# Service difficulty reports: N76823, cancelled Sep 6, 2005

A list on [N76823, cancelled Sep 6, 2005](https://openairdocs.org/deregistered/N76823-2005-09-06.md).

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

- [SDR CALA0100703](https://openairdocs.org/sdr/CALA0100703.md): Door Frame · corroded · Jul 27, 2001 · N76823 · Doug DC982 · Fuselage Main, Structure
  > INSPECTION FOUND FORWARD CARGO DOOR LOWER JAMB CORRODED UNDER DOOR STOPS AT STA 389-408. THE DOOR JAMB WAS REPAIRED IAW ECRA 5310-04165.
- [SDR CALA0100695](https://openairdocs.org/sdr/CALA0100695.md): Plate · corroded · Jul 26, 2001 · N76823 · Doug DC982 · Vertical Stabilizer
  > INSPECTION FOUND I/B AND O/B LEFT VERTICAL STABILIZER SUPPORT PLATES FOR HORIZONTAL STABILIZER PIVOT BOLT CORRODED IN AND AROUND BOLT HOLES. THE SUPPORT PLATES WERE REMOVED AND REPLACED IAW WORK CARD 08-5530-1-0005.
- [SDR CALA0100694](https://openairdocs.org/sdr/CALA0100694.md): Sill · corroded · Jul 26, 2001 · N76823 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND AFT CARGO DOOR JAMB SILL CORRODED AT STA 1155-1212. A REPAIR WAS INSTALLED IAW SRM 53-05, FIGURE 63.
- [SDR CALA0100678](https://openairdocs.org/sdr/CALA0100678.md): Spar · corroded · Jul 25, 2001 · N76823 · Doug DC982 · Horizontal Stabilizer, Spar/Rib
  > INSPECTION FOUND LT HORIZONTAL STABILIZER FORWARD UPPER SPAR AFT BARREL NUT HOLE AND BOLT HOLE CORRODED. REPAIRS WERE PERFORMED IAW ECRA 5511-01061.
- [SDR CALA0100673](https://openairdocs.org/sdr/CALA0100673.md): Plate · corroded · Jul 24, 2001 · N76823 · Doug DC982 · Vertical Stabilizer
  > INSPECTION FOUND I/B AND O/B RT VERTICAL STABILIZER SUPPORT PLATES CORRODED. THE I/B AND O/B RT VERTICAL STABILIZER SUPPORT PLATES WERE REMOVED AND REPLACED IAW EA SA003-5530-01238, SRM 51-10-2.
- [SDR CALA0100660](https://openairdocs.org/sdr/CALA0100660.md): Skin · dented · Jul 19, 2001 · N76823 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 218 JUST ABOVE LONGERON 19L. THE SKIN WAS REPAIRED IAW SRM 53-04, PAGE 218K.
- [SDR CALA9901060](https://openairdocs.org/sdr/CALA9901060.md): Wire · broken · Aug 16, 1999 · N76823 · Doug DC982 · Light System Wiring
  > INSPECTION FOUND EMERGENCY LIGHT AT ROW 6DEF INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE UNDER SEAT AND OPERATION CHECKED GOOD.
- [SDR CALA9900234](https://openairdocs.org/sdr/CALA9900234.md): Membrane · corroded · Mar 8, 1999 · N76823 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND AFT CARGO LEFT TUNNEL CUSP MEMBRANE CORRODED AT STA 1155 TO 1174. THE MEMBRANE WAS REPLACED IAW SRM 51-30-2.
- [SDR CALA9900233](https://openairdocs.org/sdr/CALA9900233.md): Seat Track · corroded · Mar 8, 1999 · N76823 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND LT CENTER SEAT TRACK CORRODED AT STA 1079 TO 1231. A NEW SEAT TRACK SECTION WAS INSTALLED IAW SRM 53-05, FIGURE 4F.
- [SDR CALA9900232](https://openairdocs.org/sdr/CALA9900232.md): Web · cracked · Mar 8, 1999 · N76823 · Doug DC982 · Passenger/Crew Doors
  > INSPECTION FOUND A 1 INCH CRACK AT AFT WEB PLATE LIGHTENING HOLE BETWEEN NR 6 AND NR 7 BEAMS OF MAIN CABIN DOOR. THE AREA WAS REPAIRED IAW SRM 51-30-1, 51-30-2, AND 51-30-4.
- [SDR CALA9900229](https://openairdocs.org/sdr/CALA9900229.md): Release Mech · failed test · Mar 6, 1999 · N76823 · Doug DC982 · Aerodynamic Fairings
  > THE TAIL CONE RELEASE PULL WAS LOW AT 15 POUNDS DURING TEST. THE TAIL CONE WAS REMOVED AND A NEW TAIL CONE WAS INSTALLED AND RIGGED IAW MM 53-53-00. OPERATIONAL CHECKS WERE GOOD.
- [SDR CALA9900217](https://openairdocs.org/sdr/CALA9900217.md): Beam · cracked · Mar 4, 1999 · N76823 · Doug DC982 · Passenger/Crew Doors
  > INSPECTION FOUND A 1 INCH CRACK IN RADIUS OF MAIN CABIN DOOR INTERIOR BEAM NR 2 FLANGE AFT END. REPAIRED BEAM IAW SRM 52-05, FIGURE 31, SHEET 3.
- [SDR CALA9900213](https://openairdocs.org/sdr/CALA9900213.md): Longeron · corroded · Mar 3, 1999 · N76823 · Doug DC982 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND LONGERON 30 CORRODED IN E & E COMPARTMENT AT STA 180. THE CORRODED SECTION OF LONGERON WAS REPLACED IAW SRM 51-10-3.
- [SDR CALA9900210](https://openairdocs.org/sdr/CALA9900210.md): Web · corroded · Mar 2, 1999 · N76823 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND E & E COMPARTMENT WEB MEMBRANE CORRODED AT STA 200, RT SIDE. THE AREA WAS REPAIRED IAW ECRA 5305-01049 AND SRM 53-05, FIGURE 55.
- [SDR CALA9900202](https://openairdocs.org/sdr/CALA9900202.md): Frame · corroded · Feb 27, 1999 · N76823 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND NR 15L CABIN WINDOW FRAME CORRODED AT STA 419. THE WINDOW FRAME SECTION WAS REMOVED AND REPLACED IAW SRM 51-10-3.
- [SDR CALA9900191](https://openairdocs.org/sdr/CALA9900191.md): Seat Track · corroded · Feb 24, 1999 · N76823 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND RT INBOARD SEAT TRACK CORRODED AT STA 226 TO 232. THE CORRODED SEAT TRACK SECTION WAS REMOVED AND REPLACED IAW SRM 53-05.
- [SDR CALA9900190](https://openairdocs.org/sdr/CALA9900190.md): Skin · dented · Feb 22, 1999 · N76823 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FUSELAGE SKIN DENTED AFT OF L-1 DOOR BETWEEN STA 229 AND 237 ABOVE LONGERON 18. A REPAIR WAS INSTALLED IAW ECRA 5330-02445.
- [SDR CALA9700315](https://openairdocs.org/sdr/CALA9700315.md): Bulkhead Tee Cap · corroded · Mar 3, 1997 · N76823 · Doug DC982 · Fuselage Main, Bulkhead
  > INSPECTION FOUND CORROSION ON BULKHEAD TEE CAP AT STA 110, LONGERON 29L. THE CORRODED AREA OF TEE CAP WAS CUT OUT, A REPAIR WAS INSTALLED IAW ECRA 5310-03443, SRM 53-04, FIGURE 14, SRM 53-01, FIGURE 2, SHEET 4 AND SRM 53-02, FIGURE 2.
- [SDR CALA9700317](https://openairdocs.org/sdr/CALA9700317.md): Channel · corroded · Mar 2, 1997 · N76823 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND MID BAGGAGE BIN THRESHOLD Z-CHANNEL CORRODED. THE CHANNEL WAS REMOVED AND REPLACED IAW SRM 51-30-0.
- [SDR CALA9601685](https://openairdocs.org/sdr/CALA9601685.md): Batteries · discharged · Nov 18, 1996 · N76823 · Doug DC982 · Emergency Lighting
  > INSPECTION FOUND THE EMERGENCY CEILING LIGHT INOPERATIVE AT ROW 12 TO 16. THE BATTERIES WERE REPLACED AND OPERATION OF THE LIGHT WAS RESTORED.
- [SDR CALA9601684](https://openairdocs.org/sdr/CALA9601684.md): Batteries · discharged · Nov 18, 1996 · N76823 · Doug DC982 · Emergency Lighting
  > INSPECTION FOUND THE CEILING EMERGENCY LIGHT INOPERATIVE AT ROW 28 TO 30. THE BATTERIES WERE REPLACED AND OPERATION OF THE LIGHT WAS RESTORED.
- [SDR CALA9601683](https://openairdocs.org/sdr/CALA9601683.md): Fuse · blown · Nov 18, 1996 · N76823 · Doug DC982 · Emergency Lighting
  > INSPECTION FOUND THE EMERGENCY EXIT LOCATOR SIGN AT AFT GALLEY DOOR INOPERATIVE. MAINTENANCE FOUND A BLOWN FUSE IN POWER SUPPLY. THE FUSE WAS REPLACED AND OPERATION OF THE EXIT SIGN WAS RESTORED.
- [SDR CALA9600840](https://openairdocs.org/sdr/CALA9600840.md): Oven · contaminated · Jun 16, 1996 · N76823 · Doug DC982 · Buffet/Galleys
  > THE FLIGHT ATTENDANT SAW SMOKE COMING FROM RT OVEN IN FORWARD GALLEY WHILE IN FLIGHT. THE SMOKE CEASED AFTER USING A HALON AND WATER FIRE EXTINGUISHER AND PULLING THE CIRCUIT BREAKERS FOR THE RIGHT AND LEFT FORWARD OVENS. THE FLIGHT WAS CONTINUED WITHOUT FUR
- [SDR CAL960371](https://openairdocs.org/sdr/CAL960371.md): T3 Blade · broken · Mar 19, 1996 · N76823 · Doug DC982 · Turbine Section
  > THE AIRCRAFT REJECTED TAKEOFF AT HIGH SPEED AFTER THE NR 2 ENGINE FAILED. THE ENGINE FAILURE WAS ACCOMPANIED BY A LOUD POP AND LOW N1. MAINTENANCE FOUND BLADES MISSING FROM COMPRESSOR WITH HEAVY DAMAGE TO TURBINE. THE NR 2 ENGINE WILL BE REMOVED AND REPLACE
- [SDR CAL960305](https://openairdocs.org/sdr/CAL960305.md): Csd Splines · damaged · Mar 12, 1996 · N76823 · Doug DC982 · Alternator-Generator Drive
  > MSY - FLT 1783 - THE LT GENERATOR TRIPPED OFF WHILE EN ROUTE FROM DCA TO IAH. ACFT DESCENDED TO FL 240 AND CREW MADE AN UNSUCCESSFUL ATTEMPT TO START APU. AT THAT TIME, DC EMERGENCY BUS C/B POPPED AND CAPT'S INSTRUMENTS WENT OFF. CIRCUIT BREAKER WAS NOT RES
- [SDR CAL951037](https://openairdocs.org/sdr/CAL951037.md): Retract Mech · malfunctioned · Nov 12, 1995 · N76823 · Doug DC982 · Landing Gear Retraction/Extension System
  > ANC - FLT 0662 - THE LANDING GEAR RED UNSAFE LIGHTS AND THE GEAR DOOR OPEN LIGHT REMAINED ILLUMINATED WITH LANDING GEAR NOISE AND VIBRATION AFTER THE GEAR HANDLE WAS RAISED DEPARTING ANC. CYCLING THE GEAR TWICE DID NOT HELP. THE AIRCRAFT WAS RETURNED TO ANC

## 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 = 'N76823' AND deregistration_id = 'N76823-2005-09-06'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N76823-2005-09-06/reports

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