# Service difficulty reports: N811US, cancelled Oct 6, 2005

A list on [N811US, cancelled Oct 6, 2005](https://openairdocs.org/deregistered/N811US-2005-10-06.md).

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

- [SDR USAAD02016](https://openairdocs.org/sdr/USAAD02016.md): Battery · discharged · Mar 19, 2002 · N811US · Doug DC981 · Emergency Lighting
  > PIT - THE DOOR EXIT AND NUMEROUS FLOOR LEVEL EMERGENCY LIGHTS WILL NOT TEST. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M)
- [SDR USAAD01184](https://openairdocs.org/sdr/USAAD01184.md): Battery · discharged · Nov 29, 2001 · N811US · Doug DC981 · Emergency Lighting
  > PIT - THE FORWARD OVERWING EXIT LIGHTS DID NOT ILLUMINATE WHEN THE AIRCRAFT POWER DROPPED OFF. MAINTENANCE REPLACED THE EMERGENCY LIGHTS BATTERY. (M)
- [SDR 2001F00647](https://openairdocs.org/sdr/2001F00647.md): Battery · discharged · Oct 26, 2001 · N811US · Doug DC981 · Emergency Lighting
  > MCO - THE SEAT MOUNTED LOW LEVEL EMERGENCY LIGHTS AND THE LEFT FORWARD EXIT IDENTIFIER LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. REF USAAD01176. (M)
- [SDR USAAD01176](https://openairdocs.org/sdr/USAAD01176.md): Battery · discharged · Oct 26, 2001 · N811US · Doug DC981 · Emergency Lighting
  > MCO - THE SEAT MOUNTED LOW LEVEL EMERGENCY LIGHTS AND THE LEFT FORWARD EXIT IDENTIFIER LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M)
- [SDR USAA011128](https://openairdocs.org/sdr/USAA011128.md): Skin · cracked · Aug 21, 2001 · N811US · Doug DC981 · Doors
  > CLT - FOUND SKIN CRACKED, SKIN ON AFT ENTRANCE DOOR L2 AROUND HOLE OPEN HOOK CUTOUT. INSTALLED DOUBLER PER E NR 72317. (M)
- [SDR USAAD01135](https://openairdocs.org/sdr/USAAD01135.md): Battery · discharged · Jul 11, 2001 · N811US · Doug DC981 · Emergency Lighting
  > CLT - THE LOW LEVEL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M)
- [SDR USAAD01115](https://openairdocs.org/sdr/USAAD01115.md): Battery · discharged · May 22, 2001 · N811US · Doug DC981 · Emergency Lighting
  > IND - THE LOW LEVEL EMERGENCY LIGHT FAILED TO TEST AT SEAT ROWS 1, 3, 6 AND 19. THE CEILING EMERGENCY LIGHTS AT SEAT ROWS 1 TO 3 AND THE RIGHT AFT EMERGENCY EXIT LIGHT WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES, (P/N 9721055, AD4002
- [SDR USAAD01090](https://openairdocs.org/sdr/USAAD01090.md): Battery · discharged · Apr 30, 2001 · N811US · Doug DC981 · Emergency Lighting
  > TPA - THE FLOOR TRACK EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M)
- [SDR USAAD01084](https://openairdocs.org/sdr/USAAD01084.md): Slide · unserviceable · Apr 25, 2001 · N811US · Doug DC981 · Escape Slide
  > MCO - THE AFT SERVICE DOOR EVACUATION SLIDE INFLATION BOTTLE PRESSURE WAS LOW. MAINTENANCE REPLACED THE AFT SERVICE DOOR EVACUATION SLIDE. (M)
- [SDR USAAD01086](https://openairdocs.org/sdr/USAAD01086.md): Battery · discharged · Apr 11, 2001 · N811US · Doug DC981 · Emergency Lighting
  > BOS - THE LOW LEVEL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M)
- [SDR USAAD00120](https://openairdocs.org/sdr/USAAD00120.md): Door · open · Jul 29, 2000 · N811US · Doug DC981 · Landing Gear Door Retract Section
  > CLT/BNA - FLT 2288 - ON TAKEOFF THERE WAS A VIBRATION FROM THE NOSE GEAR. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NOSE GEAR DOORS OPEN. THE DOORS WERE INSPECTED AND CLOSED. (X)
- [SDR USAAD99125](https://openairdocs.org/sdr/USAAD99125.md): Seal · failed · Sep 2, 1999 · N811US · Doug DC981 · Cabin Cooling System
  > MKE-CLT - FLT 751 - AFTER TAKEOFF AND CLIMBING THROUGH 17,000 FT THE AIRCRAFT WOULD NOT PRESSURIZE. THE AIRCRAFT DIVERTED TO ORD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED LEFT AIR CYCLE MACHINE AND PERI-SEALS. (M)
- [SDR USAAD99121](https://openairdocs.org/sdr/USAAD99121.md): Battery · discharged · Aug 29, 1999 · N811US · Doug DC981 · Emergency Lighting
  > PIT - THE FORWARD CABIN EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE FORWARD CABIN EMERGENCY LIGHTS BATTERIES. (M)
- [SDR USAAD99085](https://openairdocs.org/sdr/USAAD99085.md): Diode · failed · Jun 22, 1999 · N811US · Doug DC981 · Emergency Lighting
  > THE LOW LEVEL EMERGENCY LIGHTS REMAIN ON WHEN THE AIRCRAFT POWER IS TURNED OFF. MAINTENANCE RPELACED THE DIODE AT TERMINAL STRIP S3-389. (X)
- [SDR USAA990610](https://openairdocs.org/sdr/USAA990610.md): Beltframe · corrosion · Jun 12, 1999 · N811US · Doug DC981 · Fuselage Main, Frame
  > PIT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A 2 INCH AREA OF CORROSION AT STATION 1322 STRINGER 27L TO 27 BELTFRAME. REMOVED AND REPLACED BELTFRAME. (M)
- [SDR USAA990609](https://openairdocs.org/sdr/USAA990609.md): Web · cracked · Jun 12, 1999 · N811US · Doug DC981 · Fuselage Miscellaneous Structure
  > PIT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A 2 INCH CRACK CANTED WEB AT STATION 1463 STRINGER 18R. CUTOUT DAMAGE AND INSTALLED DOUBLER PER TR 53-10-25. (M)
- [SDR USAA990608](https://openairdocs.org/sdr/USAA990608.md): Fitting · cracked · Jun 12, 1999 · N811US · Doug DC981 · Spoilers
  > PIT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 2 INCH CRACK LEFT GROUND SPOILER SUPPORT FITTING LEG UPPER END. INSTALLED PART 5936838-505. (M)
- [SDR USAA990607](https://openairdocs.org/sdr/USAA990607.md): Skin · cracked · Jun 12, 1999 · N811US · Doug DC981 · Fuselage Main, Plate/Skin
  > PIT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A.750 INCH CRACK AT FORWARD UPPER CORNER OF MED DOOR JAMB STATION 168 SKIN. REPAIRED PER SRM 53-05, FIG 26 CUT OUT DAMAGED AREA AND INSTALLED FILLER AND DOUBLER. (M)
- [SDR USAAD96161](https://openairdocs.org/sdr/USAAD96161.md): Csd · failed · Nov 9, 1996 · N811US · Doug DC981 · Alternator-Generator Drive
  > FLT 741 - BWI-CLT - DURING CLIMB, LT CSD LOW OIL PRESSURE LIGHT ILLUMINATED. CAPTAIN BELIEVED CSD DID NOT DISCONNECT. RETURNED TO FIELD. MAINTENANCE FOUND THAT THE CSD FAILED, AND DID IN FACT DISCONNECT. A/C WAS RELEASED PER MEL 24-1A. THE CSD WAS LATER RE
- [SDR USAA950249](https://openairdocs.org/sdr/USAA950249.md): Feeder Cable · chafed · Mar 19, 1995 · N811US · Doug DC981 · AC Generation System
  > PIT - FLT 0992 - ON TAKEOFF, THE RIGHT GENERATOR OFF LIGHT ILLUMINATED FOLLOWED BY AC CROSSTIE LOCKOUT. CREW DECIDED TO RETURN TO PIT. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND STOWED LAV DUMP CABLE CHAFING ON GEN FEEDER CABLE. ACCOMPLISHED REPAIRS
- [SDR USAA950250](https://openairdocs.org/sdr/USAA950250.md): Csd · leaking · Mar 18, 1995 · N811US · Doug DC981 · Alternator-Generator Drive
  > PIT - FLT 0239 - AIRCRAFT RETURNED TO PIT DUE TO A GENERATOR PROBLEM. MAINTENANCE REPLACED THE RIGHT ENGINE CSD AND THE RIGHT ENGINE GENERATOR FOR TROUBLESHOOTING. OPERATIONS CHECKED GOOD. (W)
- [SDR USAA950351](https://openairdocs.org/sdr/USAA950351.md): Skin · dented · Mar 16, 1995 · N811US · Doug DC981 · Fuselage Main, Plate/Skin
  > PIT - DURING Q-2 INSPECTION, FOUND DENT 1 INCH BY 1.75 INCH BY.75 INCH DEEP BETWEEN STATION 275 AND 294 LONGERON 23L AND 27L IN SKIN AREA. INSTALLED DOUBLER REPAIR PER SRM 53-04 SH 17 FIG 38. (W)
- [SDR USAA950347](https://openairdocs.org/sdr/USAA950347.md): Floor Beam · corroded · Mar 16, 1995 · N811US · Doug DC981 · Fuselage Main, Floor Beam
  > PIT - DURING Q-2 INSPECTION, FOUND LEVEL II CORROSION AT STATION 1322 FLOOR BEAM AFT RT LAV. CUT OUT DAMAGED AREA AND INSTALLED FILLER AND REPAIR ANGLE DOUBLERS PER SRM 53-10-19. (W)
- [SDR USAA950346](https://openairdocs.org/sdr/USAA950346.md): Splice · corroded · Mar 16, 1995 · N811US · Doug DC981 · Fuselage Miscellaneous Structure
  > PIT - DURING Q-2 INSPECTION, FOUND LEVEL II CORROSION BETWEEN STATION 1193 AND 1212 LONGERON 29 LEFT. REMOVED AND REPLACED CORRODED SPLICE PER SRM 53-00 FIG 16. (W)
- [SDR USAA950341](https://openairdocs.org/sdr/USAA950341.md): Belt Frame · corroded · Mar 16, 1995 · N811US · Doug DC981 · Fuselage Main, Frame
  > PIT - DURING Q-2 INSPECTION, FOUND LEVEL I CORROSION AT STATION 1309 BETWEEN LONGERON 28L AND 29R ON BELTFRAME 'J'. CLEANED AND TREATED CORRODED AREA AND INSTALLED REPAIR DOUBLER PER SRM 53-03 FIG 7. (W)
- [SDR USAA950339](https://openairdocs.org/sdr/USAA950339.md): Threshold · corroded · Mar 16, 1995 · N811US · Doug DC981 · Fuselage Miscellaneous Structure
  > PIT - DURING Q-2 INSPECTION, FOUND LEVEL I CORROSION AFT CARGO DOOR THRESHOLD AT STATION 1155-1220 WEB AND STRAP. REMOVED AND REPLACED WEB AND STRAP PER DACO DWG NR 5936442. (W)
- [SDR USAA950338](https://openairdocs.org/sdr/USAA950338.md): Web · corroded · Mar 16, 1995 · N811US · Doug DC981 · Fuselage Miscellaneous Structure
  > PIT - DURING Q-2 INSPECTION, FOUND LEVEL I CORROSION AT STATION 1338 AFT CARGO AREA BETWEEN LONGERONS 28L AND 28R. REMOVED CORROSION, CLEANED AND TREATED. INSTALLED REPAIR DOUBLERS PER SRM 53-03 FIG 3 PER USAIR TYPICAL REPAIR 53-30-10. (W)
- [SDR USAA950337](https://openairdocs.org/sdr/USAA950337.md): Door Jamb · corroded · Mar 16, 1995 · N811US · Doug DC981 · Fuselage Miscellaneous Structure
  > PIT - DURING Q-2 INSPECTION, FOUND LEVEL I CORROSION AT FORWARD CARGO DOOR JAMB BETWEEN STATION 370 AND 427. REPLACED PAN AND SPLICED WITH REPAIR DOUBLERS PER SRM 53-05 FIG 44. (W)
- [SDR USAA950336](https://openairdocs.org/sdr/USAA950336.md): Angle · corroded · Mar 16, 1995 · N811US · Doug DC981 · Fuselage Miscellaneous Structure
  > PIT - DURING Q-2 INSPECTION, FOUND LEVEL I CORROSION BETWEEN STATION 180 AND 203 FORWARD GALLEY AREA AND SERVICE DOOR THRESHOLD JAMB PAN, CUSP ANGLE LOWER CORNER OF SERVICE DOOR OPENING. (W)
- [SDR USAA950335](https://openairdocs.org/sdr/USAA950335.md): Membrane · cracked · Mar 15, 1995 · N811US · Doug DC981 · Fuselage Miscellaneous Structure
  > PIT - DURING Q-2 INSPECTION, FOUND A 1.75 INCH CRACK BETWEEN STATION 1287 AND STATION 1309 LEFT SIDE CUSP MEMBRANE. MANUFACTURED NEW SECTION OF CUSP MEMBRANE AND ACCOMPLISHED SPLICE REPAIR PER SRM 53-05 FIG 97. (W)
- [SDR USAA950344](https://openairdocs.org/sdr/USAA950344.md): Skin · corroded · Mar 12, 1995 · N811US · Doug DC981 · Fuselage Main, Plate/Skin
  > PIT - DURING Q-2 INSPECTION, FOUND LEVEL II CORROSION AT STATION 807 LONGERON 29 LEFT SKIN. CLEANED AND TREATED CORRODED AREA AND INSTALLED REPAIR DOUBLER PER SRM 53-04 FIG 53. (W)
- [SDR USAA950343](https://openairdocs.org/sdr/USAA950343.md): Skin · corroded · Mar 12, 1995 · N811US · Doug DC981 · Fuselage Main, Plate/Skin
  > PIT - DURING Q-2 INSPECTION, FOUND LEVEL II CORROSION SKIN AT STATION 769 LONGERON 28 RT. CLEANED AND TREATED CORRODED AREA AND INSTALLED DOUBLER REPAIR PER SRM 53-04 FIG 53. (W)
- [SDR USAA950342](https://openairdocs.org/sdr/USAA950342.md): Beam · corroded · Mar 10, 1995 · N811US · Doug DC981 · Fuselage Miscellaneous Structure
  > PIT - DURING Q-2 INSPECTION, FOUND LEVEL I CORROSION AT STATION 1322 BETWEEN AFT GALLEY AND AFT LAV CENTER AISLE. REMOVED CORRODED AREA AND INSTALLED FILLER AND REPAIR ANGLE PER USAIR TYPICAL REPAIR 53-10-19. (W)
- [SDR USAA950349](https://openairdocs.org/sdr/USAA950349.md): Web · corroded · Mar 9, 1995 · N811US · Doug DC981 · Fuselage Miscellaneous Structure
  > PIT - DURING Q-2 INSPECTION, FOUND LEVEL II CORROSION STATION 1338 RT SIDE UNDER LAV THRESHOLD FLOOR BEAM AREA. CUT OUT DAMAGED SECTION AND INSTALLED DOUBLER PER SRM 53-05 FIG 72. (W)
- [SDR USAA950345](https://openairdocs.org/sdr/USAA950345.md): Splice · corroded · Mar 3, 1995 · N811US · Doug DC981 · Fuselage Miscellaneous Structure
  > PIT - DURING Q-2 INSPECTION, FOUND LEVEL II CORROSION BETWEEN STATION 1193-1212 LONGERON 28L. REMOVED REPLACED SPLICE PER SRM 53-02 FIG 16. (W)
- [SDR USAA950333](https://openairdocs.org/sdr/USAA950333.md): Skin · gouged · Mar 3, 1995 · N811US · Doug DC981 · Vertical Stabilizer, Plate/Skin
  > PIT - DURING Q-2 INSPECTION, FOUND GOUGE RT VERTICAL STAB SKIN PANEL. BURNISHED GOUGES AREA AND INSTALLED INTERNAL DOUBLER PER USAIR EA 29729 AND SRM 55-01 FIG 2 SHEET 2. (W)
- [SDR USAA950329](https://openairdocs.org/sdr/USAA950329.md): Longeron · cracked · Mar 3, 1995 · N811US · Doug DC981 · Fuselage Main, Longeron/Stringer
  > PIT - DURING Q-2 INSPECTION, FOUND.3125 INCH CRACK STATION 160 LONGERON 2 LEFT. CUT OUT DAMAGE SECTION OF LONGERON AND SPLICED IN NEW SECTION PER SRM 53-02 FIG 2. (W)
- [SDR USAA950328](https://openairdocs.org/sdr/USAA950328.md): Longeron · cracked · Mar 3, 1995 · N811US · Doug DC981 · Fuselage Main, Longeron/Stringer
  > PIT - DURING Q-2 INSPECTION, FOUND.25 INCH CRACK STATION 160 LONGERON 3 LEFT. CUT OUT DAMAGED SECTION OF LONGERON AND SPLICED IN NEW SECTION PER SRM 53-02 FIG 2. (W)
- [SDR USAA950348](https://openairdocs.org/sdr/USAA950348.md): Fitting · corroded · Mar 1, 1995 · N811US · Doug DC981 · Fuselage Miscellaneous Structure
  > PIT - DURING Q-2 INSPECTION, FOUND LEVEL II CORROSION AT STATION 1338 RT SIDE UPPER TO LOWER FRAME ATTACH LONGERON 18R CUSP. REMOVED CORROSION, TREATED AND REPLACED FITTING PER DACO PRINT REF NR 5913700. (W)
- [SDR USAA950340](https://openairdocs.org/sdr/USAA950340.md): Skin · corroded · Mar 1, 1995 · N811US · Doug DC981 · Fuselage Main, Plate/Skin
  > PIT - DURING Q-2 INSPECTION, FOUND LEVEL I CORROSION ON FUSELAGE LOWER SKIN BETWEEN 1155 AND 1174. CUT OUT DAMAGED SKIN AND INSTALLED REPAIR WITH EXTERNAL DOUBLER PER SRM 53-04 FIG 12B AND USAIR EA NR 29833. (W)
- [SDR USAA950350](https://openairdocs.org/sdr/USAA950350.md): Intercostal · corroded · Feb 28, 1995 · N811US · Doug DC981 · Fuselage Miscellaneous Structure
  > PIT - DURING Q-2 INSPECTION, FOUND LEVEL II CORROSION REF C58-53301 AT STATION 1344 AFT LEFT GALLEY ATTACHMENT AT FLOOR BEAM 1338 TO AFT PRESSURE BULKHEAD AT FLOOR LEVEL. MANUFACTURED INTERCOSTAL AND REPLACED PER SRM 53-14. (W)
- [SDR USAA950334](https://openairdocs.org/sdr/USAA950334.md): Longeron · cracked · Feb 28, 1995 · N811US · Doug DC981 · Fuselage Main, Longeron/Stringer
  > PIT - DURING Q-2 INSPECTION, FOUND.25 INCH CRACK AT STATION 256 LONGERON 17 LEFT. CUT OUT DAMAGED SECTION AND SPLICED IN NEW SECTION OF LONGERON PER USAIR TYPICAL REPAIR 53-10-17. (W)
- [SDR USAA950331](https://openairdocs.org/sdr/USAA950331.md): Skin · dent · Feb 28, 1995 · N811US · Doug DC981 · Fuselage Main, Plate/Skin
  > PIT - DURING Q-2 INSPECTION, FOUND A 1 INCH BY 100 INCH DEEP DENT AT STATION 408 LONGERON 17 LEFT. INSTALLED INTERNAL DOUBLER PER SRM 53-04 FIG 38 VIEW G. (W)
- [SDR USAA950330](https://openairdocs.org/sdr/USAA950330.md): Membrane · gouge · Feb 28, 1995 · N811US · Doug DC981 · Fuselage Miscellaneous Structure
  > PIT - DURING Q-2 INSPECTION, FOUND GOUGE JUST AFT OF SERVICE DOOR CUSP MEMBRANE STATION 200 LONG 18R. CUT OUT CUSP MEMBRANE SECTION AND INSTALLED REPAIR SECTION PER SRM 53-05 FIG 9. (W)
- [SDR USAA950327](https://openairdocs.org/sdr/USAA950327.md): Longeron · cracked · Feb 28, 1995 · N811US · Doug DC981 · Fuselage Main, Longeron/Stringer
  > PIT - DURING Q-2 INSPECTION, FOUND.1250 INCH CRACK STATION 160 LONGERON 4 LEFT. CUT OUT DAMAGED SECTION AND ACCOMPLISHED SPLICE REPAIR PER SRM 53-02 FIG 02. (W)
- [SDR USAA950332](https://openairdocs.org/sdr/USAA950332.md): Skin · cracked · Feb 24, 1995 · N811US · Doug DC981 · Fuselage Main, Plate/Skin
  > PIT - DURING Q2 INSPECTION, FOUND CRACK.5 INCH LONG STATION 160 FORWARD AIR STAIR CUT OUT UPPER FWD CORNER SKIN. CUT OUT DAMAGED AREA AND INSTALLED FILLER AND EXTERNAL DOUBLER PER SRM 53-05 FIG 57A VIEW G. (W)
- [SDR USAA950326](https://openairdocs.org/sdr/USAA950326.md): Skin · cracked · Feb 24, 1995 · N811US · Doug DC981 · Fuselage Main, Plate/Skin
  > PIT - DURING Q-2 INSPECTION, FOUND.1250 INCH CRACK AT STATION 1437 LONGERON 3L IN SKIN. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER AND FILLER PER SRM 53-04 FIG 38 FIG 38 VIEW L. (W)
- [SDR USAA950325](https://openairdocs.org/sdr/USAA950325.md): Frame · cracked · Feb 24, 1995 · N811US · Doug DC981 · Fuselage Main, Frame
  > PIT - DURING Q-2 INSPECTION, FOUND CRACK.75 INCH LONG AT STATION 1463 CANTED FRAME WEB. CUT OUT DAMAGED SECTION OF WEB AND MANUFACTURED NEW WEB PER USAIR EA 27544. (W)

## 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 = 'N811US' AND deregistration_id = 'N811US-2005-10-06'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N811US-2005-10-06/reports

---
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