# Service difficulty reports: N72825, cancelled Jul 14, 2005

A list on [N72825, cancelled Jul 14, 2005](https://openairdocs.org/deregistered/N72825-2005-07-14.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 · 82 reports

- [SDR CALA0400482](https://openairdocs.org/sdr/CALA0400482.md): Fitting · corroded · May 8, 2004 · N72825 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FITTING AT AFT LOWER CORNER OF AFT BAGGAGE BIN DOOR CUTOUT CORRODED. A NEW FITTING WAS INSTALLED IAW SRM 51-30-5.
- [SDR CALA0400165](https://openairdocs.org/sdr/CALA0400165.md): Wire · shorted · Feb 24, 2004 · N72825 · Doug DC982 · Flight Control System Wiring
  > MACH TRIM INOP LIGHT ILLUMINATED AND AIRCRAFT BEGAN TO DUTCH ROLL AT 31,000 FEET EN ROUTE. QRH PROCEDURE COMPLETED, BUT NO CHANGE RESULTED. THERE WAS MINIMUM CONTROL WITH THE RUDDER. THE AIRCRAFT WAS DIVERTED TO BWI WHERE IT LANDED WITHOUT INCIDENT. MAINTE
- [SDR CALA0300021](https://openairdocs.org/sdr/CALA0300021.md): Longeron · cracked · Jan 30, 2003 · N72825 · Doug DC982 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND A 1/2" CRACK IN LONGERON 2R AT STA 1418. A SPLICE REPAIR WAS INSTALLED IAW ECRA 5311-01132.
- [SDR CALA0200485](https://openairdocs.org/sdr/CALA0200485.md): Fire Detector · malfunctioned · Oct 3, 2002 · N72825 · Doug DC982 · Fire Detection
  > THE MID CARGO DET "B" CARGO DETECTION AND SUPRESSION LIGHT ILLUMINATED WHILE AT CRUISE ENROUTE FROM IAH TO ORD. SHORTLY AFTERWARDS THE MASTER WARNING AND CARGO FIRE INDICATION AND FIRE HORN ACTIVATED. BOTH FIRE BOTTLES WERE DISCHARGED AND THE AIRCRAFT WAS DIVE
- [SDR CALA0200015](https://openairdocs.org/sdr/CALA0200015.md): Bracket · cracked · Jan 11, 2002 · N72825 · Doug DC982 · Vertical Stabilizer
  > INSPECTION FOUND A 1/2" CRACK IN VERTICAL STABILIZER R/H SIDE SUPPORT BRACKET FOR UPPER FAIRING ABOVE JACKSCREW. A DOUBLER WAS INSTALLED ON THE SUPPORT BRACKET IAW SRM 51-30-2.
- [SDR CALA0200007](https://openairdocs.org/sdr/CALA0200007.md): Hinge · corroded · Jan 9, 2002 · N72825 · Doug DC982 · Vertical Stabilizer
  > INSPECTION FOUND LEFT I/B AND O/B VERTICAL STABILIZER HINGE PLATES CORRODED ON MATING SURFACES. NEW HINGE PLATES WERE INSTALLED IAW EA 5530-01238.
- [SDR CALA0200006](https://openairdocs.org/sdr/CALA0200006.md): Hinge · corroded · Jan 9, 2002 · N72825 · Doug DC982 · Vertical Stabilizer
  > INSPECTION FOUND RIGHT I/B AND O/B VERTICAL STABILIZER HINGE PLATES CORRODED ON MATING SURFACES. NEW HINGE PLATES WERE INSTALLED IAW EA 5530-01238.
- [SDR CALA0100495](https://openairdocs.org/sdr/CALA0100495.md): Attach Angle · cracked · May 23, 2001 · N72825 · Doug DC982 · Fuselage, Stabilizer Attach Fittings
  > INSPECTION FOUND A 1.5 INCH CRACK IN RT VERTICAL STABILIZER LOWER ATTACH ANGLE, 6 INCHES FROM TRAILING EDGE. REPAIRED IAW SRM 53-05.
- [SDR CALA0100494](https://openairdocs.org/sdr/CALA0100494.md): Attach Angle · cracked · May 23, 2001 · N72825 · Doug DC982 · Fuselage, Stabilizer Attach Fittings
  > INSPECTION FOUND A 2 INCH CRACK IN LT VERTICAL STABILIZER LOWER ATTACH ANGLE, 7 INCHES FROM TRAILING EDGE. REPAIRED IAW SRM 53-05.
- [SDR CALA0001243](https://openairdocs.org/sdr/CALA0001243.md): Doubler · corroded · Aug 7, 2000 · N72825 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND AFT CARGO THRESHOLD EXTERNAL DOUBLER CORRODED AT FS 1160 - 1205, LONGERON 28R. THE DOUBLER WAS REMOVED AND A NEW DOUBLER WAS INSTALLED IAW SRM 51-30-1, 51-30-5, AND ECRA 5310-03027.
- [SDR CALA0001242](https://openairdocs.org/sdr/CALA0001242.md): Cargo Track · corroded · Aug 7, 2000 · N72825 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND CARGO TIE DOWN TRACK CORRODED AT FS 1212 - 1220, LONGERON 28R. THE TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-30-1, 51-10-2, AND 51-10-3.
- [SDR CALA0001241](https://openairdocs.org/sdr/CALA0001241.md): Strap · corroded · Aug 7, 2000 · N72825 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND AFT LOWER CORNER STRAP OF AFT CARGO DOOR FRAME CORRODED AT STA 1212, L28R. THE STRAP WAS REMOVED AND A NEW STRAP WAS INSTALLED IAW SRM 51-30-2, 51-30-5, 51-10-4, AND 51-30-4.
- [SDR CALA0001240](https://openairdocs.org/sdr/CALA0001240.md): Web · corroded · Aug 7, 2000 · N72825 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND AFT PIT TORQUE BOX UPPER WEB CORRODED UNDER CARGO TIE DOWN TRACK AT FS 1212 - 1218 ABOVE LONGERON 28R. THE WEB WAS REMOVED AND A NEW SECTION WAS SPLICED IN IAW ECRA 5310-04030, SRM 51-10-4, AND EA 9-5310-2-A0727.
- [SDR CALA0001239](https://openairdocs.org/sdr/CALA0001239.md): Web · cracked · Aug 7, 2000 · N72825 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A.5 INCH CRACK ON AFT SIDE OF UPPER WEB IN AFT PIT AT STA 1212, RT SIDE. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 2, 53-24-0, FIGURE 11, 51-30-2, AND 51-10-3.
- [SDR CALA0001238](https://openairdocs.org/sdr/CALA0001238.md): Longeron · corroded · Aug 7, 2000 · N72825 · Doug DC982 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND LONGERON 30 CORRODED AT STA 590 - 779. THE LONGERON WAS REMOVED AND REPLACED IAW SRM 51-30-5, 51-30-4, 51-30-2. THE EXISTING DOUBLER, WATER DRAIN, LONGERON SPLICES, FILLET, AND SKIN WERE REMOVED AND REINSTALLED IAW SRM 51-30-2, 51-30-1 AND 5
- [SDR CALA0001237](https://openairdocs.org/sdr/CALA0001237.md): Angle · cracked · Aug 7, 2000 · N72825 · Doug DC982 · Entrance Stairs
  > INSPECTION FOUND A 1 INCH CRACK IN LT THREAD SUPPORT ANGLE AT FIFTH STEP FROM BOTTOM OF VENTRAL STAIRS. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-5 AND 51-30-2. THE VENTRAL STAIRS RETRACTABLE STEPS WERE REMOVED FOR REPAIR AND REINSTALLED IAW MM 52-63-
- [SDR CALA0001228](https://openairdocs.org/sdr/CALA0001228.md): Web · cracked · Aug 6, 2000 · N72825 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND LT CUSP WEB CRACKED O/B OF SEAT TRACK AT STA 1174 - 1304, LBL 54. THE CUSP WEB WAS REMOVED AND REPLACED IAW SRM 51-30-1, 51-30-2, 51-30-5, AND 53-05, FIGURE 16.
- [SDR CALA0001227](https://openairdocs.org/sdr/CALA0001227.md): Seat Track · corroded · Aug 6, 2000 · N72825 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND LEFT O/B SEAT TRACK CORRODED AT STA 1174 - 1309. THE SEAT TRACK AND FITTING WERE REMOVED AND A NEW TRACK AND FITTING WERE INSTALLED IAW SRM 51-30-1, 51-30-2, 51-30-5, 51-10-3, AND 51-10-4.
- [SDR CALA0001226](https://openairdocs.org/sdr/CALA0001226.md): Pan · corroded · Aug 6, 2000 · N72825 · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND CORROSION AROUND FASTENERS OF FORWARD CARGO DOOR LOWER JAMB PAN. THE CORRODED AREA WAS CUT OUT AND A NEW PAN AND SPLICES WERE INSTALLED IAW SRM 53-05, FIGURE 44.
- [SDR CALA0001225](https://openairdocs.org/sdr/CALA0001225.md): Pan · cracked · Aug 6, 2000 · N72825 · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND THREE RIVET NUTS CRACKED AT FORWARD CARGO DOOR PAN FORWARD LOWER CORNER. THE CRACKS WERE 0.05 INCH LONG. THE CARGO DOOR PAN SECTION WAS REMOVED AND A NEW CARGO DOOR PAN SECTION WAS INSTALLED IAW SRM 51-30-2 AND 52-05, FIGURE 44.
- [SDR CALA0001224](https://openairdocs.org/sdr/CALA0001224.md): Cargo Track · corroded · Aug 6, 2000 · N72825 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND RT CARGO TIE DOWN TRACK CORRODED AT STA 522 - 636, L28R. THE TIE DOWN TRACK WAS REMOVED AND A NEW TIE DOWN TRACK WAS INSTALLED IAW SRM 51-30-2, 51-30-5, AND 51-10-4.
- [SDR CALA0001223](https://openairdocs.org/sdr/CALA0001223.md): Angle · corroded · Aug 6, 2000 · N72825 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND RT FLOOR PANEL TRANSITION ANGLE CORRODED AT FS 598 - 636. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-10-4, 51-10-3, AND 51-30-1.
- [SDR CALA0001222](https://openairdocs.org/sdr/CALA0001222.md): Cargo Track · corroded · Aug 6, 2000 · N72825 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND RT CARGO TRACK CORRODED ON UPPER AND LOWER SURFACES IN FORWARD CARGO PIT AT FS 427 - 522. THE CARGO TRACK WAS REPLACED IAW SRM 51-30-2 AND 53-05-4.
- [SDR CALA0001221](https://openairdocs.org/sdr/CALA0001221.md): Skin · dented · Aug 6, 2000 · N72825 · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND FORWARD SKIN OF AFT CARGO DOOR DENTED. THE DENTED AREA WAS CUT OUT IAW SRM 52-05, FIGURE 3. A DOUBLER, FILLER, AND SHIMS WERE INSTALLED IAW SRM 52-05, FIGURE 3 AND 51-10-3.
- [SDR CALA0001220](https://openairdocs.org/sdr/CALA0001220.md): Stop · gouged · Aug 6, 2000 · N72825 · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND AFT CARGO DOOR STOPS GOUGED. REPAIRED IAW ECRA 5330-02819.
- [SDR CALA0001219](https://openairdocs.org/sdr/CALA0001219.md): Cargo Track · corroded · Aug 6, 2000 · N72825 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND FORWARD CARGO PIT LT CARGO TRACK CORRODED ON UPPER AND LOWER SURFACES OF CLIP NUT FLANGES AT FS 370 - 522. THE CARGO TRACK WAS REMOVED AND A NEW CARGO TRACK WAS INSTALLED IAW SRM 51-10-4 AND 53-05, FIGURE 4G.
- [SDR CALA0001218](https://openairdocs.org/sdr/CALA0001218.md): Floor Panel · corroded · Aug 6, 2000 · N72825 · Doug DC982 · Fuselage Floor Panel
  > INSPECTION FOUND AFT PIT FLOOR PANEL CORRODED AT FS 1212 - 1230. THE FLOOR PANEL WAS REMOVED AND A NEW FLOOR PANEL WAS INSTALLED IAW SRM 53-20, FIGURE 11, 51-10-3, 51-10-4, AND ECRA 5320-01265.
- [SDR CALA0001217](https://openairdocs.org/sdr/CALA0001217.md): Intercostal · corroded · Aug 6, 2000 · N72825 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND RT INTERCOSTAL CORRODED AT FS 1292 - 1309. THE INTERCOSTAL WAS REMOVED AND A NEW INTERCOSTAL WAS INSTALLED IAW SRM 51-50-2, 51-10-4, 51-30-2, AND 51-30-5.
- [SDR CALA0001216](https://openairdocs.org/sdr/CALA0001216.md): Fairing · chafed · Aug 6, 2000 · N72825 · Doug DC982 · Horizontal Stabilizer Structure
  > INSPECTION FOUND UPPER RT HORIZONTAL STABILIZER FAIRING CRACKED AT FORWARD UPPER END AND CHAFING IN THREE AREAS AT FORWARD UPPER END AND DELAMINATION NEAR CENTER OF UPPER EDGE OF FAIRING. THE ANGLE WAS REMOVED AND A REPAIR ANGLE, DOUBLER, AND FILLER WERE INST
- [SDR CALA0001215](https://openairdocs.org/sdr/CALA0001215.md): Web · cracked · Aug 6, 2000 · N72825 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A.75 INCH CRACK IN TAIL COMPARTMENT FORWARD SIDE OF STA 1485 WEB LT SIDE SKIN. REMOVED WEB IAW SRM 51-30-2 AND STOP DRILLED CRACK IAW SRM 55-01, FIGURE 2. A NEW DOUBLER WAS INSTALLED IAW SRM 55-01, FIGURE 4, 51-10-4, 51-10-3, AND 51-30.
- [SDR CALA0001213](https://openairdocs.org/sdr/CALA0001213.md): Skin · dented · Aug 6, 2000 · N72825 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND LT AFT FUSELAGE SKIN DENTED AT FS 1497. A NEW SKIN PATCH WAS INSTALLED IAW SRM 53-01, FIGURE 2, 53-34, FIGURE 5, AND 51-60-0.
- [SDR CALA0001212](https://openairdocs.org/sdr/CALA0001212.md): Structure · gouged · Aug 6, 2000 · N72825 · Doug DC982 · Horizontal Stabilizer Structure
  > INSPECTION FOUND LT HORIZONTAL STABILIZER FORWARD UPPER AND LOWER BARREL NUT HOLES GOUGED. REAMED BARREL NUT HOLES AND INSTALLED BUSHINGS IAW EA 9-5511-2-A0738 AND ECRA 5511-01029.
- [SDR CALA0001211](https://openairdocs.org/sdr/CALA0001211.md): Door Frame · bent · Aug 6, 2000 · N72825 · Doug DC982 · Fuselage Main, Structure
  > INSPECTION FOUND LOOSE AND PULLED RIVETS IN FUSELAGE SKIN AND AFT NLG DOOR JAMB WAS BENT AND GOUGED AT STA 110. THE RIVETS WERE REMOVED AND REPLACED IAW SRM 51-30-2. THE AFT DOOR JAMB WAS REMOVED AND A NEW DOOR JAMB WAS INSTALLED IAW SRM 51-30-2, 51-10-4, 51
- [SDR CALA0001210](https://openairdocs.org/sdr/CALA0001210.md): Flange · cracked · Aug 6, 2000 · N72825 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 1 INCH CRACK IN AFT FUSELAGE AC SERVICING PANEL CUTOUT FLANGE. REMOVED AND REPLACED DOUBLER IAW SRM 53-34-0, FIGURE 4, SHEET 1.
- [SDR CALA0001198](https://openairdocs.org/sdr/CALA0001198.md): Web · cracked · Aug 2, 2000 · N72825 · Doug DC982 · Vertical Stabilizer
  > INSPECTION FOUND A.25 INCH CRACK IN WEB SKIN AT RT SIDE OF TAIL COMPARTMENT STA 1485, JUST FORWARD OF RUDDER TRIM. THE WEB AND ANGLE WERE REMOVED AND THE CRACKED AREA WAS REMOVED IAW SRM 51-30-2 AND 55-01, FIGURE 4. DOUBLERS AND AN ANGLE WERE INSTALLED IAW
- [SDR CALA0001183](https://openairdocs.org/sdr/CALA0001183.md): Pan · cracked · Jul 28, 2000 · N72825 · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND AFT CARGO DOOR PAN CRACKED AT FORWARD UPPER CORNER AND AT APPROXIMATELY 12 INCHES FROM FORWARD UPPER CORNER. THE CRACKS WERE.25 INCH LONG. THE CRACKS WERE STOP DRILLED IAW SRM 52-03, FIGURE 8. A DOUBLER WAS INSTALLED AT EACH LOCATION IAW S
- [SDR CALA0001168](https://openairdocs.org/sdr/CALA0001168.md): Strap · corroded · Jul 26, 2000 · N72825 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND AFT PIT, AFT BULKHEAD, RIGHT SIDE RETAINER STRAP CORRODED AT FS 1338. A NEW RETAINER STRAP WAS INSTALLED IAW SRM 51-10-2, 53-24-0, FIGURE 11, AND 51-10-3.
- [SDR CALA0001167](https://openairdocs.org/sdr/CALA0001167.md): Seat Track · corroded · Jul 26, 2000 · N72825 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND RIGHT O/B SEAT TRACK CORRODED AT STA 807 - 1022, RBL 54. THE SEAT TRACK WAS REPLACED IAW SRM 53-05, FIGURE 4F, 51-30-1, 51-30-5, AND 51-60-0.
- [SDR CALA0001166](https://openairdocs.org/sdr/CALA0001166.md): Attach Angle · cracked · Jul 26, 2000 · N72825 · Doug DC982 · Passenger/Crew Doors
  > INSPECTION FOUND A 1.6 INCH CRACK IN L-1 DOOR LOWER FORWARD CORNER SEAL ATTACH ANGLE. THE ATTACH ANGLE WAS REMOVED AND A NEW ATTACH ANGLE WAS INSTALLED IAW SRM 51-30-7, 51-10-4, AND 51-10-3.
- [SDR CALA0001165](https://openairdocs.org/sdr/CALA0001165.md): Strap · corroded · Jul 26, 2000 · N72825 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND AFT CARGO BAY FRAME STRAP CORRODED AT STA 1231, LONGERON 28R-30. THE STRAP WAS REMOVED AND A NEW STRAP WAS INSTALLED IAW SRM 51-10-4, 51-10-3, AND 51-30-5.
- [SDR CALA0001164](https://openairdocs.org/sdr/CALA0001164.md): Doubler · chafed · Jul 26, 2000 · N72825 · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND AFT CARGO DOOR OUTER LOWER AFT DOUBLER CHAFED. THE DOUBLER WAS REMOVED AND REPLACED IAW SRM 51-30-2.
- [SDR CALA0001162](https://openairdocs.org/sdr/CALA0001162.md): Skin · gouged · Jul 25, 2000 · N72825 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND THE AFT FUSELAGE SKIN DENTED AND GOUGED AT STA 1320 BELOW NR 2 ENGINE PYLON, LONGERON 19R. THE GOUGE WAS BLENDED IAW SRM 53-01, FIGURE 1, SHEET 3. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38, SHEET 20.
- [SDR CALA0001160](https://openairdocs.org/sdr/CALA0001160.md): Floor Support · corroded · Jul 25, 2000 · N72825 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 1212, LONGERON 28L-29R. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2 AND 51-10-4.
- [SDR CALA0001159](https://openairdocs.org/sdr/CALA0001159.md): Channel · corroded · Jul 25, 2000 · N72825 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND RIGHT O/B FLOOR PANEL HAT CHANNEL CORRODED AT STA 826 - 907, RBL 54. THE HAT CHANNEL WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 53-21-00.
- [SDR CALA0001158](https://openairdocs.org/sdr/CALA0001158.md): Seat Track · corroded · Jul 25, 2000 · N72825 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND LEFT O/B SEAT TRACK CORRODED AT STA 796 - 946, LBL 54. THE SEAT TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-10-4, 53-05, FIGURE 4F, 51-30-2, 51-30-1, AND 51-10-3.
- [SDR CALA0001157](https://openairdocs.org/sdr/CALA0001157.md): Seat Track · corroded · Jul 25, 2000 · N72825 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND LT SIDE CENTER SEAT TRACK CORRODED AT FS 1031 - 1241, LBL 24. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-30-1, 51-10-4, 51-10-3, AND 53-05, FIGURE 4F.
- [SDR CALA0001156](https://openairdocs.org/sdr/CALA0001156.md): Pan · cracked · Jul 25, 2000 · N72825 · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND A 1.2 INCH CRACK IN MID CARGO DOOR AFT PAN FLANGE ADJACENT TO TORQUE TUBE CAM. THE CRACK WAS STOP DRILLED IAW SRM 52-03, FIGURE 1. THE EXISTING REPAIR DOUBLER WAS REMOVED FOR ACCESS. A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 26A
- [SDR CALA0001155](https://openairdocs.org/sdr/CALA0001155.md): Angle · gouged · Jul 25, 2000 · N72825 · Doug DC982 · Passenger/Crew Doors
  > INSPECTION FOUND L-1 DOOR UPPER AFT LINER ATTACH ANGLE GOUGED. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-5.
- [SDR CALA0001154](https://openairdocs.org/sdr/CALA0001154.md): Cargo Track · corroded · Jul 25, 2000 · N72825 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND LT CARGO TIE DOWN TRACK CORRODED AT STA 522 - 788, LONGERON 27L. THE CORROSION WAS REMOVED AND FOUND WITHIN LIMITS AT STA 522 - 655 AND STA 684 - 788. THESE SECTIONS WERE ALODINED AND PRIMED IAW SRM 51-10-3 AND 53-01. THE SECTION FROM STA 6
- [SDR CALA0001151](https://openairdocs.org/sdr/CALA0001151.md): Floor Support · corroded · Jul 24, 2000 · N72825 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 1155 - 1221, LONGERON 29R. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-30-5.

Next page: https://openairdocs.org/deregistered/N72825-2005-07-14/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 = 'N72825' AND deregistration_id = 'N72825-2005-07-14'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N72825-2005-07-14/reports

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