# Service difficulty reports: N16804, cancelled May 16, 2006

A list on [N16804, cancelled May 16, 2006](https://openairdocs.org/deregistered/N16804-2006-05-16.md).

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

Page 1 of 2 · 96 reports

- [SDR CALA0000554](https://openairdocs.org/sdr/CALA0000554.md): Angle · cracked · Apr 25, 2000 · N16804 · Doug DC982 · Fuselage Main, Attach Fittings
  > 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.md): Bracket · cracked · Apr 25, 2000 · N16804 · Doug DC982 · Fuselage Miscellaneous Structure
  > 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.md): Door Frame · corroded · Apr 20, 2000 · N16804 · Doug DC982 · Fuselage Miscellaneous Structure
  > 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.md): Frame · corroded · Apr 19, 2000 · N16804 · Doug DC982 · Fuselage Main, Frame
  > 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.md): Floor Support · corroded · Apr 19, 2000 · N16804 · Doug DC982 · Fuselage Miscellaneous Structure
  > 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.md): Cargo Track · corroded · Apr 19, 2000 · N16804 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > 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.md): Longeron · corroded · Apr 17, 2000 · N16804 · Doug DC982 · Fuselage Main, Longeron/Stringer
  > 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 REMOVED AND REPLACED IAW SRM 51-30-5.
- [SDR CALA0000499](https://openairdocs.org/sdr/CALA0000499.md): Skin · dented · Apr 17, 2000 · N16804 · Doug DC982 · Leading Edge Devices
  > 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.md): Floor Support · corroded · Apr 17, 2000 · N16804 · Doug DC982 · Fuselage Miscellaneous Structure
  > 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.md): Door Frame · corroded · Apr 17, 2000 · N16804 · Doug DC982 · Cargo/Baggage Doors
  > 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 53-05, FIGURE 44.
- [SDR CALA0000496](https://openairdocs.org/sdr/CALA0000496.md): Web · corroded · Apr 17, 2000 · N16804 · Doug DC982 · Fuselage Miscellaneous Structure
  > 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.md): Pan · worn · Apr 15, 2000 · N16804 · Doug DC982 · Cargo/Baggage Doors
  > 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.md): Floor Support · corroded · Apr 15, 2000 · N16804 · Doug DC982 · Fuselage Miscellaneous Structure
  > 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.md): Angle · cracked · Apr 15, 2000 · N16804 · Doug DC982 · Vertical Stabilizer, Attach Fittings
  > 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.md): Skin · punctured · Apr 15, 2000 · N16804 · Doug DC982 · Landing Gear Doors
  > 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.md): Bracket · cracked · Apr 15, 2000 · N16804 · Doug DC982 · Fuselage Miscellaneous Structure
  > 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.md): Cargo Track · corroded · Apr 15, 2000 · N16804 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > 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.md): Skin · dented · Apr 15, 2000 · N16804 · Doug DC982 · Fuselage Main, Plate/Skin
  > 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 DOUBLER AND FILLER WERE INSTALLED IAW SRM 53-01, FIGURE 2, 51-30-02, AND 51-30-08.
- [SDR CALA0000474](https://openairdocs.org/sdr/CALA0000474.md): Skin · damaged · Apr 15, 2000 · N16804 · Doug DC982 · Wing, Plate/Skin
  > 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 51-30-2.
- [SDR CALA0000473](https://openairdocs.org/sdr/CALA0000473.md): Skin · dented · Apr 15, 2000 · N16804 · Doug DC982 · Horizontal Stabilizer, Plate/Skin
  > 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.md): Fitting · corroded · Apr 15, 2000 · N16804 · Doug DC982 · Fuselage Miscellaneous Structure
  > 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 INSTALLED IAW SRM 51-30-5.
- [SDR CALA0000483](https://openairdocs.org/sdr/CALA0000483.md): Pan · worn · Apr 14, 2000 · N16804 · Doug DC982 · Cargo/Baggage Doors
  > 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.md): Bracket · worn · Apr 14, 2000 · N16804 · Doug DC982 · Cargo/Baggage Doors
  > 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 16A.
- [SDR CALA0000471](https://openairdocs.org/sdr/CALA0000471.md): Skin · dented · Apr 14, 2000 · N16804 · Doug DC982 · Rudder, Plate/Skin
  > 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, 51-10-4, 51-10-3, AND 51-30-6.
- [SDR CALA0000470](https://openairdocs.org/sdr/CALA0000470.md): Cargo Track · corroded · Apr 14, 2000 · N16804 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > 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, 51-10-4, AND 51-10-3.
- [SDR CALA0000469](https://openairdocs.org/sdr/CALA0000469.md): Skin · chafed · Apr 14, 2000 · N16804 · Doug DC982 · Fuselage Main, Plate/Skin
  > 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. A DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 24.
- [SDR CALA0000468](https://openairdocs.org/sdr/CALA0000468.md): Floor Support · corroded · Apr 14, 2000 · N16804 · Doug DC982 · Fuselage Miscellaneous Structure
  > 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.md): Floorbeam · corroded · Apr 14, 2000 · N16804 · Doug DC982 · Fuselage Main, Floor Beam
  > 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 51-30-1.
- [SDR CALA0000466](https://openairdocs.org/sdr/CALA0000466.md): Doubler · cracked · Apr 13, 2000 · N16804 · Doug DC982 · Landing Gear Doors
  > 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.md): Cargo Track · corroded · Apr 13, 2000 · N16804 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > 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.md): Angle · corroded · Apr 13, 2000 · N16804 · Doug DC982 · Fuselage Miscellaneous Structure
  > 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, AND 51-30-5.
- [SDR CALA0000461](https://openairdocs.org/sdr/CALA0000461.md): Skin · gouged · Apr 11, 2000 · N16804 · Doug DC982 · Landing Gear Doors
  > 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.md): Skin · chafed · Apr 11, 2000 · N16804 · Doug DC982 · Cargo/Baggage Doors
  > 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.md): Stop · chafed · Apr 11, 2000 · N16804 · Doug DC982 · Cargo/Baggage Doors
  > 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.md): Fitting · corroded · Apr 11, 2000 · N16804 · Doug DC982 · Fuselage Miscellaneous Structure
  > 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 51-30-5.
- [SDR CALA0000449](https://openairdocs.org/sdr/CALA0000449.md): Floorboard · cracked · Apr 8, 2000 · N16804 · Doug DC982 · Fuselage Floor Panel
  > 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, 51-10-3, 51-10-4, 51-30-2, AND 51-30-5.
- [SDR CALA0000448](https://openairdocs.org/sdr/CALA0000448.md): Web · corroded · Apr 8, 2000 · N16804 · Doug DC982 · Fuselage Miscellaneous Structure
  > 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, 51-30-5, AND 51-30-6.
- [SDR ALA0000447](https://openairdocs.org/sdr/ALA0000447.md): Bracket · cracked · Apr 8, 2000 · N16804 · Doug DC982 · Fuselage Miscellaneous Structure
  > 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.md): Floor Support · cracked · Apr 8, 2000 · N16804 · Doug DC982 · Fuselage Miscellaneous Structure
  > 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.md): Floorbeam · corroded · Apr 8, 2000 · N16804 · Doug DC982 · Fuselage Main, Floor Beam
  > 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.md): Angle · cracked · Apr 8, 2000 · N16804 · Doug DC982 · Fuselage Miscellaneous Structure
  > 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 ANGLE WAS INSTALLED IAW SRM 51-30-5 AND 51-30-2.
- [SDR CALA0000443](https://openairdocs.org/sdr/CALA0000443.md): Floorbeam · corroded · Apr 8, 2000 · N16804 · Doug DC982 · Fuselage Main, Floor Beam
  > 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, FIGURE 20A.
- [SDR CALA0000442](https://openairdocs.org/sdr/CALA0000442.md): Cargo Track · corroded · Apr 8, 2000 · N16804 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > 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.md): Skin · gouged · Apr 8, 2000 · N16804 · Doug DC982 · Fuselage Main, Plate/Skin
  > 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.md): Floor Support · corroded · Apr 8, 2000 · N16804 · Doug DC982 · Fuselage Miscellaneous Structure
  > 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.md): Web · worn · Apr 8, 2000 · N16804 · Doug DC982 · Fuselage Miscellaneous Structure
  > 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, FIGURE 4.
- [SDR CALA0000438](https://openairdocs.org/sdr/CALA0000438.md): Web · cracked · Apr 8, 2000 · N16804 · Doug DC982 · Fuselage Miscellaneous Structure
  > 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 51-10-3.
- [SDR CALA0000452](https://openairdocs.org/sdr/CALA0000452.md): Cargo Track · corroded · Apr 8, 2000 · N16804 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > 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 SRM 51-30-1 AND 51-30-2.
- [SDR CALA0000451](https://openairdocs.org/sdr/CALA0000451.md): Floor Support · corroded · Apr 8, 2000 · N16804 · Doug DC982 · Fuselage Miscellaneous Structure
  > 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 51-30-2, 53-01, FIGURE 2, 51-10-3, AND 51-60, FIGURE 1.
- [SDR CALA0000450](https://openairdocs.org/sdr/CALA0000450.md): Floor Support · corroded · Apr 8, 2000 · N16804 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT CORRODED JUST INSIDE AFT CARGO BAY DOORWAY. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-1.

Next page: https://openairdocs.org/deregistered/N16804-2006-05-16/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N16804' AND deregistration_id = 'N16804-2006-05-16'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N16804-2006-05-16/reports

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