# Service difficulty reports: N33805, cancelled May 18, 2004

A list on [N33805, cancelled May 18, 2004](https://openairdocs.org/deregistered/N33805-2004-05-18.md).

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

- [SDR CALA2000279](https://openairdocs.org/sdr/CALA2000279.md): Actuator · corroded · May 11, 2002 · N33805 · Doug DC982 · Entrance Stairs
  > AFT VENTRAL STAIRS ACTUATOR LOWER TUBE, RT, IS CORRODED 2 INCHES. REPLACED RT LOWER STRUT ON VENTRAL STAIRS AND PERFORMED ADJUSTMENT AND TEST IAW MM 52-63-00.
- [SDR CALA0101000](https://openairdocs.org/sdr/CALA0101000.md): Battery Pack · discharged · Nov 12, 2001 · N33805 · Doug DC982 · Emergency Lighting
  > THE OVERWING EMERGENCY EXIT IDENTIFIERS ABOVE DOORS ON LT AND RT SIDE OF AIRCRAFT WERE FOUND INOPERATIVE. THE BATTERIES IN EMERGENCY BATTERY PACKS IN O/H BIN AT ROW 20DEF WERE REPLACED IAW MM 33-50-00.
- [SDR CALA0100958](https://openairdocs.org/sdr/CALA0100958.md): Power Supply · discharged · Oct 17, 2001 · N33805 · Doug DC982 · Emergency Lighting
  > BOTH LEFT AND RIGHT OVERWING EVACUATION LIGHTS INOP. REMOVED AND REPLACED POWER SUPPLY PER MM 33-53-00 PAGE 407.
- [SDR CALA0100112](https://openairdocs.org/sdr/CALA0100112.md): Skin · dented · Feb 10, 2001 · N33805 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AT FS 275 BETWEEN LONGERON 22L AND 23L. THE DENT WAS COLD WORKED AND A DOUBLER WAS INSTALLED IAW SRM 53-04-38 AND 51-10-3.
- [SDR CALA0100109](https://openairdocs.org/sdr/CALA0100109.md): Seat Track · corroded · Feb 9, 2001 · N33805 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND CABIN LEFT I/B SEAT TRACK CORRODED AT FS 1031 - 1169. THE SEAT TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-30-1 AND 53-05, FIGURE 4.
- [SDR CALA0100098](https://openairdocs.org/sdr/CALA0100098.md): Cargo Track · corroded · Feb 2, 2001 · N33805 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND MID CARGO LT TIE DOWN TRACK CORRODED AT FS 522 - 788. THE TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-30-2 AND 53-05, FIGURE 6.
- [SDR CALA0100097](https://openairdocs.org/sdr/CALA0100097.md): Seat Track · corroded · Feb 2, 2001 · N33805 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND CABIN LEFT O/B SEAT TRACK CORRODED AT FS 1117 - 1136. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND A NEW SECTION OF TRACK WAS INSTALLED IAW SRM 53-05, FIGURE 4F.
- [SDR CALA0100096](https://openairdocs.org/sdr/CALA0100096.md): Skin · gouged · Feb 2, 2001 · N33805 · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND SKIN GOUGED AT AFT CARGO DOOR LOWER EDGE OF PAN. THE RIVETS WERE REMOVED AND A DOUBLER WAS INSTALLED IAW SRM 51-30-2 AND EA 9-5230-2-A0832.
- [SDR CALA0100088](https://openairdocs.org/sdr/CALA0100088.md): Fitting · cracked · Feb 1, 2001 · N33805 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 1 INCH CRACK IN LEFT W/W FORWARD I/B (FWD OF MLG ATTACH) ANGLE T-FITTING. THE FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 51-30-05 AND 51-30-3.
- [SDR CALA0100083](https://openairdocs.org/sdr/CALA0100083.md): Skin · corroded · Jan 31, 2001 · N33805 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND INNER SKIN DOUBLER CORRODED AT FS 1286 BETWEEN LONGERONS 21L AND 22L. THE INNER DOUBLER WAS REMOVED AND REPLACED IAW SRM 51-30-2, 51-30-5, AND ECRA 5332-01009.
- [SDR CALA0100084](https://openairdocs.org/sdr/CALA0100084.md): Frame · cracked · Jan 30, 2001 · N33805 · Doug DC982 · Fuselage Main, Frame
  > INSPECTION FOUND A 4 INCH CRACK IN AFT ACCESSORY COMPARTMENT FRAME UNDER RADIUS BLOCK AT LONGERON ATTACH POINT, FS 1446, LONGERON 5L. THE FRAME WAS REMOVED AND A NEW FRAME WAS INSTALLED IAW SRM 51-10-4, 53-03, FIGURE 30, AND 51-30-5.
- [SDR CALA0100080](https://openairdocs.org/sdr/CALA0100080.md): Pan · cracked · Jan 29, 2001 · N33805 · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND A 1 INCH CRACK IN MID CARGO DOOR PAN. THE CRACK WAS STOP DRILLED IAW SRM 52-03, FIGURE 8. A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-03, FIGURE 8, 51-10-3, AND 51-30-2.
- [SDR CALA0100079](https://openairdocs.org/sdr/CALA0100079.md): Floorbeam · corroded · Jan 29, 2001 · N33805 · Doug DC982 · Fuselage Main, Floor Beam
  > INSPECTION FOUND AFT LT LAV FLOORBEAM CORRODED AT STA 1322, LBL 41. THE CORROSION WAS TRIMMED OUT AND A DOUBLER, REPAIR STRIP, AND SHIM WERE INSTALLED IAW SRM 53-05, FIGURE 20A, 51-30-2, AND 51-30-5.
- [SDR CALA0100076](https://openairdocs.org/sdr/CALA0100076.md): Skin · dented · Jan 27, 2001 · N33805 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AT FS 275 BETWEEN LONGERONS 21L AND 22L. THE DENT WAS COLD WORKED IAW SRM 53-04-38. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-04-38, 51-10-3, AND 51-30-2.
- [SDR CALA0100075](https://openairdocs.org/sdr/CALA0100075.md): Web · corroded · Jan 27, 2001 · N33805 · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND AFT CARGO DOOR WEB CORRODED AROUND ATTACH RIVNUT HOLES. THE CORROSION WAS REMOVED IAW SRM 51-10-3. THE CORRODED AREAS WERE REPAIRED IAW SRM 52-01, FIGURE 2 AND 51-10-3.
- [SDR CALA0100074](https://openairdocs.org/sdr/CALA0100074.md): Fitting · cracked · Jan 26, 2001 · N33805 · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND A 2 INCH CRACK IN AFT CARGO DOOR LOWER FITTING. THE FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 51-30-2, 51-10-4, 51-10-3, AND 51-30-1.
- [SDR CALA0100073](https://openairdocs.org/sdr/CALA0100073.md): Skin · dented · Jan 26, 2001 · N33805 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AT FS 237 BETWEEN LONGERONS 17L AND 18L. THE SKIN WAS REMOVED AND REPLACED IAW SRM 53-34-0, FIGURE 2, PAGE 7, 51-30-2, 51-30-5, AND 51-10-3.
- [SDR CALA0100072](https://openairdocs.org/sdr/CALA0100072.md): Skin · cracked · Jan 26, 2001 · N33805 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A 1 INCH CRACK IN LT FUSELAGE SKIN ABOVE NR 1 ENGINE PYLON AT STA 1401. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 2, SHEET 3, 53-10-3, AND 51-30-2.
- [SDR CALA0100071](https://openairdocs.org/sdr/CALA0100071.md): Structure · cracked · Jan 25, 2001 · N33805 · Doug DC982 · Landing Gear Doors
  > INSPECTION FOUND TWO 1 INCH CRACKS IN FORWARD LOWER CORNER OF LT MLG I/B DOOR. THE CRACKS WERE STOP DRILLED AND DOUBLERS WERE INSTALLED IAW SRM 51-10-4, 51-10-3, 51-30-2, 51-30-5, AND EA 9-5331-2-A0831.
- [SDR CALA0100068](https://openairdocs.org/sdr/CALA0100068.md): Angle · corroded · Jan 24, 2001 · N33805 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CUSP ANGLE AT L-1 DOOR, FS 200, LBL 54 CORRODED. THE CUSP ANGLE WAS REMOVED AND REPLACED IAW EA 9-5310-2-A0829 AND ECRA 5310-04094.
- [SDR CALA0100067](https://openairdocs.org/sdr/CALA0100067.md): Fitting · cracked · Jan 24, 2001 · N33805 · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND A 1 INCH CRACK IN MID CARGO DOOR FITTING AND WITH UPPER INTERCOSTAL CLIP CRACKED. THE FITTING AND T-ANGLE WERE REMOVED AND A NEW FITTING AND ANGLE WERE INSTALLED IAW SRM 51-10-4, 51-30-2, AND 51-30-1.
- [SDR CALA0100065](https://openairdocs.org/sdr/CALA0100065.md): Skin · dented · Jan 23, 2001 · N33805 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND LT FORWARD FUSELAGE SKIN DENTED AT FS 133, L10L. THE DENT WAS COLD WORKED AND A DOUBLER WAS INSTALLED IAW SRM 51-30-5, 51-30-2, 53-04, FIGURE 35, 51-10-3, AND EA 9-5331-2-A0835.
- [SDR CALA0100064](https://openairdocs.org/sdr/CALA0100064.md): Skin · dented · Jan 23, 2001 · N33805 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FUSELAGE EXTERNAL SKIN AT FORWARD LT SIDE OF E AND E DOOR CUTOUT STA 145, L28L DENTED. THE SKIN WAS REPAIRED BY INSTALLING FILLER AND DOUBLERS IAW EA 9-5331-2-A0834 AND SRM 51-10-3.
- [SDR CALA0100054](https://openairdocs.org/sdr/CALA0100054.md): Fitting · cracked · Jan 22, 2001 · N33805 · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND A 3 INCH CRACK IN FORWARD CARGO DOOR FITTING I/B OF AFT HINGE. THE FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 51-30-1, 51-30-2, 51-10-4, AND 51-10-3.
- [SDR CALA0100053](https://openairdocs.org/sdr/CALA0100053.md): Seat Track · corroded · Jan 22, 2001 · N33805 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND CABIN LT CENTER SEAT TRACK CORRODED AT FS 1032 - 1184. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-05, FIGURE 4F.
- [SDR CALA0100052](https://openairdocs.org/sdr/CALA0100052.md): Skin · dented · Jan 21, 2001 · N33805 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AT FS 230 BETWEEN LONGERON 19L AND 20L. THE DENTED AREA WAS CUT OUT IAW SRM 53-04, FIGURE 25. A DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 25, 51-30-2, 51-30-4, AND 51-30-5.
- [SDR CALA0100051](https://openairdocs.org/sdr/CALA0100051.md): Door Frame · cracked · Jan 21, 2001 · N33805 · Doug DC982 · Fuselage Main, Structure
  > INSPECTION FOUND A 1 INCH CRACK (PAST STOP DRILL) IN RT MLG DOOR SUPPORT FRAME AT STA 946, RBL 10. THE EXISTING REPAIR DOUBLERS WERE REMOVED FOR ACCESS IAW SRM 51-30-2. THE CRACK WAS STOP DRILLED IAW SRM 51-10-4. THE REPAIR DOUBLERS WERE REINSTALLED IAW SRM
- [SDR CALA0100044](https://openairdocs.org/sdr/CALA0100044.md): Skin · dented · Jan 17, 2001 · N33805 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AT FS 260 BETWEEN LONGERONS 24R AND 25R AND BETWEEN LONGERONS 27L AND 28L. A DOUBLER WAS INSTALLED AT EACH LOCATION IAW SRM 53-04, FIGURE 38, 51-10-4, 51-10-3, AND 51-30-2.
- [SDR CALA0100043](https://openairdocs.org/sdr/CALA0100043.md): Skin · dented · Jan 17, 2001 · N33805 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AT FS 375 BETWEEN LONGERON 29L AND 30 AND AT FS 470, BETWEEN LONGERONS 20L AND 21L. A DOUBLER WAS INSTALLED AT EACH LOCATION IAW SRM 53-04, FIGURE 38, 51-10-4, 51-10-3, AND 51-30-2.
- [SDR CALA0100038](https://openairdocs.org/sdr/CALA0100038.md): Skin · dented · Jan 16, 2001 · N33805 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AT FS 500 - 520 BETWEEN LONGERONS 20R AND 21R AND AT FS 550 - 560 BETWEEN LONGERONS 21L AND 22L. THE DENTS WERE COLD WORKED AND DOUBLERS WERE INSTALLED AT EACH LOCATION IAW SRM 53-04-38 AND 51-30-2.
- [SDR CALA0100037](https://openairdocs.org/sdr/CALA0100037.md): Frame · cracked · Jan 16, 2001 · N33805 · Doug DC982 · Fuselage Main, Frame
  > INSPECTION FOUND E&E COMPARTMENT FRAME CRACKED PAST STOP DRILL HOLE AT FS 150, L21R. THE EXISTING REPAIR WAS REMOVED, THE CRACK WAS STOP DRILLED, AND A REPAIR WAS INSTALLED IAW SRM 51-30-05 AND 51-10-4.
- [SDR CALA9901474](https://openairdocs.org/sdr/CALA9901474.md): Power Supply · inop · Nov 6, 1999 · N33805 · Doug DC982 · Emergency Lighting
  > INSPECTION FOUND EMERGENCY OVERHEAD LIGHTS INOPERATIVE AT ROWS 23-27. THE BATTERY POWER SUPPLY AT STATION 1150 IN RT OVERHEAD BIN WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD IAW MM 33-53-00.
- [SDR CALA9900117](https://openairdocs.org/sdr/CALA9900117.md): Skin · dented · Feb 5, 1999 · N33805 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND THE FUSELAGE SKIN DENTED AT STA 218, LONGERON 17L. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5330-02766.
- [SDR CALA9900116](https://openairdocs.org/sdr/CALA9900116.md): Brace · cracked · Feb 5, 1999 · N33805 · Doug DC982 · Spoilers
  > INSPECTION FOUND A CRACK OF UNSPECIFIED LENGTH IN THE LT GROUND SPOILER ACTUATOR I/B ATTACH BRACKET CROSS BRACE. A NEW CROSS BRACE WAS INSTALLED IAW SRM 51-30-5.
- [SDR CALA9900107](https://openairdocs.org/sdr/CALA9900107.md): Escape Line · frayed · Feb 2, 1999 · N33805 · Doug DC982 · Emergency Equipment
  > INSPECTION FOUND THE LT AND RT OVERWING EMERGENCY ESCAPE LINES FRAYED. NEW ESCAPE LINE WAS INSTALLED IAW SRM 51-30-1 AND MM 25-61-00, FIGURE 202.
- [SDR CALA9900095](https://openairdocs.org/sdr/CALA9900095.md): Beam · cracked · Jan 29, 1999 · N33805 · Doug DC982 · Service Doors
  > INSPECTION FOUND A.5 INCH CRACK IN FORWARD SERVICE DOOR NR 4 HORIZONTAL BEAM. THE BEAM WAS REMOVED AND REPLACED IAW SRM 51-30.
- [SDR CALA9900094](https://openairdocs.org/sdr/CALA9900094.md): Beam · cracked · Jan 29, 1999 · N33805 · Doug DC982 · Passenger/Crew Doors
  > INSPECTION FOUND A.75 INCH CRACK IN OUTBOARD RADIUS OF MAIN CABIN DOOR TOP NR 1 HORIZONTAL BEAM. THE BEAM WAS REMOVED AND REPLACED IAW SRM 51-30-2.
- [SDR CALA9701503](https://openairdocs.org/sdr/CALA9701503.md): Fcu · leaking · Oct 24, 1997 · N33805 · Doug DC982 · APU Engine Fuel and Control
  > WHILE OPERATING THE APU WITH THE NR 1 GENERATOR PLACARDED INOPERATIVE, THE APU AUTO SHUTDOWN WHEN CLIMBING THROUGH 28,000 FEET. THE APU WAS RESTARTED AT 26,000 FEET AND THE AIRCRAFT LANDED WITHOUT FURTHER PROBLEM. THE APU FCU WAS FOUND LEAKING. THE APU FCU
- [SDR CALA9700222](https://openairdocs.org/sdr/CALA9700222.md): Power Supply · inoperative · Feb 19, 1997 · N33805 · Doug DC982 · Emergency Lighting
  > INSPECTION FOUND TWO EXTERIOR OVERWING EMERGENCY EVACUATION LIGHTS INOPERATIVE. MAINTENANCE FOUND THE POWER SUPPLY AT FAULT. THE POWER SUPPLY WAS REMOVED AND REPLACED.
- [SDR CALA9700152](https://openairdocs.org/sdr/CALA9700152.md): Door Pan · cracked · Jan 28, 1997 · N33805 · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND A 3 INCH CRACK IN MAIN BAGGAGE BIN DOOR PAN AT LOCK AFT CAM AREA. THE PAN WAS REPAIRED IAW ECRA 5210-01283 AND SRM 52-05, FIGURE 26A.
- [SDR CALA9700147](https://openairdocs.org/sdr/CALA9700147.md): Door Pan · cracked · Jan 27, 1997 · N33805 · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND A 3 INCH CRACK IN FORWARD BAGGAGE BIN DOOR PAN AT LOCK CAM AREA. THE PAN WAS REPAIRED IAW ECRA 5210-01283 AND SRM 52-05, FIGURE 26A.
- [SDR CALA9700154](https://openairdocs.org/sdr/CALA9700154.md): Fitting · cracked · Jan 22, 1997 · N33805 · Doug DC982 · Fuselage, Door Hinge
  > INSPECTION FOUND A 2.5 INCH CRACK IN UPPER RIGHT FITTING AND A 1.5 INCH CRACK IN UPPER LEFT FITTING AT MAIN BAGGAGE BIN STA 826. THE FITTINGS WERE REPLACED IAW SRM 51-30-5.
- [SDR CALA9700153](https://openairdocs.org/sdr/CALA9700153.md): Belt Frame · corroded · Jan 22, 1997 · N33805 · Doug DC982 · Fuselage Main, Frame
  > INSPECTION FOUND BELT FRAME LOWER CHANNEL CORRODED AT STA 1307, LONGERON 27R TO 27L. THE CORRODED SECTION OF BELT FRAME WAS CUT OUT, A NEW SEGMENT OF FRAME AND REPAIR DOUBLERS WERE INSTALLED IAW SRM 53-03, FIGURE 2A.
- [SDR CALA9700151](https://openairdocs.org/sdr/CALA9700151.md): Door Pan · cracked · Jan 21, 1997 · N33805 · Doug DC982 · Passenger/Crew Doors
  > INSPECTION FOUND A 1.25 INCH CRACK AT LOWER HINGE CUTOUT OF MAIN CABIN DOOR PAN. THE PAN WAS REPLACED IAW SRM 52-11-0.
- [SDR CALA9700150](https://openairdocs.org/sdr/CALA9700150.md): Angle · corroded · Jan 20, 1997 · N33805 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND Z-ANGLE AND FLOOR MOUNTS CORRODED AT AFT SERVICE DOOR THRESHOLD. A NEW Z-ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-30-2.
- [SDR CALA9700149](https://openairdocs.org/sdr/CALA9700149.md): Rib · cracked · Jan 20, 1997 · N33805 · Doug DC982 · Wing, Rib/Bulkhead
  > INSPECTION FOUND A.5 INCH CRACK IN LT WING LEADING EDGE RIB JUST OUTBOARD OF 8L SLAT TRACK AT STA XRS 270. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5710-01776.
- [SDR CALA9700148](https://openairdocs.org/sdr/CALA9700148.md): Rib · cracked · Jan 20, 1997 · N33805 · Doug DC982 · Wing, Rib/Bulkhead
  > INSPECTION FOUND A.5 INCH CRACK IN RT WING LEADING EDGE RIB, TWO RIBS OUTBOARD OF 8R SLAT TRACK, STA XRS 277. A DOUBLER WAS INSTALLED IAW SRM 57-01.
- [SDR CALA9600647](https://openairdocs.org/sdr/CALA9600647.md): Actuator · inoperative · May 25, 1996 · N33805 · Doug DC982 · Landing Gear Actuator
  > THE NOSE GEAR WAS SLOW TO RETRACT AFTER TAKEOFF. THE RED LIGHT EXTINGUISHED AND DOORS CLOSED AFTER APPROXIMATELY 20 TO 25 SECONDS. THE FLIGHT WAS CONTINUED AND THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE FOUND THE NOSE GEAR RETRACT CYLINDER AT
- [SDR CAL950114](https://openairdocs.org/sdr/CAL950114.md): Circuit Breaker · failed · Feb 10, 1995 · N33805 · Doug DC982 · AC Power Distribution System
  > FLT NR 0246 - IAH - SEVERAL LEFT AC BUS CIRCUIT BREAKERS BEGAN POPPING AFTER TAKEOFF FROM IAH. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE B1-743 TO AMP 'C' PHASE CIRCUIT BREAKER ON LEFT GENERATOR PANEL AT FAULT.

## 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 = 'N33805' AND deregistration_id = 'N33805-2004-05-18'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N33805-2004-05-18/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.