# Service difficulty reports: N806US, cancelled Jul 29, 2013

A list on [N806US, cancelled Jul 29, 2013](https://openairdocs.org/deregistered/N806US-2013-07-29.md).

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

- [SDR USAAD01077](https://openairdocs.org/sdr/USAAD01077.md): Light · failed · Apr 5, 2001 · N806US · Doug DC981 · Emergency Lighting
  > IND - THE MAIN ENTRY DOOR WALK-AROUND AND THE LOW LEVEL EMERGENCY LIGHTS AT THE FORWARD SERVICE DOOR AND SEAT ROW 11 WERE INOPERATIVE. THE AFT LOW LEVEL EMERGENCY LIGHT RECEIVER WAS INOPERATIVE. MAINTENANCE REPLACED THE MAIN ENTRY DOOR WALK-AROUND LIGHT ASSE
- [SDR USAAD01037](https://openairdocs.org/sdr/USAAD01037.md): Battery · discharged · Feb 20, 2001 · N806US · Doug DC981 · Emergency Lighting
  > IND - THE CEILING EMERGENCY LIGHTS BETWEEN THE AFT LAVATORIES WERE INOPERATIVE. REPLACED BATTERIES AT B5-27 IN THE RIGHT LAVATORY CEILING. (M)
- [SDR USAAD00154](https://openairdocs.org/sdr/USAAD00154.md): Relay · stuck · Sep 27, 2000 · N806US · Doug DC981 · Stabilizer Control System
  > PIT-FLL - FLT 1221 - OUT OF 10,000 FEET, THE AUTOPILOT WAS ENGAGED AND OPERATION WAS NORMAL FOR 2-3 MINUTES BEFORE THE AIRCRAFT NOSED DOWN. THE AUTOPILOT WAS DISENGAGED AND THE AIRCRAFT WAS RE-TRIMMED TO NORMAL FLIGHT. AT 26,000 FT, THE AUTOPILOT WAS AGAIN E
- [SDR USAAD00034](https://openairdocs.org/sdr/USAAD00034.md): Power Supply · failed · Feb 26, 2000 · N806US · Doug DC981 · Emergency Lighting
  > TPA - THE LEFT AND RIGHT OVERWING EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE OVERWING EMERGENCY LIGHT POWER SUPPLIES. (M)
- [SDR USAAD99107](https://openairdocs.org/sdr/USAAD99107.md): Battery · discharged · Jul 30, 1999 · N806US · Doug DC981 · Emergency Lighting
  > PHL - THE TAIL AREA EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY FOR THE TAIL AREA EMERGENCY LIGHTS. (M)
- [SDR USAA990794](https://openairdocs.org/sdr/USAA990794.md): Skin · cracked · Jul 22, 1999 · N806US · Doug DC981 · Wing, Plate/Skin
  > PIT - DURING Q5/C2 CHECK, FOUND 2.375 INCH CRACK AT LOWER LEFT WING FIXED LEADING EDGE XFS 343. INSTALLED DOUBLERS PER EA 52330. (M)
- [SDR USAA990741](https://openairdocs.org/sdr/USAA990741.md): Doubler · cracked · Jul 22, 1999 · N806US · Doug DC981 · Wing Miscellaneous Structure
  > PIT - DURING Q5/C2 CHECK FOUND 2 INCH CRACK AT LEFT WING PRODUCTIONS SPLICE DOUBLER STATION XFS 196.236. REPLACED DOUBLER (SPLICE) AND ADDED STRAPS PER SRM 57-06B (FIGURE 9). (M)
- [SDR USAAD98189](https://openairdocs.org/sdr/USAAD98189.md): O-Ring · failed · Oct 22, 1998 · N806US · Doug DC981 · Engine Thrust Reverser
  > CLT-TPA - FLT 1816 - DURING CRUISE THE LEFT HYDRAULIC QUANTITY LOW LIGHT ILLUMINATED. THE AIRCRAFT DIVERTED TO SAV AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED AN O-RING ON THE LEFT THRUST REVERSER CONTROL VALVE. (M)
- [SDR USAAD98129](https://openairdocs.org/sdr/USAAD98129.md): Sensor · out of adjust · Jul 30, 1998 · N806US · Doug DC981 · Door Warning System
  > PIT - FLT 2032 - AFTER TAKEOFF, THE FORWARD CARGO DOOR CAUTION LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE FORWARD CARGO DOOR WARNING SENSOR TARGET SLIGHTLY OUT OF POSITION. THE TARGET WAS STRAIGH
- [SDR USAAD98072](https://openairdocs.org/sdr/USAAD98072.md): Filter · failed · Apr 26, 1998 · N806US · Doug DC981 · Turbine Engine Oil System
  > MCO - FLT 1445 - EN ROUTE CLT/ MIA, CREW RECEIVED THE RIGHT ENGINE OIL CLOG LIGHT. CREW REDUCED POWER TO IDLE AND THE LIGHT REMAINED ILLUMINATED. FLIGHT DIVERTED TO MCO AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND THE OIL FILTER PAPERS WERE SEPARA
- [SDR USAAD97163](https://openairdocs.org/sdr/USAAD97163.md): Engine · failed · Sep 22, 1997 · N806US · Doug DC981 · Engine (Turbine/Turboprop)
  > MCO - FL 1484 - CLIMBING THROUGH 3000 FT, CREW RECEIVED THE NR 1 ENGINE OIL STRAINER CLOG LIGHT. CREW REDUCED POWER ON THE NR 1 ENGINE. FLIGHT RETURNED TO MCO AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND THE NR 1 ENGIEN 'MAKING METAL' AND REPLACED
- [SDR USAAD97122](https://openairdocs.org/sdr/USAAD97122.md): Batteries · discharged · Jul 15, 1997 · N806US · Doug DC981 · Emergency Lighting
  > ROC - FOUND FORWARD SECTION OF EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES IN POWER SUPPLY. (M)
- [SDR USAAD97024](https://openairdocs.org/sdr/USAAD97024.md): Battery Pack · discharged · Jan 28, 1997 · N806US · Doug DC981 · Emergency Lighting
  > RSW - GALLEY AND COCKPIT EMERGENCY LIGHTS WOULD NOT SHUT OFF. REPLACED BATTERY PACK. (M)
- [SDR USAAD96178](https://openairdocs.org/sdr/USAAD96178.md): Engine · failed · Dec 8, 1996 · N806US · Doug DC981 · Engine (Turbine/Turboprop)
  > FLT 532 - CLT-BDL - AFTER TAKEOFF, CREW HEARD A LOUD BANG, AND NR 2 ENGINE EPR WAS DROPPING. RETURNED TO CLT. A/C WAS FERRIED TO PIT, WHERE NR 2 ENGINE WAS CHANGED. (M)
- [SDR USAAD96040](https://openairdocs.org/sdr/USAAD96040.md): Duct · loose · Apr 21, 1996 · N806US · Doug DC981 · Cabin Cooling System
  > RSW - FL 1028 - AFTER TAKEOFF, CREW RECEIVED MASTER WARNING LIGHT DUE TO THE TAIL HIGH TEMPERATURE SIGNAL. FLIGHT RETURNED TO RSW AND LANDED WITH NO FURTHER INCIDENT. MX FOUND THE DUCTING AT THE WATER SEPARATOR ON THE RIGHT PACK LEAKING. DUCTING WAS SECURED
- [SDR USAAD96035](https://openairdocs.org/sdr/USAAD96035.md): Duct · separated · Mar 31, 1996 · N806US · Doug DC981 · Air Distribution System
  > CAE - FL 256 - EN ROUTE SRQ-CLT, IN THE VICINITY OF CAE, CREW NOTED LOSS OF CABIN PRESSURIZATION. CREW PERFORMED AN EMERGENCY DESCENT TO 10,000 FEET. FLIGHT CONTINUED TO CLT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND AND REPAIRED A SEPARATED DUC
- [SDR USAA950180](https://openairdocs.org/sdr/USAA950180.md): Skin · cracked · Feb 9, 1995 · N806US · Doug DC981 · Vertical Stabilizer, Plate/Skin
  > PIT - DURING Q-4 CHECK, INSPECTION FOUND CRACK.5 INCH AT STA 1408 AND 1429 LT SIDE LONGERON 2 LT DORSAL FIN SKIN. CUT OUT DAMAGE SKIN AND INSTALLED SKIN SPLICE REPAIR PER DACO PER SKETCH 3413J AND EA 29421 AND EO 5388X223. (W)
- [SDR USAA950160](https://openairdocs.org/sdr/USAA950160.md): Beltframe · cracked · Feb 9, 1995 · N806US · Doug DC981 · Fuselage Main, Frame
  > PIT - DURING Q-4 CHECK INSPECTION, FOUND TWO EACH CRACKS BOTH.5 INCH, STA 1418 LONGERON 2 LT BELTFRAME. CUT OUT DAMAGE AREA AND INSTALLED FILLER, DOUBLERS PER SRM 53-03 FIG 32 SHT 4 PG 135. (W)
- [SDR USAA950159](https://openairdocs.org/sdr/USAA950159.md): Tie Dn Track · corrosion · Feb 9, 1995 · N806US · Doug DC981 · Fuselage, Seat/Cargo Attach Fittings
  > PIT - DURING Q-4 CHECK, INSPECTION FOUND CORROSION BETWEEN STA 541 AND 634, LT SIDE TIE DOWN TRACK. INSTALLED REPAIR ANGLES PER TYPICAL REPAIR 53-20-09A. (W)
- [SDR USAA950168](https://openairdocs.org/sdr/USAA950168.md): Skin · cracked · Feb 7, 1995 · N806US · Doug DC981 · Wing, Plate/Skin
  > PIT - DURING Q-4 CHECK, INSPECTION FOUND CRACKS 2 EACH.25 INCH BY.1250 INCH RT WING FUEL PANELS ACCESS DOOR AREA, LEADING EDGE SKIN. STOP DRILLED CRACKS, MFG DOUBLERS AND INSTALLED REPAIR PER SRM 57-06B PAGE 9 FIG 3. (W)
- [SDR USAA950167](https://openairdocs.org/sdr/USAA950167.md): Longeron · cracked · Feb 7, 1995 · N806US · Doug DC981 · Fuselage Main, Longeron/Stringer
  > PIT - DURING Q-4 CHECK, INSPECTION FOUND CRACK.5 INCH STA 1418 LONGERON 2RT. SPLICED IN NEW SECTION OF LONGERON, PER SRM 53-02 FIG 5. (W)
- [SDR USAA950166](https://openairdocs.org/sdr/USAA950166.md): Skin · cracked · Feb 7, 1995 · N806US · Doug DC981 · Fuselage Main, Plate/Skin
  > PIT - DURING Q-4 CHECK, INSPECTION FOUND.52 INCH CRACK STA 1437 BETWEEN LONGERON 2 AND 3 LT, IN SKIN. CUT OUT DAMAGE AND INSTALLED PLUG REPAIR DOUBLER PER SRM 53-04 FIG 38. (W)
- [SDR USAA950179](https://openairdocs.org/sdr/USAA950179.md): Beltframe · cracked · Feb 6, 1995 · N806US · Doug DC981 · Fuselage Main, Frame
  > PIT - DURING Q-4 CHECK, INSPECTION FOUND CRACK.25 INCH STA 446 LONGERON 30 BELTFRAME. INSTALLED REPAIR 'J' ANGLE PLATES PER SRM 53-03 FIG 2A. (W)
- [SDR USAA950177](https://openairdocs.org/sdr/USAA950177.md): Floorbeam · corrosion · Feb 6, 1995 · N806US · Doug DC981 · Fuselage Main, Floor Beam
  > PIT - DURING Q-4 CHECK, INSPECTION FOUND CORROSION LEVEL I AREA PREVIOUSLY REWORKED STA 1322 RT SIDE LAV AREA FLOORBEAM. CORROSION TASK NR C58-53300. CUT OUT DAMAGED AREA, INSTALLED FILLER, REPAIR ANGLES AND DOUBLER. PE SRM 53-05 TYPICAL REPAIR 53-10-19 EA
- [SDR USAA950176](https://openairdocs.org/sdr/USAA950176.md): Floorbeam · corrosion · Feb 6, 1995 · N806US · Doug DC981 · Fuselage Main, Floor Beam
  > PIT - DURING Q-4 CHECK, INSPECTION FOUND CORROSION LEVEL I AREA PREVIOUSLY REWORKED STA 1338 RT LAV AREA FLOORBEAM. CORROSION TASK NR C58-53300. REPLACED TOP ANGLE AND INSTALLED DOUBLER REPAIRS, WEB AND FITTING TYPICAL REPAIR 53-10-14 AND SRM 53-05 FIG 72.
- [SDR USAA950178](https://openairdocs.org/sdr/USAA950178.md): Attach Angle · corrosion · Feb 3, 1995 · N806US · Doug DC981 · Fuselage Miscellaneous Structure
  > PIT - DURING Q-4 CHECK, INSPECTION FOUND CORROSION LEVEL I AREA PREVIOUSLY REWORKED AFT PAC DOOR LOWER THRESHOLD ATTACH ANGLE STA 1338 AT FLOOR PANEL NR 101 ATTACH ANGLE. REMOVED CORROSION AND INSTALLED REPAIR DOUBLER PER SRM 53-05 FIG 34 EA 29474. (W)
- [SDR USAA950175](https://openairdocs.org/sdr/USAA950175.md): Seat Track · worn · Jan 31, 1995 · N806US · Doug DC981 · Fuselage, Seat/Cargo Attach Fittings
  > PIT - DURING Q-4 CHECK, INSPECTION FOUND COCKPIT AND CO-PILOTS AFT SEAT TRACKS WEAR BEYOND LIMITS. REMOVED AND INSTALLED REPAIR KIT PER TYPICAL REPAIR 53-20-06. (W)
- [SDR USAA950173](https://openairdocs.org/sdr/USAA950173.md): Seat Track · corrosion · Jan 31, 1995 · N806US · Doug DC981 · Fuselage, Seat/Cargo Attach Fittings
  > PIT - DURING Q-4 CHECK, INSPECTION FOUND CORROSION BETWEEN STA 332 AND 389 RT I/B SEAT TRACK. SPLICED IN NEW SECTION OF SEAT TRACK PER SRM 53-05 FIG 4. (W)
- [SDR USAA950172](https://openairdocs.org/sdr/USAA950172.md): Seat Track · corrosion · Jan 31, 1995 · N806US · Doug DC981 · Fuselage, Seat/Cargo Attach Fittings
  > PIT - DURING Q-4 CHECK, INSPECTION FOUND CORROSION STA 693 LT SIDE TIE DOWN TRACK. REMOVED CORROSION AND INSTALLED REPAIR STRAPS PER USAIR TYPICAL REPAIR 53-20-09A. (W)
- [SDR USAA950171](https://openairdocs.org/sdr/USAA950171.md): Seat Track · corrosion · Jan 31, 1995 · N806US · Doug DC981 · Fuselage, Seat/Cargo Attach Fittings
  > PIT - DURING Q-4 CHECK, INSPECTION FOUND CORROSION STA 541 RT SIDE TIE DOWN TRACK. REMOVED CORROSION, CLEANED, ALODINE, PRIMED, INSTALLED 'L' ANGLES, PER USAIR TYPICAL REPAIR 53-20-09A. (W)
- [SDR USAA950170](https://openairdocs.org/sdr/USAA950170.md): Skin · lightning strike · Jan 31, 1995 · N806US · Doug DC981 · Fuselage Main, Plate/Skin
  > PIT - DURING Q-4 CHECK, INSPECTION FOUND LIGHTNING STRIKE.375 INCH BY.035 INCH DEEP STA 1172 LONGERON 30 IN SKIN. INSTALLED EXTERNAL DOUBLER, DAMAGE WAS BLENDED. PER SRM 53-04 FIG 38 VIEW G USAIR EA 29390. (W)
- [SDR USAA950169](https://openairdocs.org/sdr/USAA950169.md): Longeron · cracked · Jan 31, 1995 · N806US · Doug DC981 · Fuselage Main, Longeron/Stringer
  > PIT - DURING Q-4 CHECK, INSPECTION FOUND.75 INCH CRACK STA 1309 LONGERON 12 FEET. INSTALLED LONGERON AND SPLICE PER SRM USAIR TYPICAL REPAIR 53-10-17. (W)
- [SDR USAA950165](https://openairdocs.org/sdr/USAA950165.md): Stiffener · cracked · Jan 31, 1995 · N806US · Doug DC981 · Fuselage Miscellaneous Structure
  > PIT - DURING Q-4 CHECK, INSPECTION FOUND 1 INCH CRACK STA 1338 CENTER TOP OF AFT PASS DOCK IN STIFFENER. STOP DRILLED CRACK AND INSTALLED REPAIR ANGLE DOUBLERS PER SRM 53-01 FIG 2 SHEET 4. (W)
- [SDR USAA950164](https://openairdocs.org/sdr/USAA950164.md): Skin · corrosion · Jan 31, 1995 · N806US · Doug DC981 · Fuselage Main, Plate/Skin
  > PIT - DURING Q-4 CHECK, INSPECTION FOUND CORROSION LEVEL I STA 800 BETWEEN LONGERONS 28 RT AND 29 RT SKIN. CORROSION TASK NR C22-57301. INSTALLED DOUBLER PER SRM 53-04 FIG 53. (W)
- [SDR USAA950163](https://openairdocs.org/sdr/USAA950163.md): Skin · corrosion · Jan 31, 1995 · N806US · Doug DC981 · Fuselage Main, Plate/Skin
  > PIT - DURING Q-4 CHECK, INSPECTION FOUND CORROSION LEVEL I STA 823 LONGERON 29 RT, IN SKIN. CORROSION TASK NR C22-57301. INSTALLED DOUBLER PER SRM 53-04 FIG 53. (W)
- [SDR USAA950161](https://openairdocs.org/sdr/USAA950161.md): Skin · dent · Jan 25, 1995 · N806US · Doug DC981 · Fuselage Main, Plate/Skin
  > PIT - DURING Q-4 CHECK, INSPECTION FOUND DENT BEYOND LIMITS.065 INCH DEEP FUSELAGE STA 345 LONGERON 20 RT. CUT OUT DAMAGED SKIN AND INSTALLED PLUG FILLER AND INTERNAL DOUBLER PER SRM 53-04 FIG 38 AND EA 26628 REV B. (W)
- [SDR USAA950174](https://openairdocs.org/sdr/USAA950174.md): Skin · gouged · Jan 24, 1995 · N806US · Doug DC981 · Fuselage Main, Plate/Skin
  > PIT - DURING Q-4 CHECK, INSPECTION FOUND GOUGE.022 INCH IN FUSELAGE LT SIDE STA 229 BETWEEN LONGERON 18L AND 19L SKIN. BLENDED DAMAGED SKIN AND INSTALLED INTERNAL DOUBLER PER SRM 53-04 FIG 38. (W)
- [SDR USAA950162](https://openairdocs.org/sdr/USAA950162.md): Skin · dent · Jan 24, 1995 · N806US · Doug DC981 · Fuselage Main, Plate/Skin
  > DURING Q-4 CHECK, INSPECTION FOUND DENTS BOTH.063 INCH DEEP STA 229, LONGERONS 22 TO 26 LT, IN SKIN. CUT OUT DAMAGE SKIN AND INSTALLED FLUSH REPAIR WITH INTERNAL FINGER DOUBLER. PER SRM 53-04 FIG 26. (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 = 'N806US' AND deregistration_id = 'N806US-2013-07-29'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N806US-2013-07-29/reports

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