# Service difficulty reports: N17812, cancelled Apr 1, 2004

A list on [N17812, cancelled Apr 1, 2004](https://openairdocs.org/deregistered/N17812-2004-04-01.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 · 89 reports

- [SDR CALA0300159](https://openairdocs.org/sdr/CALA0300159.md): Skin · dented · Mar 11, 2003 · N17812 · Doug DC982 · Cargo/Baggage Doors
  > MAINTENANCE FOUND A CREASE IN THE AFT UPPER CORNER OF THE OUTER SKIN OF THE AFT CARGO DOOR. THE CREASED AREA OF DOOR SKIN WAS REPAIRED IAW ECRA 5232-01023. A DIP WAS ISSUED TO PERFORM INSPECTION OF THE REPAIR IAW ECRA 5232-01023 BEGINNING AT OR BEFORE 45,815 C
- [SDR CALA0300108](https://openairdocs.org/sdr/CALA0300108.md): Frame · corroded · Mar 8, 2003 · N17812 · Doug DC982 · Fuselage Main, Frame
  > INSPECTION FOUND BELTFRAME LOWER CHANNEL AND WEB CORRODED AT STA 1309 FROM LONGERON 28L TO 28R. REPAIRED IAW SRM 53-03, PAGE 04A, FIGURE 2A.
- [SDR CALA0300107](https://openairdocs.org/sdr/CALA0300107.md): Cable · out of rig · Mar 8, 2003 · N17812 · Doug DC982 · Aerodynamic Fairings
  > THE TAILCONE FAILED TO DROP WITHIN SPECIFICATIONS AT ALL THREE POSITIONS DURING FUNCTIONAL TEST. THE PULL EXCEEDED 35 POUNDS. THE TAILCONE CABLES WERE ADJUSTED IAW 53-53-00.
- [SDR CALA0300106](https://openairdocs.org/sdr/CALA0300106.md): Light · inoperative · Mar 8, 2003 · N17812 · Doug DC982 · Escape Slide
  > THE TAILCONE SLIDE LIGHT FAILED BATTERY TEST. THE SLIDE ASSEMBLY WAS REMOVED AND REPLACED IAW MM 25-62-01.
- [SDR CALA0300101](https://openairdocs.org/sdr/CALA0300101.md): Frame · cracked · Mar 7, 2003 · N17812 · Doug DC982 · Fuselage Main, Frame
  > INSPECTION FOUND A 1" CRACK IN FRAME RADIUS AT STA 1418, LONGERON 2L AND 2R. REPAIRS WERE INSTALLED AT EACH LOCATION IAW ECRA 5310-04332.
- [SDR CALA0300100](https://openairdocs.org/sdr/CALA0300100.md): Web · corroded · Mar 6, 2003 · N17812 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND WEB AT STA 1338 AFT PRESSURE BULKHEAD T-CAP CORRODED. THE CORRODED SECTION OF WEB WAS CUT OUT AND A NEW SECTION WAS INSTALLED IAW SRM 51-70-4, FIGURE 1.
- [SDR CALA0300093](https://openairdocs.org/sdr/CALA0300093.md): Frame · cracked · Mar 3, 2003 · N17812 · Doug DC982 · Fuselage Main, Frame
  > INSPECTION FOUND A 3/4" CRACK IN FRAME AT STA 1418, LONGERON 1. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-03, FIGURE 4.
- [SDR CALA0300089](https://openairdocs.org/sdr/CALA0300089.md): Casting · cracked · Mar 3, 2003 · N17812 · Doug DC982 · Passenger/Crew Doors
  > INSPECTION FOUND A 1/2" CRACK IN AFT ENTRY DOOR LEFT LOWER CASTING. THE CASTING WAS REMOVED AND A NEW CASTING WAS INSTALLED IAW SRM 51-30-0.
- [SDR CALA0100630](https://openairdocs.org/sdr/CALA0100630.md): Battery · discharged · Jul 2, 2001 · N17812 · Doug DC982 · Emergency Lighting
  > THE EMERGENCY CEILING LIGHTS WERE FOUND INOPERATIVE AT ROW 15. THE BATTERIES WERE REMOVED AND REPLACED AND OPERATION CHECKED GOOD.
- [SDR CALA0000744](https://openairdocs.org/sdr/CALA0000744.md): Skin · cracked · May 25, 2000 · N17812 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CABIN LT SUBFLOOR SKIN CRACKED AT FS 218. THE SUBFLOOR PANEL WAS REMOVED IAW SRM 51-30-2 AND 51-30-5. A NEW SUBFLOOR WAS INSTALLED IAW SRM 53-14-1, 51-10-4, AND 51-30-1.
- [SDR CALA0000743](https://openairdocs.org/sdr/CALA0000743.md): Cargo Track · corroded · May 25, 2000 · N17812 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND AFT CARGO LT TIE DOWN TRACK CORRODED FROM STA 1003 - 1212. THE TIE DOWN TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-1 AND 51-30-2.
- [SDR CALA0000304](https://openairdocs.org/sdr/CALA0000304.md): Clip · cracked · Mar 13, 2000 · N17812 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 2.3 INCH CRACK IN AFT CARGO FORWARD BULKHEAD FRAME CLIP AT STA 1003, LONGERON 28R. THE CLIP WAS REMOVED AND A NEW CLIP WAS INSTALLED IAW SRM 51-30-5, 51-10-3, 51-10-4, AND 51-30-2.
- [SDR CALA0000303](https://openairdocs.org/sdr/CALA0000303.md): Skin · cracked · Mar 13, 2000 · N17812 · Doug DC982 · Landing Gear Doors
  > INSPECTION FOUND A 4 INCH CRACK IN PREVIOUS DOUBLER REPAIR OF UPPER FORWARD CORNER RT MLG DOOR. THE DOUBLER WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-30-5.
- [SDR CALA0000301](https://openairdocs.org/sdr/CALA0000301.md): Floorbeam · gouged · Mar 11, 2000 · N17812 · Doug DC982 · Fuselage Main, Floor Beam
  > INSPECTION FOUND AFT CARGO CEILING FLOORBEAM GOUGED AT FS 1174, RBL 2. A DOUBLER AND SHIM WERE INSTALLED IAW SRM 53-05, FIGURE 86, 51-10-2, 51-10-3, AND 53-04, FIGURE 36.
- [SDR CALA0000300](https://openairdocs.org/sdr/CALA0000300.md): Cargo Track · corroded · Mar 11, 2000 · N17812 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND MID PIT RT CARGO TIE DOWN TRACK CORRODED FROM STA 427-636. THE TRACK WAS REMOVED AND NEW TRACK WAS INSTALLED IAW SRM 51-30-1 AND 51-30-2.
- [SDR CALA0000299](https://openairdocs.org/sdr/CALA0000299.md): Skin · dented · Mar 11, 2000 · N17812 · Doug DC982 · Rudder, Plate/Skin
  > INSPECTION FOUND RUDDER SKIN DENTED AT UPPER LEFT SIDE. THE DENTED AREA WAS REMOVED. A FILLER AND DOUBLER REPAIR WAS INSTALLED IAW SRM 55-03 AND 51-10-3.
- [SDR CALA0000298](https://openairdocs.org/sdr/CALA0000298.md): Skin · dented · Mar 11, 2000 · N17812 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AT FS 133 BETWEEN LONGERONS 18L AND 19L. THE DENT WAS COLD WORKED IAW SRM 53-04, FIGURE 38. A DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38 AND 51-10-3.
- [SDR CALA0000297](https://openairdocs.org/sdr/CALA0000297.md): Skin · dented · Mar 11, 2000 · N17812 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND RIGHT EXTERNAL FUSELAGE SKIN DENTED AT STA 560 BETWEEN LONGERON 21R AND 22R. THE DOUBLER WAS REMOVED AND THE AREA WAS COLD WORKED IAW ECRA 5330-01856. A REPAIR WAS INSTALLED IAW SRM 51-10-3, 53-04, FIGURE 38, AND ECRA 5330-01856.
- [SDR CALA0000296](https://openairdocs.org/sdr/CALA0000296.md): Stop · gouged · Mar 11, 2000 · N17812 · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND FORWARD CARGO DOOR STOP GOUGED. A DOUBLER WAS INSTALLED IAW SRM 52-03, FIGURE 8, 51-10-2, 51-10-3, AND 51-30-2.
- [SDR CALA0000295](https://openairdocs.org/sdr/CALA0000295.md): Skin · gouged · Mar 11, 2000 · N17812 · Doug DC982 · Ailerons
  > INSPECTION FOUND LEFT AILERON LOWER SURFACE SKIN GOUGED. THE AILERON WAS REPAIRED IAW ECRA 5750-03367.
- [SDR CALA0000294](https://openairdocs.org/sdr/CALA0000294.md): Pan · cracked · Mar 11, 2000 · N17812 · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND SEVERAL.125 INCH CRACKS AROUND DOOR SEAL RIVET HOLE AT AFT CARGO DOOR UPPER AFT CORNER. THE FASTENERS WERE REMOVED IAW SRM 52-03, FIGURE 8. DOUBLERS WERE INSTALLED IAW SRM 51-10-4, 51-10-3, AND 52-03, FIGURE 8.
- [SDR CALA0000291](https://openairdocs.org/sdr/CALA0000291.md): Bracket · cracked · Mar 10, 2000 · N17812 · Doug DC982 · Engine Thrust Reverser
  > INSPECTION FOUND NR 2 T/R UPPER DOOR I/B SIDE WING FAIRING SUPPORT BRACKET AND ANGLE CLIP CRACKED. THE CRACKS WERE 1 AND 1/8 LONG. THE I/B SIDE SUPPORT BRACKET AND ANGLE CLIP WERE REMOVED IAW SRM 51-30-2. REPAIR WAS INSTALLED IAW SRM 51-10-2, 51-10-3, 51-30
- [SDR CALA0000290](https://openairdocs.org/sdr/CALA0000290.md): Stop · gouged · Mar 10, 2000 · N17812 · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND MID CARGO DOOR STOPS GOUGED IN TWO PLACES. DOUBLERS WERE INSTALLED IAW SRM 51-10-3, 51-30-2, AND 51-30-5, AND ECRA 5330-02819.
- [SDR CALA0000289](https://openairdocs.org/sdr/CALA0000289.md): Cargo Track · corroded · Mar 10, 2000 · N17812 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND AFT CARGO TIE DOWN TRACK CORRODED FROM STA 1003 TO 1212. THE TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-1 AND 51-30-2.
- [SDR CALA0000288](https://openairdocs.org/sdr/CALA0000288.md): Stop · gouged · Mar 10, 2000 · N17812 · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND AFT CARGO DOOR STOPS GOUGED IN THREE PLACES. REPAIRS WERE INSTALLED IAW SRM 52-03, FIGURE 8, 51-10-3, AND ECRA 5330-02819.
- [SDR CALA0000287](https://openairdocs.org/sdr/CALA0000287.md): Skin · cracked · Mar 9, 2000 · N17812 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A 2 INCH CRACK IN FUSELAGE SKIN NEXT TO TOP RT RADOME HINGE. A DOUBLER AND FILLER WERE INSTALLED IAW SRM 51-10-3 AND 53-05, FIGURE 7.
- [SDR CALA0000286](https://openairdocs.org/sdr/CALA0000286.md): Stop · worn · Mar 9, 2000 · N17812 · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND MID CARGO DOOR STOP WORN. A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-03, FIGURE 8, 51-10-3, AND 51-30-2.
- [SDR CALA0000285](https://openairdocs.org/sdr/CALA0000285.md): Support · corroded · Mar 9, 2000 · N17812 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 200, LBL 12 TO LBL 15. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-4.
- [SDR CALA0000284](https://openairdocs.org/sdr/CALA0000284.md): Skin · dented · Mar 9, 2000 · N17812 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND EXTERNAL FUSELAGE SKIN SCRATCHED AND DENTED AT FS 280 BETWEEN LONGERONS 22L AND 23L. THE AREA WAS COLD WORKED AND DOUBLERS WERE INSTALLED IAW SRM 53-01, FIGURE 38 AND 51-10-3.
- [SDR CALA0000283](https://openairdocs.org/sdr/CALA0000283.md): Cargo Track · corroded · Mar 9, 2000 · N17812 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND AFT CARGO AFT RT TIE DOWN TRACK CORRODED AROUND FASTENER HOLES. THE TIE DOWN TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-2.
- [SDR CALA0000282](https://openairdocs.org/sdr/CALA0000282.md): Intercostal · corroded · Mar 8, 2000 · N17812 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND INTERCOSTAL CORRODED AT FS 1309-1331, LONGERON 29R. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-30-5.
- [SDR CALA0000281](https://openairdocs.org/sdr/CALA0000281.md): Floor Panel · corroded · Mar 8, 2000 · N17812 · Doug DC982 · Fuselage Floor Panel
  > INSPECTION FOUND COCKPIT FLOOR SKIN CORRODED AT FS 160, LBL 6. THE CORROSION WAS REMOVED IAW SRM 53-01, FIGURE 2 AND 51-10-3. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 2, 51-10-04, 51-30-02.
- [SDR CALA0000280](https://openairdocs.org/sdr/CALA0000280.md): Stop · worn · Mar 8, 2000 · N17812 · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND TWO MID CARGO DOOR STOPS WORN. REPAIRED STOPS IAW ECRA 5330-02819.
- [SDR CALA0000279](https://openairdocs.org/sdr/CALA0000279.md): Stop · worn · Mar 8, 2000 · N17812 · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND TWO AFT CARGO DOOR STOPS WORN. THE AREAS WERE REPAIRED IAW SRM 52-03, FIGURE 8, 51-30-2, 52-30-7, 51-10-3, AND ECRA 5330-02819.
- [SDR CALA0000272](https://openairdocs.org/sdr/CALA0000272.md): Stop · gouged · Mar 6, 2000 · N17812 · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND MID CARGO DOOR STOP GOUGED.. THE DOOR STOP WAS REPAIRED IAW ECRA 5330-02819.
- [SDR CALA0000271](https://openairdocs.org/sdr/CALA0000271.md): Angle · cracked · Mar 6, 2000 · N17812 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FILLET PANEL SUPPORT ANGLE CRACKED AT STA 945, LONGERON 30. THE SUPPORT ANGLE WAS REMOVED AND A NEW SUPPORT ANGLE WAS INSTALLED IAW SRM 51-10-04, 51-10-3, AND 51-30-1.
- [SDR CALA0000258](https://openairdocs.org/sdr/CALA0000258.md): Stop · gouged · Mar 3, 2000 · N17812 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FORWARD CARGO DOOR STOP GOUGED. THE DOOR STOP WAS REPAIRED IAW ECRA 5330-02819.
- [SDR CALA0000257](https://openairdocs.org/sdr/CALA0000257.md): Flange · corroded · Mar 3, 2000 · N17812 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND ANTENNA FLANGE CORRODED IN MID PIT AT STA 600, LONGERON 29L TO 30. THE ANTENNA FLANGE WAS REMOVED AND A NEW FLANGE AND DOUBLER WERE INSTALLED IAW SRM 51-10-3, 51-10-4, 51-30-2, AND 51-30-5.
- [SDR CALA0000256](https://openairdocs.org/sdr/CALA0000256.md): Floorbeam · corroded · Mar 3, 2000 · N17812 · Doug DC982 · Fuselage Main, Floor Beam
  > INSPECTION FOUND L-1 DOOR THRESHOLD LOWER SUB FLOOR WEB CORRODED AND ATTACH ANGLE CRACKED. THE SUB FLOOR WEB WAS REMOVED IAW SRM 51-30-2. A NEW SUB FLOOR WEB WAS INSTALLED IAW SRM 53-14-1, FIGURE 1 AND 53-01, FIGURE 4. THE ATTACH ANGLE WAS REMOVED AND REPLA
- [SDR CALA0000255](https://openairdocs.org/sdr/CALA0000255.md): Web · corroded · Mar 3, 2000 · N17812 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND LEFT CUSP WEB ON FORWARD SIDE OF FRAME AT STA 237, LONGERON 18L CORRODED. THE CORRODED AREA WAS CUT OUT IAW SRM 53-01, FIGURE 4. A DOUBLER, PLATE, TEE ANGLE, AND BRACKET WERE INSTALLED IAW SRM 53-01, 53-10-2, 51-30-3, AND 51-30-2.
- [SDR CALA0000254](https://openairdocs.org/sdr/CALA0000254.md): Web · cracked · Mar 3, 2000 · N17812 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 3 INCH CRACK IN MAIN ENRTY DOOR AFT TORQUE BOX UPPER WEB TENSION LEG AT FS 208, LONGERON 11L. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-30-1 AND 51-30-2.
- [SDR CALA0000253](https://openairdocs.org/sdr/CALA0000253.md): Seat Track · corroded · Mar 3, 2000 · N17812 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND LEFT O/B SEAT TRACK CORRODED AT FS 1174-1300. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-1.
- [SDR CALA0000252](https://openairdocs.org/sdr/CALA0000252.md): Intercostal · cracked · Mar 3, 2000 · N17812 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 1.5 INCH CRACK IN FORWARD CARGO INTERCOSTAL AFT SUPPORT ANGLE AT STA 237 BETWEEN LONGERON 27R AND 28R. THE SUPPORT ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-5.
- [SDR CALA0000251](https://openairdocs.org/sdr/CALA0000251.md): Skin · dented · Mar 3, 2000 · N17812 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED BETWEEN FS 465 AND 484 AT LONGERON 21R AND 22R. THE DENT WAS COLD WORKED IAW SRM 53-04, FIGURE 8, CONDITION 2. AN INTERNAL DOUBLER WAS INSTALLED IAW SRM 51-10-04, 51-10-3, 51-30-02, AND 53-04, FIGURE 38, VIEW P.
- [SDR CALA0000250](https://openairdocs.org/sdr/CALA0000250.md): Seat Track · corroded · Mar 3, 2000 · N17812 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND LEFT I/B SET TRACK CORRODED AT FS 1030-1300. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-05, FIGURE 5F.
- [SDR CALA0000249](https://openairdocs.org/sdr/CALA0000249.md): Floorbeam · cracked · Mar 3, 2000 · N17812 · Doug DC982 · Fuselage Main, Floor Beam
  > INSPECTION FOUND A 3 INCH CRACK IN R-1 DOOR THRESHOLD FLOOR SUPPORT WEB AT FORWARD EDGE OF DOOR CUTOUT. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 2, 51-10-3, 51-30-2, AND 51-30-6.
- [SDR CALA0000248](https://openairdocs.org/sdr/CALA0000248.md): Angle · cracked · Mar 3, 2000 · N17812 · Doug DC982 · Rudder Structure
  > INSPECTION FOUND A 1 INCH CRACK IN LOWER RUDDER FAIRING AT STIFFENER ANGLE. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-4.
- [SDR CALA0000247](https://openairdocs.org/sdr/CALA0000247.md): Angle · cracked · Mar 3, 2000 · N17812 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 1 INCH CRACK IN LONGERON 30 FILLET PANEL SUPPORT ANGLE AT STA 970. THE SUPPORT ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-4.
- [SDR CALA0000246](https://openairdocs.org/sdr/CALA0000246.md): Seat Track · corroded · Mar 3, 2000 · N17812 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND LEFT CENTER SEAT TRACK CORRODED AT FS 1030-1100, LBL 22. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-1.
- [SDR CALA0000245](https://openairdocs.org/sdr/CALA0000245.md): Stop · worn · Mar 3, 2000 · N17812 · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND FORWARD CARGO DOOR STOP WORN. REPAIRED IAW ECRA 5330-02819.

Next page: https://openairdocs.org/deregistered/N17812-2004-04-01/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 = 'N17812' AND deregistration_id = 'N17812-2004-04-01'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N17812-2004-04-01/reports

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