# Service difficulty reports: N15820, cancelled Mar 21, 2013

A list on [N15820, cancelled Mar 21, 2013](https://openairdocs.org/deregistered/N15820-2013-03-21.md).

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

- [SDR CALA0300140](https://openairdocs.org/sdr/CALA0300140.md): Skin · cracked · Mar 23, 2003 · N15820 · Doug DC982 · Passenger/Crew Doors
  > INSPECTION FOUND A 1/2" CRACK IN L-1 DOOR SKIN AT AFT LOWER CORNER. A REPAIR WAS INSTALLED IAW SRM 52-05, PAGE 223.
- [SDR CALA0100862](https://openairdocs.org/sdr/CALA0100862.md): Skin Panel · dented · Sep 12, 2001 · N15820 · Doug DC982 · Trailing Edge Flaps
  > INSPECTION FOUND L/H I/B FLAP SKIN PANEL DENTED AFT OF MLG. A NEW SKIN PANEL WAS INSTALLED IAW SRM 51-30-1.
- [SDR CALA0100857](https://openairdocs.org/sdr/CALA0100857.md): Bracket · cracked · Sep 9, 2001 · N15820 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND ONE EACH 3/4" CRACK IN GUSSET ATTACH BRACKETS AT RIVET ATTACH ON L/H AND R/H SIDE OF NWW FWD WALL. A NEW STIFFENER WAS INSTALLED AT EACH LOCATION IAW SRM 53-14-1, FIGURE 4 AND 51-30-0.
- [SDR CALA0100856](https://openairdocs.org/sdr/CALA0100856.md): Web · cracked · Sep 9, 2001 · N15820 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 3/4" CRACK IN UPPER WEB IN TAIL COMPARTMENT ON L/H SIDE BY RUDDER SECTOR. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 53-01, PAGE 9.
- [SDR CALA0100855](https://openairdocs.org/sdr/CALA0100855.md): Web · cracked · Sep 9, 2001 · N15820 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 1.5 INCH CRACK IN VENT BOX WEB AT UPPER AFT CORNER AT STA 1485, RT SIDE. AN ANGLE BRACKET WAS INSTALLED IAW SRM 51-30-5.
- [SDR CALA0100848](https://openairdocs.org/sdr/CALA0100848.md): Beltframe · cracked · Sep 9, 2001 · N15820 · Doug DC982 · Fuselage Main, Frame
  > INSPECTION FOUND A 1" CRACK IN BELTFRAME AT STA 1418, LONGERON 2R. THE CRACK WAS STOP DRILLED AND A REPAIR WAS INSTALLED IAW DRAWING SRO9530003.
- [SDR CALA0100847](https://openairdocs.org/sdr/CALA0100847.md): Cargo Track · corroded · Sep 9, 2001 · N15820 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND LT TRACK TIE DOWN FLANGES IN AFT PIT CORRODED AT STA 1212. THE LT TRACK TIE DOWN FLANGES WERE REPAIRED IAW SRM 51-30-0.
- [SDR CALA0100846](https://openairdocs.org/sdr/CALA0100846.md): Angle · cracked · Sep 8, 2001 · N15820 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 1 INCH CRACK IN SUPPORT ANGLE ATTACHED TO AFT CROSSBEAM IN TAIL COMPARTMENT AT TORQUE TUBE, RT SIDE. THE SUPPORT ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-02.
- [SDR CALA0100845](https://openairdocs.org/sdr/CALA0100845.md): Strap · cracked · Sep 8, 2001 · N15820 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 6 INCH CRACK IN TAIL COMPARTMENT STRAP CAP AT STA 1446, LONGERONS 2R/2L. THE STRAP CAP WAS REMOVED AND REPLACED IAW SRM 51-30-2.
- [SDR CALA0100844](https://openairdocs.org/sdr/CALA0100844.md): Floor Support · corroded · Sep 7, 2001 · N15820 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND UPPER SURFACE OF CENTER FLOOR SUPPORT CORRODED AT STA 1287-1307. THE CENTER FLOOR SUPPORT WAS REPAIRED IAW SRM 53-01, FIGURE 2.
- [SDR CALA0100842](https://openairdocs.org/sdr/CALA0100842.md): Splice · cracked · Sep 7, 2001 · N15820 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A.75 INCH CRACK ON LONGERON SPLICE AT L28L BETWEEN STA 218 AND 229. THE LONGERON SPLICE WAS REMOVED AND A NEW SPLICE WAS INSTALLED IAW SRM 51-30-2 AND 51-30-5.
- [SDR CALA0100835](https://openairdocs.org/sdr/CALA0100835.md): Seat Track · corroded · Sep 6, 2001 · N15820 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND L/H O/B SEAT TRACK AT GALLEY MOUNT STA 1174 AND L/H CENTER SEAT TRACK AT GALLEY MOUNT STA 1193 CORRODED. THE SEAT TRACKS WERE REMOVED AND REPLACED IAW SRM 51-30-01.
- [SDR CALA9900437](https://openairdocs.org/sdr/CALA9900437.md): Pipe · dented · Apr 25, 1999 · N15820 · Doug DC982 · Aerodynamic Fairings
  > TAIL CONE RELEASE CABLE GUIDE TUBE LOWER RIGHT HAS SEVERAL DAMAGED AREAS, DENTS, AND SHARP CREASES. REMOVED AND REPLACED PIPE ASSY PER MM 53-50-00.
- [SDR CALA9900436](https://openairdocs.org/sdr/CALA9900436.md): Cable · frayed · Apr 25, 1999 · N15820 · Doug DC982 · Aerodynamic Fairings
  > UPPER LEFT TAILCONE RELEASE CABLE WORN AND FRAYED WHERE IT PASSES OVER UPPER PULLY. REMOVED AND REPLACED PULLY PER MM 53-53-00.
- [SDR CALA9900435](https://openairdocs.org/sdr/CALA9900435.md): Latch · worn · Apr 25, 1999 · N15820 · Doug DC982 · Aerodynamic Fairings
  > UPPER LEFT TAIL CONE LATCH HAS DEEP INDENTATIONS ON BOTH SIDES. REMOVED AND REPLACED LATCH. PERFORMED FUNCTIONAL TEST PER CARD 08-5350-1-0008.
- [SDR CALA9900434](https://openairdocs.org/sdr/CALA9900434.md): Latch · worn · Apr 25, 1999 · N15820 · Doug DC982 · Aerodynamic Fairings
  > UPPER RIGHT TAIL CONE LATCH HAS DEEP INDENTATIONS ON BOTH SIDES. REPLACED LATCH PIN, RIGGED CABLES PER MM 53-33-00 AND TESTED TAIL CONE PER CARD 08-5350-1-0008.
- [SDR CALA9900441](https://openairdocs.org/sdr/CALA9900441.md): Pan · cracked · Apr 23, 1999 · N15820 · Doug DC982 · Cargo/Baggage Doors
  > HI-SHEAR HOLE IS CRACKED (.25) IN FWD BAG BIN DOOR. FABRICATED AND INSTALLED STRAP PER EC/RA 5230-01462.
- [SDR CALA9900431](https://openairdocs.org/sdr/CALA9900431.md): Beam · cracked · Apr 22, 1999 · N15820 · Doug DC982 · Service Doors
  > INSPECTION FOUND A.5 INCH CRACK IN FORWARD END OF FORWARD SERVICE DOOR NR 4 BEAM. THE BEAM WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-30-5.
- [SDR CALA9900430](https://openairdocs.org/sdr/CALA9900430.md): Gusset · cracked · Apr 22, 1999 · N15820 · Doug DC982 · Service Doors
  > INSPECTION FOUND A.5 INCH CRACK IN GUSSET AT FORWARD END OF NR 1 BEAM ON FORWARD SERVICE DOOR. A NEW GUSSET WAS INSTALLED IAW SRM 51-30-5.
- [SDR CALA9900427](https://openairdocs.org/sdr/CALA9900427.md): Skin · cracked · Apr 20, 1999 · N15820 · Doug DC982 · Passenger/Crew Doors
  > INSPECTION FOUND A.5 INCH CRACK IN HOLD OPEN HOOK CUTOUT OF FORWARD ENTRY DOOR. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 20A.
- [SDR CALA9900426](https://openairdocs.org/sdr/CALA9900426.md): Beam · cracked · Apr 19, 1999 · N15820 · Doug DC982 · Passenger/Crew Doors
  > INSPECTION FOUND A.5 INCH CRACK AT FORWARD AND AFT ENDS OF MAIN CABIN DOOR NR 1 BEAM. A NEW BEAM WAS INSTALLED IAW SRM 51-30-2 AND 51-30-5.
- [SDR CALA9900425](https://openairdocs.org/sdr/CALA9900425.md): Jamb · corroded · Apr 19, 1999 · N15820 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND THE FORWARD CARGO DOOR JAMB LOWER PAN SECTION CORRODED. A REPAIR WAS INSTALLED IAW SRM 53-05, FIGURE 44.
- [SDR CALA9900422](https://openairdocs.org/sdr/CALA9900422.md): Seat Track · corroded · Apr 16, 1999 · N15820 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND RT INBOARD SEAT TRACK CORRODED AT STA 200-265. A NEW SECTION OF SEAT TRACK WAS INSTALLED IAW SRM 53-05.
- [SDR CALA9900421](https://openairdocs.org/sdr/CALA9900421.md): Intercostal · cracked · Apr 16, 1999 · N15820 · Doug DC982 · Passenger/Crew Doors
  > INSPECTION FOUND A.5 INCH CRACK IN INTERCOSTAL OF FORWARD ENTRY DOOR JUST AFT OF INTERNAL DOOR HANDLE. THE INTERCOSTAL WAS REPLACED IAW SRM 51-30-1 AND 51-30-2.
- [SDR CALA9900420](https://openairdocs.org/sdr/CALA9900420.md): Skin · dented · Apr 16, 1999 · N15820 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND LT FUSELAGE SKIN DENTED AT STA 237 BETWEEN LONGERON 17L AND 18L. THE SKIN AND LOWER SECTION OF FINGER DOUBLER WERE REPLACED IAW ECRA 5330-02445.
- [SDR CALA9900416](https://openairdocs.org/sdr/CALA9900416.md): Angle · corroded · Apr 15, 1999 · N15820 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND AFT CARGO COMPARTMENT Z-ANGLE CORRODED AROUND HI SHEARS. A REPAIR WAS INSTALLED IAW SRM 53-05, FIGURE 63.
- [SDR CALA9900411](https://openairdocs.org/sdr/CALA9900411.md): Skin · dented · Apr 14, 1999 · N15820 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 383 BETWEEN L30 AND L29R. A REPAIR WAS INSTALLED IAW SRM 53-04, FIGURE 38, SHEET 22.
- [SDR CALA9900389](https://openairdocs.org/sdr/CALA9900389.md): Spacer · corroded · Apr 12, 1999 · N15820 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND MAIN BAGGAGE BIN Z-ANGLE CORRODED ON REPAIR SPACER AT STA 636 TO 693. THE SPACER WAS REMOVED AND REPLACED IAW SRM 53-05, FIGURE 63.
- [SDR CALA9700637](https://openairdocs.org/sdr/CALA9700637.md): Prox Sensor · damaged · May 4, 1997 · N15820 · Doug DC982 · Landing Gear Position and Warning
  > THE GEAR DOOR OPEN LIGHT REMAINED ON WHEN GEAR WAS EXTENDED FOR LANDING ON APPROACH. A GO-AROUND WAS PERFORMED WHILE COMPLYING WITH ABNORMAL PROCEDURES. THE GEAR DOOR OPEN LIGHT REMAINED ON. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE D1-30
- [SDR CALA9700548](https://openairdocs.org/sdr/CALA9700548.md): Skin · dented · Apr 9, 1997 · N15820 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A 2.75 INCH LONG BY.25 INCH DEEP DENT IN LT FUSELAGE SKIN AT STA 664 BETWEEN LONGERON 22L AND 23L. DOUBLER AND FILLER WERE INSTALLED IAW SRM 53-04, FIGURE 38.
- [SDR CALA9700549](https://openairdocs.org/sdr/CALA9700549.md): Jamb · corroded · Apr 7, 1997 · N15820 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND MAIN BAGGAGE BIN DOORWAY JAMB BEAM CORRODED AROUND SEVERAL HI-SHEARS. THE CORROSION WAS REMOVED, DOUBLERS WERE INSTALLED IAW SRM 53-05, FIGURE 63.
- [SDR CALA9700550](https://openairdocs.org/sdr/CALA9700550.md): Angle · cracked · Apr 4, 1997 · N15820 · Doug DC982 · Wing Miscellaneous Structure
  > INSPECTION FOUND A.75 INCH CRACK IN LT WING LEADING EDGE RIB ANGLE JUST OUTBOARD OF 8L SLAT TRACK AT STA XRS 276. AN ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-30-2.
- [SDR CALA9700444](https://openairdocs.org/sdr/CALA9700444.md): Actuator Link · broken · Mar 31, 1997 · N15820 · Doug DC982 · Landing Gear Actuator
  > THE LT MLG UNSAFE LIGHT AND GEAR DOOR OPEN LIGHT REMAINED ILLUMINATED AFTER TAKEOFF. THE GEAR WAS CYCLED, BUT THERE WAS NO CHANGE IN INDICATION. THE AIRCRAFT WAS RETURNED TO SFO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LT MLG ACTUATOR LOWER L
- [SDR CALA9601332](https://openairdocs.org/sdr/CALA9601332.md): Air Cyc Mach · inoperative · Sep 26, 1996 · N15820 · Doug DC982 · Cabin Cooling System
  > SMOKE ENTERED THE CABIN DURING TAXI OUT. THE AIRCRAFT WAS RETURNED TO THE GATE. THE AIR COND TURBINE NOZZLE C/B POPPED WHEN COLDER POSITION SELECTED. MAINTENANCE FOUND WIRING CHAFING/SHORTING TO RT TURBINE NOZZLE SHUTOFF VALVE. THE WIRING WAS SPLICED AND T
- [SDR CALA9600659](https://openairdocs.org/sdr/CALA9600659.md): Control Valve · stuck open · May 29, 1996 · N15820 · Doug DC982 · Cabin Cooling System
  > STRONG FUMES WERE REPORTED IN THE CABIN AFTER TAKEOFF FROM IAH. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED A BURN-OUT PROCEDURE PER MM 21-20-02, PARAGRAPH 7C. THE RT CABIN TEMP CONTROL VALVE WAS FOUND STUCK IN T

## 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 = 'N15820' AND deregistration_id = 'N15820-2013-03-21'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N15820-2013-03-21/reports

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