# Service difficulty reports: N72822, cancelled Sep 26, 2005

A list on [N72822, cancelled Sep 26, 2005](https://openairdocs.org/deregistered/N72822-2005-09-26.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 · 55 reports

- [SDR CALA0400556](https://openairdocs.org/sdr/CALA0400556.md): Battery · inoperative · Jun 29, 2004 · N72822 · Doug DC982 · Emergency Lighting
  > THE CABIN OVERHEAD EMERGENCY LIGHTS WOULD NOT ILLUMINATE BETWEEN ROWS 10-18. THE POWER PACK BATTERIES AT STA 500 WERE REMOVED AND REPLACED IAW MM 33-53-00.
- [SDR CALA0400527](https://openairdocs.org/sdr/CALA0400527.md): Battery · inoperative · Jun 9, 2004 · N72822 · Doug DC982 · Emergency Lighting
  > INSPECTION FOUND THE FLIGHT DECK AND FORWARD CEILING EMERGENCY LIGHT INOPERATIVE. THE EMERGENCY LIGHT BATTERIES IN FORWARD CEILING WERE REPLACED AND OPERATIONAL CHECKS WERE GOOD.
- [SDR CALA0400353](https://openairdocs.org/sdr/CALA0400353.md): Skin · cracked · Apr 10, 2004 · N72822 · Doug DC982 · Wing, Plate/Skin
  > INSPECTION FOUND A 1.5 INCH CRACK IN LEFT WING SKIN JUST FORWARD OF PANEL 1196C UPPER LEFT WING AREA, STA XOS 286. REPAIRED IAW ECRA 5720-01946.
- [SDR CALA0400338](https://openairdocs.org/sdr/CALA0400338.md): Skin · cracked · Apr 7, 2004 · N72822 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND EXTERIOR FUSELAGE SKIN BULGED WITH RIVETS POPPING AROUND LOWER TCAS ANTENNA AND A 2 INCH CRACK WAS FOUND IN SKIN FORWARD OF TCAS ANTENNA AT STA 237. A REPAIR WAS INSTALLED IAW SRM 53-04, FIGURE 12C.
- [SDR CALA0400326](https://openairdocs.org/sdr/CALA0400326.md): Beltframe · corroded · Apr 6, 2004 · N72822 · Doug DC982 · Fuselage Main, Frame
  > INSPECTION FOUND BELTFRAME UNDER TIEDOWN RAIL CORRODED AT STA 1231 BETWEEN STRINGER 27L AND 28L IN AFT BAGGAGE BIN. THE CORRODED AREA OF BELTFRAME WAS CUT OUT AND REPAIR PARTS WERE INSTALLED IAW SRM 53-03, FIGURE 5.
- [SDR CALA0400319](https://openairdocs.org/sdr/CALA0400319.md): Floor Support · corroded · Apr 4, 2004 · N72822 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT CORRODED IN MID BAG BIN AT STA 788, LBL 24. REPAIRED FLOOR SUPPORT IAW SRM 51-70-5.
- [SDR CALA0300062](https://openairdocs.org/sdr/CALA0300062.md): Cargo Track · corroded · Feb 21, 2003 · N72822 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND RT TIEDOWN RAIL CORRODED AT STA 522 - 636. A NEW TIEDOWN RAIL WAS INSTALLED IAW ECRA 5321-01134.
- [SDR CALA0300061](https://openairdocs.org/sdr/CALA0300061.md): Cable · frayed · Feb 21, 2003 · N72822 · Doug DC982 · Aerodynamic Fairings
  > THE TAILCONE FAILED TO SEPARATE FROM AIRCRAFT WHEN USING AFT ENTRANCE DOOR TO DEPLOY TAILCONE. FOUND L/H TAILCONE RELEASE CABLE FRAYED IN TWO PLACES WHERE IT PASSES OVER UPPER PULLEY. REPLACED CABLE AND PERFORMED ADJUSTMENT TEST OF TAILCONE SYSTEM IAW MM 53-53
- [SDR CALA0300046](https://openairdocs.org/sdr/CALA0300046.md): Frame · cracked · Feb 13, 2003 · N72822 · Doug DC982 · Fuselage Main, Frame
  > INSPECTION FOUND A 1" CRACK IN FUSELAGE FRAME AT STA 1418, LONGERON 1L. REPAIRED IAW SRM 53-03, PAGE 5.
- [SDR CALA0300036](https://openairdocs.org/sdr/CALA0300036.md): Pan · cracked · Feb 11, 2003 · N72822 · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND A 1.5 INCH CRACK IN FORWARD BAGGAGE BIN BACK PAN AT AFT SIDE WALL JUST AT LOWER LATCH BETWEEN THE TWO LOWER STOP PADS. A DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 26A.
- [SDR CALA0300027](https://openairdocs.org/sdr/CALA0300027.md): Longeron · cracked · Feb 9, 2003 · N72822 · Doug DC982 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND A 2" CRACK IN LONGERON 2R AFT OF STA 1418. A SPLICE REPAIR WAS INSTALLED IAW ECRA 5311-01132.
- [SDR CALA0200299](https://openairdocs.org/sdr/CALA0200299.md): Longeron · corroded · May 19, 2002 · N72822 · Doug DC982 · Fuselage Main, Longeron/Stringer
  > LONGERON 28R AT STATION 351 CORRODED. CUT OT DAMGED SECTION. SPLICED IN NEW SECTION PER SRM 53-02.
- [SDR CALA0100261](https://openairdocs.org/sdr/CALA0100261.md): Skin · damaged · Mar 29, 2001 · N72822 · Doug DC982 · Leading Edge Devices
  > INSPECTION FOUND RT NR 3 SLAT LEADING EDGE SKIN CREASED. THE INNER SKIN WAS REMOVED IAW SRM 51-30-8. THE SLAT SKIN WAS REPAIRED IAW ECRA 5754-01039. REINSTALLED INNER SKIN IAW SRM 51-30-8. REINSTALLED ANTI-ICE DUCT IAW MM 30-10-00. LEAK AND OPERATIONAL CH
- [SDR CALA0100259](https://openairdocs.org/sdr/CALA0100259.md): Beam · corroded · Mar 28, 2001 · N72822 · Doug DC982 · Fuselage Main, Structure
  > INSPECTION FOUND AFT CARGO PIT DOOR JAMB BEAM CORRODED. A NEW BEAM WAS INSTALLED IAW SRM 51-30-4 AND 51-30-5. TWO DOOR STOP BRACKETS AND 3 SCUFF PLATE STRAPS WERE INSTALLED IAW SRM 51-30-5 AND 51-30-2.
- [SDR CALA0100258](https://openairdocs.org/sdr/CALA0100258.md): Skin · dented · Mar 27, 2001 · N72822 · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND FORWARD CARGO DOOR DENTED ON OUTER SKIN. THE CARGO DOOR WAS REMOVED IAW MM 52-31-00. THE DOOR WAS REPAIRED IAW SRM 53-04, FIGURE 38 AND 51-10-3. THE DOOR WAS REINSTALLED IAW MM 52-31-00.
- [SDR CALA0100257](https://openairdocs.org/sdr/CALA0100257.md): Web · cracked · Mar 27, 2001 · N72822 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 6 INCH CRACK IN MAIN CABIN DOOR TORQUE BOX WEB TANG AT FS 200, LBL 54. THE TORQUE BOX WEB TANG WAS REPAIRED IAW EA 9-5314-2-A0880 AND ECRA 5310-04121.
- [SDR CALA0100255](https://openairdocs.org/sdr/CALA0100255.md): Skin · dented · Mar 27, 2001 · N72822 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AT FS 200-220 BETWEEN LONGERON 18 L AND 19L. THE DENTED AREA WAS CUT OUT IAW SRM 53-04, FIGURE 25. A REPAIR DOUBLER AND FILLER WERE INSTALLED IAW SRM 53-01, FIGURE 25, 51-10-3, AND 53-04, FIGURE 25. REINSTALLED
- [SDR CALA0100254](https://openairdocs.org/sdr/CALA0100254.md): Floor Panel · corroded · Mar 27, 2001 · N72822 · Doug DC982 · Fuselage Floor Panel
  > INSPECTION FOUND MAIN CABIN FLOOR PANEL CORRODED AT STA 256-313, LBL 22-44. THE PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLED IAW ECRA 5320-01265 AND SRM 51-30-1.
- [SDR CALA0100251](https://openairdocs.org/sdr/CALA0100251.md): Skin · gouged · Mar 24, 2001 · N72822 · Doug DC982 · Trailing Edge Flaps
  > INSPECTION FOUND RIGHT T/E INBOARD FLAP LOWER SKIN AFT OF MLG PITTED AND GOUGED. THE INBOARD T/E FLAP WAS REMOVED IAW MM 27-50-00. THE INBOARD T/E FLAP WEDGE WAS RESKINNED IAW SRM 51-10-4, 51-30-2, AND 57-50-9. THE INBOARD T/E FLAP WEDGE WAS REINSTALLED IAW
- [SDR CALA0100250](https://openairdocs.org/sdr/CALA0100250.md): Angle · cracked · Mar 24, 2001 · N72822 · Doug DC982 · Fuselage, Stabilizer Attach Fittings
  > INSPECTION FOUND A CRACK IN AFT FUSELAGE TO VERTICAL STABILIZER ANGLE AT AFT END LT SIDE. THE CRACKED AREA WAS REMOVED IAW SRM 53-05, FIGURE 23. DOUBLER AND FILLER WERE INSTALLED IAW SRM 53-05, FIGURE 23, 51-10-3, 51-20-0, AND 51-30-5.
- [SDR CALA0100249](https://openairdocs.org/sdr/CALA0100249.md): Angle · cracked · Mar 24, 2001 · N72822 · Doug DC982 · Fuselage, Stabilizer Attach Fittings
  > INSPECTION FOUND A CRACK IN AFT FUSELAGE TO VERTICAL STABILIZER ANGLE AT AFT END RT SIDE. THE CRACKED AREA WAS REMOVED IAW SRM 53-05, FIGURE 23. DOUBLER AND FILLER WERE INSTALLED IAW SRM 51-10-3, 53-05, FIGURE 23, AND 51-20-0.
- [SDR CALA0100248](https://openairdocs.org/sdr/CALA0100248.md): Frame · cracked · Mar 23, 2001 · N72822 · Doug DC982 · Fuselage Main, Frame
  > INSPECTION FOUND A 1 INCH CRACK IN LEFT W/W LOWER FORWARD FRAME I/B NEXT TO KEEL BEAM. REPAIR DOUBLERS WERE INSTALLED IAW 53-01, FIGURE 2, 51-10-4, 51-10-3, AND 51-30-2.
- [SDR CALA0100247](https://openairdocs.org/sdr/CALA0100247.md): Frame · cracked · Mar 23, 2001 · N72822 · Doug DC982 · Fuselage Main, Frame
  > INSPECTION FOUND A 1 INCH CRACK IN RIGHT W/W FORWARD FRAME AT I/B LEADING EDGE NEXT TO KEEL BEAM. REPAIR DOUBLERS WERE INSTALLED IAW SRM 53-01, FIGURE 2, 51-10-4, 51-10-3, AND 51-30-2.
- [SDR CALA0100246](https://openairdocs.org/sdr/CALA0100246.md): Beam · corroded · Mar 23, 2001 · N72822 · Doug DC982 · Fuselage Main, Structure
  > INSPECTION FOUND MID CARGO DOOR JAMB BEAM CORRODED. THE CORROSION WAS REMOVED. A DOUBLER WAS INSTALLED IAW ECRA 5310-03027.
- [SDR CALA0100243](https://openairdocs.org/sdr/CALA0100243.md): Skin · dented · Mar 22, 2001 · N72822 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AT FS 463 BETWEEN LONGERON 16R AND 17R. A DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38, VIEW E, 51-10-3, AND 51-30-2.
- [SDR CALA0100242](https://openairdocs.org/sdr/CALA0100242.md): Web · corroded · Mar 22, 2001 · N72822 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND E&E BAY OVERHEAD FLOOR WEB PANEL HAD CORROSION BLEEDING OUT FROM THE FLOORBEAM AND LOWER SURFACE OF WEB PANEL AT STA 200, RBL 10. THE FLOOR PANEL WAS REMOVED FOR ACCESS AND THE CORROSION WAS REMOVED IAW SRM 51-10-3. THE CORROSION WAS FOUND O
- [SDR CALA0100241](https://openairdocs.org/sdr/CALA0100241.md): Skin · dented · Mar 22, 2001 · N72822 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AT FS 200 - 220 BETWEEN LONGERON 17L AND 18L. THE SKIN WAS REPAIRED IAW ECRA 5330-02471.
- [SDR CALA0100239](https://openairdocs.org/sdr/CALA0100239.md): Skin · dented · Mar 20, 2001 · N72822 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND LT AFT FUSELAGE LOWER SKIN DENTED BELOW OUTFLOW VALVE. THE AREA WAS REFORMED IAW SRM 53-04, FIGURE 38. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38, 51-10-4, 51-10-3, AND 51-30-2.
- [SDR CALA0100234](https://openairdocs.org/sdr/CALA0100234.md): Skin · dented · Mar 17, 2001 · N72822 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AT FS 200 - 220 BETWEEN LONGERON 16R AND 18R. A REPAIR DOUBLER WAS INSTALLED.
- [SDR CALA0000903](https://openairdocs.org/sdr/CALA0000903.md): Proximity Switch · out of rig · Jun 18, 2000 · N72822 · Doug DC982 · Landing Gear Position and Warning
  > THE RED NOSE GEAR LIGHT REMAINED ILLUMINATED WHEN GEAR WAS RETRACTED AFTER TAKEOFF. THE GEAR WAS CYCLED, BUT THE LIGHT REMAINED ILLUMINATED. THE AIRCRAFT WAS RETURNED TO DEN WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NOSE GEAR UPLOCK PROXIMITY
- [SDR CALA9900070](https://openairdocs.org/sdr/CALA9900070.md): Handle · out of adjust · Jan 23, 1999 · N72822 · Doug DC982 · Aerodynamic Fairings
  > THE TAIL CONE EXTERIOR RELEASE HANDLE FAILED PULL TEST. THE HANDLE FAILED LOW AT 18 POUNDS. THE TAIL CONE EXTERIOR RELEASE HANDLE WAS RIGGED AND FELL WITHIN TEST LIMITS IAW MM 53-53-00.
- [SDR CALA9900069](https://openairdocs.org/sdr/CALA9900069.md): Skin · dented · Jan 22, 1999 · N72822 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 260, LONGERON 19R. REPAIRED IAW SRM 53-04, FIGURE 38.
- [SDR CALA9900033](https://openairdocs.org/sdr/CALA9900033.md): Skin · dented · Jan 20, 1999 · N72822 · Doug DC982 · Fuselage Main, Plate/Skin
  > DENT AT STA 294 LEFT BETWEEN LONG 22 AND 23. COLD FORMED DENT BACK TO CONTOUR. FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 53-04.
- [SDR CALA9900032](https://openairdocs.org/sdr/CALA9900032.md): Beam · cracked · Jan 20, 1999 · N72822 · Doug DC982 · Service Doors
  > FORWARD SERVICE DOOR NUMBER 4 BEAM CRACKED AT AFT SIDE RADIUS 3/4. INSTALLED NEW BEAM PER SRM 51-30.
- [SDR CALA9900031](https://openairdocs.org/sdr/CALA9900031.md): Skin · lightning strike · Jan 19, 1999 · N72822 · Doug DC982 · Fuselage Main, Plate/Skin
  > SEVERAL SMALL LIGHTNING STRIKES, LONG 24 TO 26 LT STA 218 TO 313. BLENDED OUT LIGHTNING STRIKE DAMAGE OR PLUGGED AS NECESSARY PER SRM 53-04 FIG 38.
- [SDR CALA9900029](https://openairdocs.org/sdr/CALA9900029.md): Skin · dented · Jan 19, 1999 · N72822 · Doug DC982 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN AT STA 237 HAS A DEEP DENT. INSTALLED NEW SECTION OF SKIN PER EC/RA 5330-02445.
- [SDR CALA9900028](https://openairdocs.org/sdr/CALA9900028.md): Seat Track · corroded · Jan 19, 1999 · N72822 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON FLOOR BOARD SUPPORT FLANGE LEFT CENTER SEAT TRACK, SEVERAL AREAS STA 1136 TO 1231. REMOVED AND REPLACED SEAT TRACK PER SRM 51-30-0 FROM STA 1032 TO 1245.
- [SDR CALA9900026](https://openairdocs.org/sdr/CALA9900026.md): Skin · damaged · Jan 19, 1999 · N72822 · Doug DC982 · Fuselage Main, Plate/Skin
  > SMALL CUTOUT FOR MAIN CABIN DOOR HOLD OPEN HOOK FUSELAGE SKIN PULLED AWAY, 2 X 1 X.125. INSTALLED DOUBLERS PER SRM 53-04.
- [SDR CALA9900066](https://openairdocs.org/sdr/CALA9900066.md): Support · corroded · Jan 18, 1999 · N72822 · Doug DC982 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT CORRODED STA 190 APPROX BETWEEN PANEL K AND J FORWARD ENTRY, LIGHT CORROSION. FABRICATED FLOOR SUPPORT, PRIMED AND INSTALLED PER SRM 51-3-2.
- [SDR CALA9900060](https://openairdocs.org/sdr/CALA9900060.md): Bulkhead Doubler · corroded · Jan 15, 1999 · N72822 · Doug DC982 · Fuselage Main, Bulkhead
  > APB HAS CORROSION, BOTTOM AFT OF LONG 30. REMOVED AND REPLACED JACKPOST DOUBLER PER SRM 51-30-1 AND 51-30-2.
- [SDR CALA9900017](https://openairdocs.org/sdr/CALA9900017.md): Seat Track · cracked · Jan 14, 1999 · N72822 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION AND EXPOSED SEAT TRACK MATERIAL RT CENTER SEAT TRACK BETWEEN STA 218 - 229. REMOVED AND REPLACED SEAT TRACK AT STA 218 THROUGH STA 229 RT CENTER PER SRM 53-05.
- [SDR CALA9801698](https://openairdocs.org/sdr/CALA9801698.md): Duct · ruptured · Sep 10, 1998 · N72822 · Doug DC982 · Engine Anti-Icing System
  > THE RT FIRE DETECTOR LOOP LIGHT ILLUMINATED, FOLLOWED BY THE RT FIRE WARNING LIGHT AND BELL WHILE EN ROUTE FROM IAH TO CLE. THE RIGHT ENGINE POWER WAS REDUCED AND THE FIRE WARNINGS CEASED. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. M
- [SDR CALA9801369](https://openairdocs.org/sdr/CALA9801369.md): C-7 Blade · broken · Jul 29, 1998 · N72822 · Doug DC982 · Turbine Engine Compressor Section
  > THE TOWER REPORTED THAT THE NR 1 ENGINE HAD SPARKS COMING FROM EXHAUST AREA AFTER TAKEOFF. THE CREW REPORTED THAT THERE WERE NO UNUSUAL NR 1 ENGINE INSTRUMENT INDICATIONS AND OPERATION APPEARED NORMAL. THE ENGINE WAS NOT SHUTDOWN. THE AIRCRAFT WAS RETURNED
- [SDR CALA9701634](https://openairdocs.org/sdr/CALA9701634.md): Fma · burned · Nov 17, 1997 · N72822 · Doug DC982 · Flight Management Computing Hardware System
  > A PUFF OF SMOKE WAS SEEN COMING FROM BEHIND CAPTAIN'S FMA UPON LANDING AT IAH. THE FMA WENT BLANK AND THE SMOKE STOPPED. THE AIRCRAFT ARRIVED AT GATE WITHOUT INCIDENT. MAINTENANCE VERIFIED THAT THE FMA WAS BURNED. THE ASSOCIATED WIRING BEHIND CAPTAIN'S PAN
- [SDR CALA9700754](https://openairdocs.org/sdr/CALA9700754.md): Actuator · inoperative · May 20, 1997 · N72822 · Doug DC982 · Autopilot System
  > AUTOTHROTTLES DISENGAGED AND SPEED FLAGS CAME INTO VIEW ON BOTH F/D'S DURING T/O ROLL. A/C BEGAN TO OSCILLATE IN YAW DURING INITIAL CLIMB. THE YAW DAMP WAS TURNED OFF AND YAWING STOPPED. AUTOTHROTTLE AND AUTOPILOT WOULD NOT ENGAGE. THE C/B LABELLED DFGS SWI
- [SDR CALA9700610](https://openairdocs.org/sdr/CALA9700610.md): Oil Presure Tube · cracked · Apr 26, 1997 · N72822 · Doug DC982 · Engine Oil Pressure
  > CREW NOTICE NR 1 ENGINE OIL PRESSURE DECREASING SHUTDOWN NR 1 ENGINE. INSPECTION FOUND CRACK TUBE TO OIL PRESSURE SWITCH. REPLACED TUBE (P/N 793814-501) LEAKED CHECK AND RETURNED TO SERVICE.
- [SDR CALA9700312](https://openairdocs.org/sdr/CALA9700312.md): Slide · leaking · Mar 6, 1997 · N72822 · Doug DC982 · Escape Slide
  > THE LT AFT GALLEY SLIDE PACK BEGAN TO DEPRESSURIZE DURING ARMING OF SLIDE. THE SLIDE WAS REMOVED AND REPLACED IAW MM 25-60-0.
- [SDR CALA9700306](https://openairdocs.org/sdr/CALA9700306.md): Intercostal · cracked · Feb 21, 1997 · N72822 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A.75 AND.625 CRACK IN MID BAGGAGE BIN CEILING INTERCOSTAL AT STA 769-788. THE AREA WAS REPAIRED BY INSTALLING A DOUBLER IAW SRM 51-30-5.
- [SDR CALA9700305](https://openairdocs.org/sdr/CALA9700305.md): Support · corroded · Feb 21, 1997 · N72822 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 1155. A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-5.
- [SDR CALA9700308](https://openairdocs.org/sdr/CALA9700308.md): Angle · cracked · Feb 20, 1997 · N72822 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 1.3 CRACK IN LT SIDE VERTICAL FIN INNER ATTACH ANGLE. THE RT SIDE VERTICAL FIN INNER ATTACH ANGLE WAS FOUND BROKEN IN HALF. THE ATTACH ANGLES WERE REPLACED IAW SRM 51-30-5 AND 51-30-2.

Next page: https://openairdocs.org/deregistered/N72822-2005-09-26/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 = 'N72822' AND deregistration_id = 'N72822-2005-09-26'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N72822-2005-09-26/reports

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