FRAME CENTER FLOOR STA 1300 CORRODED. REMOVED AND REPLACED SPLICES IAW SRM 51-30-2 AND 51-30-5.
- [SDR CALA0000505](https://openairdocs.org/sdr/CALA0000505), Apr 19, 2000: FLOOR SUPPORT. CORRODED. INSPECTION FOUND MID CARGO COMPARTMENT FLOORBOARD SUPPORT CORRODED AT FS 598 - 636, RBL 20. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-1.
- [SDR CALA0000504](https://openairdocs.org/sdr/CALA0000504), Apr 19, 2000: CARGO TRACK. CORRODED. INSPECTION FOUND THE AFT CARGO PIT RT FLOOR TIE DOWN TRACK CORRODED AT STA 1211. THE TIE DOWN TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-1.
- [SDR CALA0000500](https://openairdocs.org/sdr/CALA0000500), Apr 17, 2000: LONGERON. CORRODED. INSPECTION FOUND LONGERON 29L TO 29R HAD SEVERAL CORRODED FASTENERS IN LONGERONS AND SPLICES IN MID CARGO COMPARTMENT AT FS 579 - 598. THE LONGERON SPLICES WERE
- [SDR CALA0000499](https://openairdocs.org/sdr/CALA0000499), Apr 17, 2000: SKIN. DENTED. INSPECTION FOUND LT WING NR 1 SLAT DENTED. THE DENTED AREA WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 57-06, FIGURE 1.
- [SDR CALA0000498](https://openairdocs.org/sdr/CALA0000498), Apr 17, 2000: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FORWARD CARGO COMPARTMENT FLOOR SUPPORT CORRODED AT STA 427 - 463. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-1.
- [SDR CALA0000497](https://openairdocs.org/sdr/CALA0000497), Apr 17, 2000: DOOR FRAME. CORRODED. INSPECTION FOUND FORWARD CARGO DOOR JAMB AT O/B END OF TORQUE BOX CORRODED FROM STA 370 - 427. THE CORRODED AREA WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 
- [SDR CALA0000496](https://openairdocs.org/sdr/CALA0000496), Apr 17, 2000: WEB. CORRODED. INSPECTION FOUND AFT CARGO DOOR AFT JAMB TORQUE BOX UPPER WEB CORRODED AT LONGERON 28R. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-30-5.
- [SDR CALA0000482](https://openairdocs.org/sdr/CALA0000482), Apr 15, 2000: PAN. WORN. INSPECTION FOUND AFT CARGO DOOR PAN STOP WORN. A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-03, FIGURE 8 AND 51-10-3.
- [SDR CALA0000480](https://openairdocs.org/sdr/CALA0000480), Apr 15, 2000: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED IN AFT PIT AT STA 1117 FROM LONGERON 28L TO 28R. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-2.
- [SDR CALA0000479](https://openairdocs.org/sdr/CALA0000479), Apr 15, 2000: ANGLE. CRACKED. INSPECTION FOUND A 1.5 INCH CRACK IN VERTICAL STABILIZER REAR SPAR LOWER ATTACH ANGLE ON LT SIDE. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-5 AND 51-30-2
- [SDR CALA0000478](https://openairdocs.org/sdr/CALA0000478), Apr 15, 2000: SKIN. PUNCTURED. INSPECTION FOUND THREE HOLES PUNCTURED INTO RT I/B MLG DOOR OUTER SKIN UPPER BLOCK. THE DAMAGED SKIN WAS REMOVED AND REPLACED IAW SRM 51-30-2.
- [SDR CALA0000477](https://openairdocs.org/sdr/CALA0000477), Apr 15, 2000: BRACKET. CRACKED. INSPECTION FOUND A 4 INCH CRACK IN TWO RT AFT LAV WALL ATTACH ANGLE BRACKETS. THE WALL ATTACH ANGLE BRACKETS WERE REMOVED AND REPLACED IAW MM 51-10-2.
- [SDR CALA0000476](https://openairdocs.org/sdr/CALA0000476), Apr 15, 2000: CARGO TRACK. CORRODED. INSPECTION FOUND FORWARD CARGO RT TIEDOWN TRACK CORRODED AT FS 229 - 370. THE TIEDOWN TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-1.
- [SDR CALA0000475](https://openairdocs.org/sdr/CALA0000475), Apr 15, 2000: SKIN. DENTED. INSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AT FS 1380 BETWEEN LONGERON 4L AND 6L. THE DENTED SECTION OF SKIN WAS CUTOUT IAW SRM 53-01, FIGURE 2. A REPAIR DO
- [SDR CALA0000474](https://openairdocs.org/sdr/CALA0000474), Apr 15, 2000: SKIN. DAMAGED. INSPECTION FOUND LT WING TIP UPPER T/E SCREW HOLES ELONGATED. THE ELONGATED HOLES WERE CUTOUT AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-01, FIGURE 5 AND 51-
- [SDR CALA0000473](https://openairdocs.org/sdr/CALA0000473), Apr 15, 2000: SKIN. DENTED. INSPECTION FOUND LT HORIZONTAL STABILIZER O/B LEADING EDGE SKIN DENTED. DOUBLERS WERE INSTALLED IAW SRM 55-03, FIGURE 3.
- [SDR CALA0000472](https://openairdocs.org/sdr/CALA0000472), Apr 15, 2000: FITTING. CORRODED. INSPECTION FOUND SUPPORT FITTING CORRODED AT E & E COMPARTMENT INSIDE OF DOOR TORQUE BOX FS 148, LONGERON 28L. THE FITTING WAS REMOVED AND A NEW FITTING WAS INS
- [SDR CALA0000483](https://openairdocs.org/sdr/CALA0000483), Apr 14, 2000: PAN. WORN. INSPECTION FOUND FORWARD CARGO DOOR PAN WORN. A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-03, FIGURE 8 AND 51-10-3.
- [SDR CALA0000481](https://openairdocs.org/sdr/CALA0000481), Apr 14, 2000: BRACKET. WORN. INSPECTION FOUND TWO FORWARD AND TWO AFT SUPPORT BRACKETS HAD WORN AND ELONGATED HOLES AT AFT CARGO DOOR HINGE. A DOUBLER WAS INSTALLED IAW SRM 53-05, FIGURE 16
- [SDR CALA0000471](https://openairdocs.org/sdr/CALA0000471), Apr 14, 2000: SKIN. DENTED. INSPECTION FOUND EXTERNAL SKIN OF LT SIDE OF RUDDER DENTED BETWEEN CENTER AND LOWER HINGE POINT. A REPAIR DOUBLER WAS INSTALLED IAW SRM 55-01, FIGURE 10A, 51-10
- [SDR CALA0000470](https://openairdocs.org/sdr/CALA0000470), Apr 14, 2000: CARGO TRACK. CORRODED. INSPECTION FOUND RT TIEDOWN TRACK ATTACH FITTING CORRODED IN AFT CARGO PIT AT FS 1007. THE FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 51-30-1, 
- [SDR CALA0000469](https://openairdocs.org/sdr/CALA0000469), Apr 14, 2000: SKIN. CHAFED. INSPECTION FOUND EXTERNAL FUSELAGE SKIN CHAFED AT AREA OF HOLD OPEN HOOK RECEPTACLE FOR FORWARD ENTRY DOOR. THE CHAFED AREA WAS BLENDED IAW SRM 53-01, FIGURE 1.
- [SDR CALA0000468](https://openairdocs.org/sdr/CALA0000468), Apr 14, 2000: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED IN AFT PIT AT STA 1155 FROM LONGERON 28L TO 28R. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-2.
- [SDR CALA0000467](https://openairdocs.org/sdr/CALA0000467), Apr 14, 2000: FLOORBEAM. CORRODED. INSPECTION FOUND R-1 DOOR FLOORBEAM CORRODED AT FS 160 - 200, RBL 48. THE FLOORBEAM WAS REMOVED AND A NEW FLOORBEAM WAS INSTALLED IAW SRM 51-30-2, 51-10-3 AND 5
- [SDR CALA0000466](https://openairdocs.org/sdr/CALA0000466), Apr 13, 2000: DOUBLER. CRACKED. INSPECTION FOUND A 6 INCH CRACK IN LT MLG DOOR I/B LOWER AFT CORNER. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 28 AND 51-30-5
- [SDR CALA0000465](https://openairdocs.org/sdr/CALA0000465), Apr 13, 2000: CARGO TRACK. CORRODED. INSPECTION FOUND LT CARGO TIEDOWN TRACK CORRODED IN AFT PIT AT FS 1007 - 1360, LONGERON 27L. THE TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-30-3.
- [SDR CALA0000464](https://openairdocs.org/sdr/CALA0000464), Apr 13, 2000: ANGLE. CORRODED. INSPECTION FOUND WEB AND ATTACH ANGLE CORRODED AT PAX DOOR JAMB AFT SIDE, FS 200, LBL 58. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-2, 51-10-3, 51-10-4, 
- [SDR CALA0000461](https://openairdocs.org/sdr/CALA0000461), Apr 11, 2000: SKIN. GOUGED. INSPECTION FOUND RT MLG DOOR LOWER SKIN, GOUGED ON O/B SIDE. THE GOUGED SKIN SECTION WAS REMOVED AND A NEW SKIN SECTION WAS INSTALLED IAW SRM 51-30-2.
- [SDR CALA0000460](https://openairdocs.org/sdr/CALA0000460), Apr 11, 2000: SKIN. CHAFED. INSPECTION FOUND MID CARGO DOOR OUTER SKIN CHAFED AT LOWER AFT CORNER. A DOUBLER WAS INSTALLED IAW SRM 51-30-2.
- [SDR CALA0000458](https://openairdocs.org/sdr/CALA0000458), Apr 11, 2000: STOP. CHAFED. INSPECTION FOUND AFT CARGO DOOR PAN STOP CHAFED. A DOUBLER REPAIR WAS INSTALLED IAW SRM 51-10-3, 51-30-1, 51-30-2, AND ECRA 5330-02189.
- [SDR CALA0000456](https://openairdocs.org/sdr/CALA0000456), Apr 11, 2000: FITTING. CORRODED. INSPECTION FOUND DOOR LATCH SUPPORT FITTING INSIDE OF E&E COMPARTMENT DOOR CORRODED AT FS 48, LONGERON 28 RT. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-30
- [SDR CALA0000449](https://openairdocs.org/sdr/CALA0000449), Apr 8, 2000: FLOORBOARD. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN CABIN LT FLOOR SKIN AT FS 218, LBL 54. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 2, 51-10-
- [SDR CALA0000448](https://openairdocs.org/sdr/CALA0000448), Apr 8, 2000: WEB. CORRODED. INSPECTION FOUND CUSP WEB CORRODED AT FS 200 - 218, LBL 54. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-10-3, 53-01, FIGURE 4, 51-01, 51-30-2, 51
- [SDR ALA0000447](https://openairdocs.org/sdr/ALA0000447), Apr 8, 2000: BRACKET. CRACKED. INSPECTION FOUND SUB FLOOR BRACKET CRACKED AT FS 200, LBL 58. A NEW BRACKET WAS INSTALLED IAW SRM 51-30-5.
- [SDR CALA0000446](https://openairdocs.org/sdr/CALA0000446), Apr 8, 2000: FLOOR SUPPORT. CRACKED. INSPECTION FOUND A 4 INCH CRACK IN L-1 DOOR FLOOR SUPPORT AT FS 200. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-3 AND 51-30-5.
- [SDR CALA0000445](https://openairdocs.org/sdr/CALA0000445), Apr 8, 2000: FLOORBEAM. CORRODED. INSPECTION FOUND MID CARGO BAY FLOORBOARD SUPPORT CORRODED ON LOWER SIDE AT FS 636, LBL 15 TO RBL 15. THE FLOOR SUPPORT WAS REMOVEDAND REPLACED IAW SRM 51-30-2.
- [SDR ALA0000444](https://openairdocs.org/sdr/ALA0000444), Apr 8, 2000: ANGLE. CRACKED. INSPECTION FOUND A 6 CRACK IN CABIN RT SUPPORT ANGLE AT FS 1308, STRINGER 13 RT - 14 RT. THE FASTENER WAS REMOVED, THE CRACK WAS STOP DRILLED, AND A REPAIR ANGL
- [SDR CALA0000443](https://openairdocs.org/sdr/CALA0000443), Apr 8, 2000: FLOORBEAM. CORRODED. INSPECTION FOUND TOP T-CHORD OF FLOORBEAM CORRODED THE ENTIRE LENGTH AT STA 1322 LT, RT AND CENTER AISLE. THE FLOORBEAM WAS REMOVED AND REPLACED IAW SRM 53-05, 
- [SDR CALA0000442](https://openairdocs.org/sdr/CALA0000442), Apr 8, 2000: CARGO TRACK. CORRODED. INSPECTION FOUND RT CARGO TIE DOWN TRACK CORRODED IN AFT PIT AT FS 1007 - 1360. THE TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-1 AND 51-30-2.
- [SDR CALA0000441](https://openairdocs.org/sdr/CALA0000441), Apr 8, 2000: SKIN. GOUGED. INSPECTION FOUND EXTERNAL FUSELAGE SKIN GOUGED AT FS 487 BETWEEN LONGERON 23 RT AND 24 RT. A DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38.
- [SDR CALA0000440](https://openairdocs.org/sdr/CALA0000440), Apr 8, 2000: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT AT RT AFT LAV CENTER AISLE, FS 1307 - 1338 CORRODED. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-01.
- [SDR CALA0000439](https://openairdocs.org/sdr/CALA0000439), Apr 8, 2000: WEB. WORN. INSPECTION FOUND A HOLE WORN INTO CUSP WEB AT FS 220, RBL 54. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-01, PAGE 18, 53-11-3, PAGE 49, 51-30-08, AND 53-01, FIGU
- [SDR CALA0000438](https://openairdocs.org/sdr/CALA0000438), Apr 8, 2000: WEB. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN L-1 DOOR CUSP WEB AT AFT END AND BULGING AT RIVETS, FS 198. FILLERS AND DOUBLERS WERE INSTALLED IAW ECRA 5320-01638 AND SRM 5
- [SDR CALA0000452](https://openairdocs.org/sdr/CALA0000452), Apr 8, 2000: CARGO TRACK. CORRODED. INSPECTION FOUND MID CARGO BAY FLOOR, LT CARGO TRACK CORRODED AROUND CLIPNUT HOLES ON LOWER SURFACE, FS 579 - 676. THE CARGO TRACK WAS REMOVED AND REPLACED IAW 
- [SDR CALA0000451](https://openairdocs.org/sdr/CALA0000451), Apr 8, 2000: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED AT RT FS 1007 IN AFT CARGO BAY. THE SUPPORT WAS REMOVED AND A NEW SUPPORT AND REPAIR DOUBLER WERE INSTALLED IAW SRM 51-3
- [SDR CALA0000450](https://openairdocs.org/sdr/CALA0000450), Apr 8, 2000: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED JUST INSIDE AFT CARGO BAY DOORWAY. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-1.

All 96: https://openairdocs.org/deregistered/N16804-2006-05-16/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 19980104006259I](https://openairdocs.org/incident/19980104006259I), Jan 4, 1998: Doug DC982 (N16804), Omaha, NE. Narrative: aircraft en-route denver, co to cleveland, oh diverted into Omaha, NE due to #2 engine oil leak and some smoke in the cabin. The aircraft landed…

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