# Service difficulty reports: N72830, cancelled Jun 24, 2005

A list on [N72830, cancelled Jun 24, 2005](https://openairdocs.org/deregistered/N72830-2005-06-24.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 · 71 reports

- [SDR CALA0400059](https://openairdocs.org/sdr/CALA0400059.md): Floor Support · corroded · Jan 25, 2004 · N72830 · Doug DC982 · Fuselage Miscellaneous Structure
  > 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.md): Beltframe · cracked · Dec 13, 2002 · N72830 · Doug DC982 · Fuselage Main, Frame
  > 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.md): Cable · frayed · Dec 11, 2002 · N72830 · Doug DC982 · Aerodynamic Fairings
  > 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. REMOVED AND REPLACED CABLE ASSEMBLY. RIGGED AND ADJUSTED TAILCONE RELEASE SYSTEM IAW MM 53-53-00.
- [SDR CALA0200577](https://openairdocs.org/sdr/CALA0200577.md): Longeron · cracked · Dec 9, 2002 · N72830 · Doug DC982 · Fuselage Main, Longeron/Stringer
  > 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.md): Intercostal · cracked · Dec 9, 2002 · N72830 · Doug DC982 · Fuselage Miscellaneous Structure
  > 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.md): Intercostal · cracked · Dec 8, 2002 · N72830 · Doug DC982 · Fuselage Miscellaneous Structure
  > 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 51-70-05.
- [SDR CALA0000732](https://openairdocs.org/sdr/CALA0000732.md): Panel · corroded · May 21, 2000 · N72830 · Doug DC982 · Fuselage Main, Bulkhead
  > 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 51-30-2.
- [SDR CALA0000728](https://openairdocs.org/sdr/CALA0000728.md): Cargo Track · corroded · May 20, 2000 · N72830 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > 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 REPLACED IAW SRM 51-30-1.
- [SDR CALA0000727](https://openairdocs.org/sdr/CALA0000727.md): Fitting · cracked · May 20, 2000 · N72830 · Doug DC982 · Cargo/Baggage Doors
  > 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.md): Skin · dented · May 18, 2000 · N72830 · Doug DC982 · Fuselage Main, Plate/Skin
  > 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.md): Skin · worn · May 17, 2000 · N72830 · Doug DC982 · Service Doors
  > 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.md): Seat Track · corroded · May 17, 2000 · N72830 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > 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.md): Frame · gouged · May 17, 2000 · N72830 · Doug DC982 · Fuselage Main, Frame
  > 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 51-30-2.
- [SDR CALA0000690](https://openairdocs.org/sdr/CALA0000690.md): Longeron · cracked · May 17, 2000 · N72830 · Doug DC982 · Fuselage Main, Longeron/Stringer
  > 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.md): Pan · worn · May 17, 2000 · N72830 · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND FORWARD CARGO DOOR AFT TO CENTER 3 DOOR STOPS WORN. REPAIRED IAW ECRA 5330-02819.
- [SDR CALA0000688](https://openairdocs.org/sdr/CALA0000688.md): Attach Fitting · cracked · May 17, 2000 · N72830 · Doug DC982 · Vertical Stabilizer, Attach Fittings
  > 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.md): Skin · punctured · May 16, 2000 · N72830 · Doug DC982 · Fuselage Main, Plate/Skin
  > 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 WAS REMOVED, AN EXTERNAL AND INTERNAL DOUBLER WERE INSTALLED IAW SRM 53-04, FIGURES 4 AND 38.
- [SDR CALA0000685](https://openairdocs.org/sdr/CALA0000685.md): Strap · cracked · May 16, 2000 · N72830 · Doug DC982 · Fuselage Miscellaneous Structure
  > 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 STRAP WAS REMOVED AND REPLACED IAW SRM 51-30-1.
- [SDR CALA0000684](https://openairdocs.org/sdr/CALA0000684.md): Pan · worn · May 16, 2000 · N72830 · Doug DC982 · Cargo/Baggage Doors
  > 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 51-30-2.
- [SDR CALA0000683](https://openairdocs.org/sdr/CALA0000683.md): Angle · corroded · May 16, 2000 · N72830 · Doug DC982 · Fuselage Miscellaneous Structure
  > 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.md): Cargo Track · corroded · May 15, 2000 · N72830 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > 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.md): Floorboard · corroded · May 15, 2000 · N72830 · Doug DC982 · Fuselage Floor Panel
  > 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.md): Pan · worn · May 15, 2000 · N72830 · Doug DC982 · Cargo/Baggage Doors
  > 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.md): Door Frame · corroded · May 15, 2000 · N72830 · Doug DC982 · Fuselage Main, Structure
  > 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.md): Skin · cracked · May 15, 2000 · N72830 · Doug DC982 · Fuselage Main, Plate/Skin
  > 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 INSTALLED IAW SRM 52-01, FIGURE 4.
- [SDR CALA0000674](https://openairdocs.org/sdr/CALA0000674.md): Beam · cracked · May 11, 2000 · N72830 · Doug DC982 · Fuselage Main, Structure
  > 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.md): Panel · cracked · May 11, 2000 · N72830 · Doug DC982 · Vertical Stabilizer, Plate/Skin
  > INSPECTION FOUND VERTICAL STABILIZER REAR SPAR LOWER ACCESS PANEL CRACKED IN SEVERAL PLACES. THE CRACKS WERE APPROXIMATELY.5 INCH LONG. THE CRACKS WERE STOP DRILLED IAW SRM 53-01, FIGURE 2. DOUBLERS WERE INSTALLED IAW SRM 53-01, FIGURE 1 AND 51-10-3.
- [SDR CALA0000672](https://openairdocs.org/sdr/CALA0000672.md): Bracket · cracked · May 11, 2000 · N72830 · Doug DC982 · Fuselage Main, Structure
  > 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 BRACKET WAS REMOVED AND REPLACED IAW SRM 51-30-1.
- [SDR CALA0000671](https://openairdocs.org/sdr/CALA0000671.md): Pan · chafed · May 11, 2000 · N72830 · Doug DC982 · Cargo/Baggage Doors
  > 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.md): Cargo Track · corroded · May 10, 2000 · N72830 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > 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.md): Panel · corroded · May 10, 2000 · N72830 · Doug DC982 · Wing, Plate/Skin
  > 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.md): Floor Support · corroded · May 10, 2000 · N72830 · Doug DC982 · Fuselage Miscellaneous Structure
  > 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.md): Attach Angle · cracked · May 10, 2000 · N72830 · Doug DC982 · Fuselage, Stabilizer Attach Fittings
  > 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.md): Skin · dented · May 10, 2000 · N72830 · Doug DC982 · Trailing Edge Flaps
  > 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 AND 51-30-8.
- [SDR CALA0000654](https://openairdocs.org/sdr/CALA0000654.md): Skin · chafed · May 10, 2000 · N72830 · Doug DC982 · Cargo/Baggage Doors
  > 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.md): Skin · cracked · May 10, 2000 · N72830 · Doug DC982 · Cargo/Baggage Doors
  > 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, FIGURE 26A. AN ANGLE WAS INSTALLED IAW SRM 52-05, FIGURE 26A AND 51-10-3.
- [SDR CALA0000652](https://openairdocs.org/sdr/CALA0000652.md): Cargo Track · corroded · May 10, 2000 · N72830 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > 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.md): Skin · gouged · May 10, 2000 · N72830 · Doug DC982 · Cargo/Baggage Doors
  > 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 1, 52-20, FIGURE 2, 51-10-3, AND 52-01, FIGURE 2.
- [SDR CALA0000650](https://openairdocs.org/sdr/CALA0000650.md): Pan · worn · May 10, 2000 · N72830 · Doug DC982 · Cargo/Baggage Doors
  > 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.md): Floor Support · corroded · May 8, 2000 · N72830 · Doug DC982 · Fuselage Miscellaneous Structure
  > 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.md): Floor Support · corroded · May 8, 2000 · N72830 · Doug DC982 · Fuselage Miscellaneous Structure
  > 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.md): Floor Support · corroded · May 8, 2000 · N72830 · Doug DC982 · Fuselage Miscellaneous Structure
  > 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.md): Cargo Track · corroded · May 8, 2000 · N72830 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > 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.md): Floor Support · corroded · May 8, 2000 · N72830 · Doug DC982 · Fuselage Miscellaneous Structure
  > 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.md): Web · cracked · May 4, 2000 · N72830 · Doug DC982 · Fuselage Miscellaneous Structure
  > 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.md): Seat Track · gouged · May 4, 2000 · N72830 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > 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.md): Seat Track · gouged · May 4, 2000 · N72830 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > 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.md): Galley Track · corroded · May 4, 2000 · N72830 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > 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.md): Floor Support · corroded · May 4, 2000 · N72830 · Doug DC982 · Fuselage Miscellaneous Structure
  > 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.md): Seat Track · corroded · May 4, 2000 · N72830 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > 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.

Next page: https://openairdocs.org/deregistered/N72830-2005-06-24/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 = 'N72830' AND deregistration_id = 'N72830-2005-06-24'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N72830-2005-06-24/reports

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