# Service difficulty reports: N12811, cancelled Jun 1, 2007

A list on [N12811, cancelled Jun 1, 2007](https://openairdocs.org/deregistered/N12811-2007-06-01.md).

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

- [SDR CALA0400031](https://openairdocs.org/sdr/CALA0400031.md): Megaphone · inoperative · Jan 15, 2004 · N12811 · Doug DC982 · Emergency Equipment
  > INSPECTION FOUND THE FORWARD CABIN MEGAPHONE INOPERATIVE. THE MEGAPHONE WAS REMOVED AND REPLACED.
- [SDR CALA0300530](https://openairdocs.org/sdr/CALA0300530.md): Fan · seized · Aug 17, 2003 · N12811 · Doug DC982 · Air Distribution Fan
  > A/C HAD A CHRONIC INFLT PROBLEM WITH AN ELECTRICAL ODOR AFT. TROUBLESHOOTING PERFORMED. SOURCE OF ODOR APPEARED TO BE COMING FROM AFT GALLEY. COFFEEMAKERS, OVENS, & ACCESS PANELS INSPECTED, NO EVIDENCE OF BURNING. PACK BURNOUT PERFORMED & COALESCER BAGS R & R.
- [SDR CALA0200341](https://openairdocs.org/sdr/CALA0200341.md): Beltframe · cracked · Jun 14, 2002 · N12811 · Doug DC982 · Fuselage Main, Frame
  > INSPECTION FOUND A 1" CRACK IN TAIL COMPARTMENT BELTFRAME AT STA 1418, LONGERON 1. REPAIRED BELTFRAME IAW SRM 53-03, FIGURE 4.
- [SDR CALA0200338](https://openairdocs.org/sdr/CALA0200338.md): Web · cracked · Jun 12, 2002 · N12811 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND TAIL COMPARTMENT BELTFRAME WEB CRACKED AT STA 1463 L18R AND L18L. BOTH CRACKS WERE 2" LONG. THE CRACKS WERE STOP DRILLED AND DOUBLERS WERE INSTALLED IAW SRM 53-01, FIGURE 2.
- [SDR CALA0000459](https://openairdocs.org/sdr/CALA0000459.md): Pan · chafed · Apr 11, 2000 · N12811 · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND AFT BAG BIN DOOR PAN CHAFED AT STOP PAD AREAS. REPAIRED IAW ECRA 5230-01540.
- [SDR CALA0000457](https://openairdocs.org/sdr/CALA0000457.md): Pan · chafed · Apr 11, 2000 · N12811 · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND DOOR PAN CHAFED BY DOOR STOP IN TWO PLACES AT AFT SIDE AND THREE PLACES AT FORWARD SIDE, FORWARD BAGGAGE BIN. REPAIRED IAW ECRA 5230-01540.
- [SDR CALA0000455](https://openairdocs.org/sdr/CALA0000455.md): Longeron · cracked · Apr 11, 2000 · N12811 · Doug DC982 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND A HALF INCH CRACK IN LONGERON 4 LT AT STA 160. THE LONGERON WAS REPAIRED IAW ECRA 5310-04005.
- [SDR CALA0000454](https://openairdocs.org/sdr/CALA0000454.md): Angle · cracked · Apr 11, 2000 · N12811 · Doug DC982 · Vertical Stabilizer
  > INSPECTION FOUND LT VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE CRACKED AT STA 1474 - 1485. THERE WERE FIVE CRACKS TOTALING 8 INCHES IN COMBINED LENGTH. THE ATTACH ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-05 AND 51-30-01.
- [SDR CALA0000413](https://openairdocs.org/sdr/CALA0000413.md): Cable · out of rig · Apr 6, 2000 · N12811 · Doug DC982 · Aerodynamic Fairings
  > THE FORCE REQUIRED TO DROP THE TAIL CONE USING INTERIOR AND EXTERIOR RELEASE HANDLES EXCEEDED 35 POUNDS. THE TAIL CONE RELEASE SYSTEM CABLES WERE ADJUSTED IAW MM 53-53-00.
- [SDR CALA0000408](https://openairdocs.org/sdr/CALA0000408.md): Frame · worn · Apr 5, 2000 · N12811 · Doug DC982 · Fuselage Main, Frame
  > INSPECTION FOUND A HOLE WORN INTO FRAME WEB AT STA 1380 AT LT AIR CONDITIONING TEMP CONTROL VALVE. REPAIRED FRAME WEB IAW SRM 53-01.
- [SDR CALA0000407](https://openairdocs.org/sdr/CALA0000407.md): Beam · cracked · Apr 5, 2000 · N12811 · Doug DC982 · Service Doors
  > INSPECTION FOUND A 1 INCH CRACK IN FORWARD SERVICE DOOR LOWER FORWARD BEAM. THE BEAM WAS REMOVED AND REPLACED IAW SRM 51-30-2.
- [SDR CALA0000406](https://openairdocs.org/sdr/CALA0000406.md): Cargo Track · corroded · Apr 5, 2000 · N12811 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND AFT CARGO BIN LEFT AND RIGHT TIEDOWN TRACKS CORRODED AROUND NUT PLATE HOLES AT STA 1022. THE TIEDOWN TRACKS WERE REMOVED AND REPLACED IAW SRM 51-10-3 AND 51-30-5.
- [SDR CALA0000405](https://openairdocs.org/sdr/CALA0000405.md): Pan · cracked · Apr 5, 2000 · N12811 · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND MID CARGO BIN DOOR PAN CRACKED AT FORWARD AND AFT LATCH. REPAIRED IAW SRM 52-05, FIGURE 26A.
- [SDR CALA0000404](https://openairdocs.org/sdr/CALA0000404.md): Skin · gouged · Apr 5, 2000 · N12811 · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND FORWARD CARGO DOOR SKIN GOUGED AT DOOR BOTTOM. REPAIRED IAW SRM 52-03, FIGURE 7.
- [SDR CALA0000402](https://openairdocs.org/sdr/CALA0000402.md): Pan · worn · Apr 5, 2000 · N12811 · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND FORWARD CARGO DOOR OUTER PAN WORN AT DOOR STOP PADS. REPAIRED AFT STOPS IAW ECRA 5330-02819.
- [SDR CALA0000401](https://openairdocs.org/sdr/CALA0000401.md): Pan · worn · Apr 5, 2000 · N12811 · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND FORWARD CARGO BIN LOWER DOOR PAN WORN IN TWO PLACES BY DOOR STOPS. TWO STRAPS WERE INSTALLED IAW ECRA 5330-02819.
- [SDR CALA0000394](https://openairdocs.org/sdr/CALA0000394.md): Floorbeam · gouged · Apr 4, 2000 · N12811 · Doug DC982 · Fuselage Main, Floor Beam
  > INSPECTION FOUND A HOLE GOUGED IN CABIN FLOORBEAM AT STA 396. A REPAIR WAS INSTALLED IAW SRM 53-05 SHEETS 1, 2 & 3.
- [SDR CALA0000379](https://openairdocs.org/sdr/CALA0000379.md): Longeron · cracked · Mar 31, 2000 · N12811 · Doug DC982 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND A.5 INCH CRACK IN LONGERON 2R JUST OVER BELTFRAME AT STA 1429. A NEW SECTION OF LONGERON WAS SPLICED IN IAW SRM 53-02, FIGURE 18, SHEET 2.
- [SDR CALA0000375](https://openairdocs.org/sdr/CALA0000375.md): Pan · cracked · Mar 30, 2000 · N12811 · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND AFT BAG BIN DOOR EXTERIOR HANDLE PAN GOUGED WITH A 1 INCH CRACK. THE PAN WAS REMOVED AND REPLACED IAW MM 51-30-02.
- [SDR CALA0000374](https://openairdocs.org/sdr/CALA0000374.md): Beltframe · corroded · Mar 30, 2000 · N12811 · Doug DC982 · Fuselage Main, Frame
  > INSPECTION FOUND BELTFRAME CORRODED ON AFT SIDE AT STA 541 FROM LONGERON 29L TO 29R. THE CORROSION WAS REMOVED, TREATED AND PRIMED AREA IAW SRM 51-10-3 AND REINSTALLED FASTENERS IAW SRM 51-30-5.
- [SDR CALA0000373](https://openairdocs.org/sdr/CALA0000373.md): Beltframe · corroded · Mar 30, 2000 · N12811 · Doug DC982 · Fuselage Main, Frame
  > INSPECTION FOUND AFT BAG BIN BELTFRAME CORRODED AT STA 1238, LONGERON 24L. THE CORROSION WAS REMOVED, TREATED, AND PRIMED IAW SRM 53-01, FIGURE 1.
- [SDR CALA0000369](https://openairdocs.org/sdr/CALA0000369.md): Skin · dented · Mar 30, 2000 · N12811 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 389, LONGERON 29R TO 30. A REPAIR WAS INSTALLED IAW ECRA 5330-02800.
- [SDR CALA0000421](https://openairdocs.org/sdr/CALA0000421.md): Seat Track · corroded · Mar 30, 2000 · N12811 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND RT O/B SEAT TRACK CORRODED IN FORWARD GALLEY AREA AT STA 218-266. THE SEAT TRACK WAS REPLACED IAW SRM 53-05, FIGURE 4F.
- [SDR CALA0000368](https://openairdocs.org/sdr/CALA0000368.md): Floor Support · cracked · Mar 28, 2000 · N12811 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A.5 INCH CRACK IN MAIN CABIN FLOOR SUPPORT AT STA 826 UNDER RIGHT I/B SEAT TRACK. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-1.
- [SDR CALA0000367](https://openairdocs.org/sdr/CALA0000367.md): Seat Track · cracked · Mar 28, 2000 · N12811 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND A.75 INCH CRACK IN MAIN CABIN FLOOR SUPPORT AT STA 927 BELOW LT O/B SEAT TRACK. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-0.
- [SDR CALA0000366](https://openairdocs.org/sdr/CALA0000366.md): Floor Support · corroded · Mar 28, 2000 · N12811 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FORWARD R-1 ENTRY SLIDE ARMING BAR ATTACHED FORWARD AND AFT FLOOR SUPPORTS CORRODED. THE SUPPORTS WERE REMOVED AND NEW ONES WERE INSTALLED IAW SRM 51-30-1.
- [SDR CALA0000355](https://openairdocs.org/sdr/CALA0000355.md): Seat Track · corroded · Mar 27, 2000 · N12811 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND LT CENTER SEAT TRACK CORRODED ON BOTH SIDES OF FLOOR SUPPORT FLANGES FROM FS 1041 - 1309. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-00.
- [SDR CALA0000332](https://openairdocs.org/sdr/CALA0000332.md): Skin · dented · Mar 22, 2000 · N12811 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FUSELAGE SKIN DENTED AND GOUGED AT STA 120-133, LONGERON 23R. A REPAIR WAS INSTALLED IAW SRM 53-04, FIGURE 38.
- [SDR CALA0000330](https://openairdocs.org/sdr/CALA0000330.md): Line · frayed · Mar 22, 2000 · N12811 · Doug DC982 · Emergency Equipment
  > INSPECTION FOUND THE LEFT AND RIGHT OVERWING EMERGENCY ESCAPE LINES FRAYED AT ATTACH HOOK. THE EMERGENCY ESCAPE LINES WERE REMOVED AND REPLACED IAW MM 25-60-00.
- [SDR CALA0000329](https://openairdocs.org/sdr/CALA0000329.md): Skin · dented · Mar 22, 2000 · N12811 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND LT FUSELAGE SKIN DENTED AT STA 712, LONGERON 20L. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38.
- [SDR CALA9801857](https://openairdocs.org/sdr/CALA9801857.md): Actuator · burnt · Sep 26, 1998 · N12811 · Doug DC982 · Drag Control Actuator
  > THE CO-PILOT OBSERVED SMOKE COMING FROM THE THROTTLE QUADRANT AFTER TAKEOFF FROM COS. THE ELECTRICAL FIRE/SMOKE OF UNKNOWN ORIGIN EMERGENCY LIST WAS INITIATED AND THE AIRCRAFT WAS RETURNED TO COS WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE AUTO S
- [SDR CALA9800596](https://openairdocs.org/sdr/CALA9800596.md): Beam · cracked · Mar 26, 1998 · N12811 · Doug DC982 · Passenger/Crew Doors
  > INSPECTION FOUND A 1 INCH CRACK AT FORWARD END AND AFT END OF NR 1 DOOR BEAM OF MAIN CABIN DOOR. A NEW NR 1 MAIN CABIN DOOR BEAM WAS INSTALLED IAW SRM 51-30-1, 51-30-2, AND 51-30-5.
- [SDR CALA9800589](https://openairdocs.org/sdr/CALA9800589.md): Intercostal · cracked · Mar 25, 1998 · N12811 · Doug DC982 · Passenger/Crew Doors
  > INSPECTION FOUND A 1 INCH CRACK IN RADIUS OF MAIN CABIN DOOR INTERCOSTAL AFT OF HANDLE TORQUE SHAFT. THE INTERCOSTAL WAS REPLACED IAW SRM 51-30-02 AND 51-30-05.
- [SDR CALA9800588](https://openairdocs.org/sdr/CALA9800588.md): Skin · cracked · Mar 25, 1998 · N12811 · Doug DC982 · Passenger/Crew Doors
  > INSPECTION FOUND A 1 INCH CRACK IN MAIN CABIN DOOR EXTERIOR SKIN AROUND HOLD OPEN HOOK CUTOUT. A DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 20A, PAGE 43.
- [SDR CALA9800587](https://openairdocs.org/sdr/CALA9800587.md): Pivot Plates · corroded · Mar 25, 1998 · N12811 · Doug DC982 · Horizontal Stabilizer Structure
  > INSPECTION FOUND LT HORIZONTAL STABILIZER INBOARD AND OUTBOARD SET OF PIVOT PLATES CORRODED. THE PIVOT PLATES WERE REPLACED IAW SRM 51-30-5.
- [SDR CALA9701510](https://openairdocs.org/sdr/CALA9701510.md): Retract Mech · malfunctioned · Oct 28, 1997 · N12811 · Doug DC982 · Landing Gear Retraction/Extension System
  > THE AIRCRAFT WAS STUCK IN GROUND MODE AND THE GEAR WOULD NOT RETRACT AFTER TAKEOFF. QRH PROCEDURES WERE COMPLIED WITH AND THE AIRCRAFT WAS RETURNED TO IAH WHERE IT MADE A NORMAL LANDING. MAINTENANCE CHECKED THE GROUND SENSING SWITCHES IAW MM 32-23-01 AND NO
- [SDR CALA9700188](https://openairdocs.org/sdr/CALA9700188.md): Bus Control · malfunctioned · Feb 17, 1997 · N12811 · Doug DC982 · AC Generation System
  > ALL ELECTRICAL POWER FELL OFF LINE AND ARTS WAS INITIATED AFTER TAKEOFF. EMERGENCY POWER WAS TURNED ON, THE APU GENERATOR WAS PUT ON LINE, PARTIAL POWER WAS RESTORED. WHEN ATTEMPTING TO TURN EMERGENCY POWER OFF A LOUD HUM WAS HEARD FROM CIRCUIT BREAKER PANEL
- [SDR CALA9600967](https://openairdocs.org/sdr/CALA9600967.md): Airseal · worn · Jul 6, 1996 · N12811 · Doug DC982 · Turbine Section
  > THE NR 1 ENGINE SPOOLED DOWN ACCOMPANIED BY A LOUD EXPLOSION WHILE CLIMBING THROUGH FL 310. ABNORMAL PROCEDURES WERE COMPLIED WITH AND THE AIRCRAFT WAS RETURNED TO SFO WHERE IT LANDED WITHOUT INCIDENT. THE NR 1 ENGINE WAS REMOVED AND REPLACED. THE SDR WILL
- [SDR CAL960033](https://openairdocs.org/sdr/CAL960033.md): Skin · cracked · Jan 16, 1996 · N12811 · Doug DC982 · Wing, Plate/Skin
  > IAH - FLT 1707 - INSPECTION FOUND A 5.25 INCH CRACK IN LEFT WING LEADING EDGE SKIN AT STA 242. A DOUBLER REPAIR WAS INSTALLED IAW ECRA 5730-01428. (X)
- [SDR CAL950515](https://openairdocs.org/sdr/CAL950515.md): Eel Batteries · inoperative · Jun 21, 1995 · N12811 · Doug DC982 · Emergency Lighting
  > FLT NR 0299 - EWR - INSPECTION FOUND THE INTERIOR EMERGENCY EXIT LIGHTS AT ROW 6-9 AND AT ENTRANCE TO COCKPIT DOOR INOPERATIVE. THE BATTERIES AT ROW 7 AND IN THE FORWARD OVERHEAD CEILING COMPARTMENT WERE REPLACED. OPERATION OF THE EMERGENCY EXIT LIGHTS WAS R

## 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 = 'N12811' AND deregistration_id = 'N12811-2007-06-01'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N12811-2007-06-01/reports

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