# Service difficulty reports: N563AU, cancelled Aug 16, 2007

A list on [N563AU, cancelled Aug 16, 2007](https://openairdocs.org/deregistered/N563AU-2007-08-16.md).

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

Page 1 of 2 · 53 reports

- [SDR COOSDR060032](https://openairdocs.org/sdr/COOSDR060032.md): Rib · cracked · Aug 24, 2006 · N563AU · Boeing 737301 · Wing, Rib/Bulkhead
  > RT WING AT WBL 114 RIB UPPER CHORD CRACKED NEAR STR-2. (K)
- [SDR SB05062](https://openairdocs.org/sdr/SB05062.md): Charger · inoperative · May 19, 2005 · N563AU · Boeing 737301 · Emergency Lighting
  > CLT - MAINTENANCE REPORTED THE EMERGENCY LIGHTS FOR SEAT ROWS 11 THROUGH 16 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD.
- [SDR SB05017](https://openairdocs.org/sdr/SB05017.md): Wire · faulty · Jan 27, 2005 · N563AU · Boeing 737301 · Light System Wiring
  > PVD - MAINTENANCE REPORTED THE EMERGENCY LIGHTS WOULD NOT SHUTOFF. MAINTENANCE REPAIRED WIRING AT THE EMERGENCY LIGHT CIRCUIT BREAKER ON THE P-18 PANEL. OPERATIONAL CHECK GOOD.
- [SDR SB04158](https://openairdocs.org/sdr/SB04158.md): Indicator · faulty · Nov 25, 2004 · N563AU · Boeing 737301 · Trailing Flap Position Indicating System
  > DURING APPROACH TO PHL FROM ORD, CREW EXPERIENCED A FLAP DISAGREEMENT WHEN FLAP HANDLE WAS PLACED BEYOND 15 UNITS. A FLAP SPLIT WAS CLEARLY INDICATED. NO ROLL FORCES WERE FELT. AN EMERGENCY WAS DECLARED AND EQUIPMENT WAS CALLED OUT. FLIGHT LANDED WITHOUT I
- [SDR USAASB04114](https://openairdocs.org/sdr/USAASB04114.md): Power Supply · inoperative · Aug 30, 2004 · N563AU · Boeing 737301 · Emergency Lighting
  > BOS - PILOT REPORTED THE COCKPIT EMERGENCY EXIT LIGHT IS INOPERATIVE. MAINTENANCE REPAIRED EMERGENCY LIGHT IN COCKPIT AND REMOVED AND REPLACED POWER SUPPLY. OPERATIONAL CHECK GOOD. (M)
- [SDR USA2004F00071](https://openairdocs.org/sdr/USA2004F00071.md): Wire · broken · Jun 8, 2004 · N563AU · Boeing 737301 · Light System Wiring
  > MAINTNANCE REPORTED THE EMERGENCY LIGHT AT ROW 9 INOPERATIVE. MAINTENANCE REPLACED A BROKEN WIRE. OPERATIONAL CHECK GOOD.
- [SDR USA2004F00080](https://openairdocs.org/sdr/USA2004F00080.md): Shuttle Valve · faulty · Jun 5, 2004 · N563AU · Boeing 737301 · Hydraulic System, Main
  > ENROUTE, CREW REPORTED THE ELEVATOR FEEL WAS VERY HARD IN FLIGHT. ON APPROACH, VERY HEAVY NOSE DOWN PRESSURE IS REQUIRED TO GET A MINIMAL NOSE DOWN RESPONSE. ON LANDING NOT AS MUCH EFFORT WAS REQUIRED. AC WAS FOUND IN SAFE CONDITION FOR MAINT FERRY FLIGHT.
- [SDR USA2004F00078](https://openairdocs.org/sdr/USA2004F00078.md): Control System · malfunctioned · Jun 5, 2004 · N563AU · Boeing 737301 · Elevator Control System
  > ENROUTE, CREW REPORTED THE ELEVATOR FEEL WAS VERY HARD IN FLIGHT. ON APPROACH, VERY HEAVY NOSE DOWN PRESSURE IS REQUIRED TO GET A MINIMAL NOSE DOWN RESPONSE. ON LANDING, NOT AS MUCH EFFORT WAS REQUIRED. AIRCRAFT WAS FOUND IN SAFE CONDITION FOR MAINTENANCE F
- [SDR USAA040116](https://openairdocs.org/sdr/USAA040116.md): Skin · cracked · Apr 7, 2004 · N563AU · Boeing 737301 · Fuselage Main, Plate/Skin
  > CLT - FOUND SKIN CRACKED.700 INCH, 3 INCHES AFT OF FS 727D ADJACENT OT S23R. INSTALLED DOUBLER PER SRM 53-00-01. (M)
- [SDR USAASB03179](https://openairdocs.org/sdr/USAASB03179.md): Control Column · stiff · Oct 12, 2003 · N563AU · Boeing 737301 · Control Column Section
  > EN ROUTE FROM CLT TO RDU, CREW REPORTED STIFF FLIGHT CONTROLS, ELEVATOR AND AILERONS. FEELS SOMEWHAT LIKE MANUAL REVERSION. DURING FLARE ON FINAL, THE CONTROL COLUMN BOUND FOR A MOMENT AND THEN BROKE FREE. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANC
- [SDR USAASB03149](https://openairdocs.org/sdr/USAASB03149.md): Charger · inoperative · Aug 24, 2003 · N563AU · Boeing 737301 · Emergency Lighting
  > MAINTENANCE REPORTED THE EMERGENCY LIGHTS AT SEAT ROW 10ABC AND THE LEFT EMERGENCY EXIT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE CHARGER ASSEMBLY AND THE BATTERY PACK, P/N 2013-1A. OPS CHECK GOOD. (M)
- [SDR USAASB03143](https://openairdocs.org/sdr/USAASB03143.md): Battery Pack · inoperative · Aug 22, 2003 · N563AU · Boeing 737301 · Emergency Lighting
  > MAINTENANCE REPORTED THE LEFT EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M)
- [SDR USAASB03137](https://openairdocs.org/sdr/USAASB03137.md): Battery Pack · inoperative · Aug 13, 2003 · N563AU · Boeing 737301 · Emergency Lighting
  > ATL - MAINTENANCE REPORTED THE LOW LEVEL EMERGENCY EXIT LIGHTING, AT THE LEFT OVERWING EXIT, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AT THE LEFT OVERWING EXIT POSITION. OPERATIONAL CHECK GOOD. (M)
- [SDR USAASB03121](https://openairdocs.org/sdr/USAASB03121.md): Charger · inoperative · Jul 26, 2003 · N563AU · Boeing 737301 · Emergency Lighting
  > PILOT REPORTED THE RIGHT OVERHEAD EMERGENCY EXIT SIGN, THE LEFT OVERWING EXIT SIGN, THE LEFT SIDEWALL EXIT SIGN AT ROW 10 AISLE EXIT AND THE EMERGENCY LIGHTS AT ROW 14 DEF GRAB RAIL LIGHTS INTERMITTENTLY ILLUMINATE WITH EMERGENCY LIGHTS ARMED AND EXTINGUISH FI
- [SDR USAASB02168](https://openairdocs.org/sdr/USAASB02168.md): Battery Pack · discharged · Sep 7, 2002 · N563AU · Boeing 737301 · Emergency Lighting
  > GSO - MAINTENANCE FOUND EMERGENCY EXIT LIGHTS INOPERATIVE AT THE LEFT ESCAPE HATCH FLOOR LEVEL, SEAT ROW 10 LEFT SIDE AND THE BULLNOSE LIGHT AT SEAT ROW 15 RIGHT SIDE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M)
- [SDR USAASB02085](https://openairdocs.org/sdr/USAASB02085.md): Relief Valve · failed · Apr 27, 2002 · N563AU · Boeing 737301 · Cabin Pressure Control System
  > CLT - FLT 384 - ON CLIMB-OUT FROM TPA, CREW REPORTED AN AUTO FAIL LIGHT AND THE CABIN ALTITUDE CLIMBING AT 4000 FPM. STANDBY MODE HAD NO EFFECT. FLIGHT DESCENDED TO 10,000 FEET AND DIVERTED TO CLT. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLAC
- [SDR USAA020113](https://openairdocs.org/sdr/USAA020113.md): Skin · cracked · Mar 21, 2002 · N563AU · Boeing 737301 · Fuselage Main, Plate/Skin
  > TPA - FOUND SKIN CRACKED 2 FT BY 3 FT DOUBLER INSTALLED, CROWN SKIN DIRECTLY BELOW DORSAL FIN SEAL STATION 1000. INSTALLED NEW DOUBLER PER WORK INSTRUCTIONS OF EA AND ENG USING DOUBLER AND TRIPLER PER EA 67346B. (M)
- [SDR USAA020112](https://openairdocs.org/sdr/USAA020112.md): Skin · worn · Mar 21, 2002 · N563AU · Boeing 737301 · Fuselage Main, Plate/Skin
  > TPA - FOUND SKIN WITH WORN AREA, FUSELAGE CROWN STATION 1000, DORSAL FIN CONTACT. INSTALLED DOUBLER AND TRIPLER PER EA 86014A. (M)
- [SDR USAASB01129](https://openairdocs.org/sdr/USAASB01129.md): Proximity Sensor · failed · May 7, 2001 · N563AU · Boeing 737301 · Landing Gear Position and Warning
  > CLT - FLT 1670 - AFTER TAKEOFF FROM SAV, EN ROUTE TO CLT, CREW ATTEMPTED TO RAISE THE LANDING GEAR HANDLE BUT THE HANDLE WOULD NOT MOVE MORE THAN HALFWAY UP. AFTER FLAPS WERE UP, GEAR WARNING HORN STOPPED SOUNDING. CREW DID NOT ATTEMPT OVER-RIDE BUT ELECTED
- [SDR USAASB00251](https://openairdocs.org/sdr/USAASB00251.md): Acm · overserviced · Sep 11, 2000 · N563AU · Boeing 737301 · Cabin Cooling System
  > PIT - FLT 9228 - AFTER TAKEOFF, CLIMBING THROUGH 2,000 FEET, CREW NOTICED AN INCREASING OILY SMELL IN THE FLIGHT COMPARTMENT. ODOR SEEMED TO BE MORE OILY THAN ELECTRICAL RELATED. NORMAL ENGINE READINGS AND PACK INDICATIONS WERE NOTED. CREW DONNED THEIR OXYG
- [SDR USAASB00242](https://openairdocs.org/sdr/USAASB00242.md): Switch · faulty · Sep 2, 2000 · N563AU · Boeing 737301 · Leading Edge Slat Control System
  > PHL - FLT 663 - AFTER TAKEOFF FROM PHL, AT 1,500 FEET, CREW TRIED TO RETRACT FLAPS AND SLAT DISAGREEMENT LIGHTS ON PEDESTAL AND OVERHEAD PANEL ILLUMINATED. CREW ACCOMPLISHED QUICK REFERENCE HANDBOOK PROCEDURES BUT PROBLEM REOCCURRED. CAPTAIN ADVISED THAT VIS
- [SDR USAA000786](https://openairdocs.org/sdr/USAA000786.md): Skin · cracked · Jun 5, 2000 · N563AU · Boeing 737301 · Fuselage Main, Plate/Skin
  > CLT - FOUND SKIN CRACKED.250 INCH, LEFT C/D WINDOW POST. INSTALLED DOUBLER PER EA 67382. (M)
- [SDR USAA000769](https://openairdocs.org/sdr/USAA000769.md): Stiffener · corroded · May 31, 2000 · N563AU · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - FOUND STIFFENER CORRODED 1 INCH BY 1 INCH, NOSE W/W STIFFENER BS 235.8, RBL 10. INSTALLED REPAIR ANGLE PER SRM 51-70-12. CORROSION LEVEL 1. (M)
- [SDR USAA000770](https://openairdocs.org/sdr/USAA000770.md): Floorbeam · corroded · May 31, 2000 · N563AU · Boeing 737301 · Fuselage Main, Floor Beam
  > CLT - FOUND FLOORBEAM CORRODED 1 INCH, STATION 312, LBBL 1 PLUS 8. FABRICATED ANGLES AND INSTALLED PER SRM 53-10-51. CORROSION LEVEL 2. (M)
- [SDR USAA000771](https://openairdocs.org/sdr/USAA000771.md): Angle · cracked · May 31, 2000 · N563AU · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - FOUND Q-3 CHECK, FOUND Z-ANGLE CRACKED 2 INCHES, LEFT AFT ENTRY DOOR THRESHOLD. REPAIRED PER SRM 51-10-2. (M)
- [SDR USAA000772](https://openairdocs.org/sdr/USAA000772.md): Floorbeam · corroded · May 31, 2000 · N563AU · Boeing 737301 · Fuselage Main, Floor Beam
  > CLT - FOUND FLOORBEAM CORRODED 2 INCHES, 328 FLOORBEAM, RBBL 36 TO 38. REPLACED T-CAP PER SRM 53-10-51 FIG 205. CORROSION LEVEL 2. (M)
- [SDR USAA000759](https://openairdocs.org/sdr/USAA000759.md): Skin · cracked · May 31, 2000 · N563AU · Boeing 737301 · Fuselage Main, Plate/Skin
  > CLT - FOUND SKIN CRACKED 1 INCH IN TWO PLACES, BS 178, WL 199 AND 202 AT RBL 5. INSTALLED REPAIR ANGLE PER TR 53-10-07. (M)
- [SDR USAA000760](https://openairdocs.org/sdr/USAA000760.md): Intercostal · cracked · May 31, 2000 · N563AU · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - FOUND INTERCOSTAL CRACKED 1 INCH, STATION 291.5 AND STATION 270 BETWEEN STRINGER 11 AND 12R. INSTALLED NEW FABRICATED PART PER SRM 51-30-2. (M)
- [SDR USAA000761](https://openairdocs.org/sdr/USAA000761.md): Door Frame · cracked · May 31, 2000 · N563AU · Boeing 737301 · Fuselage Main, Structure
  > CLT - FOUND DOOR FRAME CRACKED.25 INCH, STATION 294.5 INBOARD SIDE OF R-1 DOOR FRAME. INSTALLED DOUBLER PER SRM 51-70-11. (M)
- [SDR USAA000762](https://openairdocs.org/sdr/USAA000762.md): Frame · cracked · May 31, 2000 · N563AU · Boeing 737301 · Fuselage Main, Structure
  > CLT - FOUND FORWARD SERVICE DOOR FRAME CRACKED.75 INCH, STATION 294.5, WL 207.5. INSTALLED REPAIR ANGLE PER SRM 53-10-02. (M)
- [SDR USAA000763](https://openairdocs.org/sdr/USAA000763.md): Tie Clip · cracked · May 31, 2000 · N563AU · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - FOUND TIE CLIP CRACKED.5 INCH, BS 727C, STRINGER 4L. REPLACED TIE CLIP PER SRM 51-10-02. (M)
- [SDR USAA000764](https://openairdocs.org/sdr/USAA000764.md): Tie Clip · cracked · May 31, 2000 · N563AU · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - FOUND TIE CLIP CRACKED.5 INCH, BS 727D, STRINGER 4L. REPLACED TIE CLIP PER SRM 51-10-02. (M)
- [SDR USAA000765](https://openairdocs.org/sdr/USAA000765.md): Frame · cracked · May 31, 2000 · N563AU · Boeing 737301 · Fuselage Main, Frame
  > CLT - FOUND FRAME CRACKED.5 INCH, STATION 807, RIGHT BIN RAIL ATTACH STRINGER 8 TO 9. INSTALLED DOUBLER PER TR 53-10-14. (M)
- [SDR USAA000766](https://openairdocs.org/sdr/USAA000766.md): Track · cracked · May 31, 2000 · N563AU · Boeing 737301 · Fuselage, Seat/Cargo Attach Fittings
  > CLT - FOUND O/H BIN RAIL CRACKED.5 INCH, STATION 827, LEFT O/H BIN RAIL ATTACH STRINGER 8 TO 9. INSTALLED DOUBLER PER TR 53-10-14A. (M)
- [SDR USAA000767](https://openairdocs.org/sdr/USAA000767.md): Frame · cracked · May 31, 2000 · N563AU · Boeing 737301 · Fuselage Main, Frame
  > CLT - FOUND FRAME CRACKED.25 INCH, STATION 847, LT O/H BIN RAIL ATTACH STRINGER 8 TO 9. INSTALLED DOUBLER PER TR 53-10-14A. (M)
- [SDR USAA000768](https://openairdocs.org/sdr/USAA000768.md): Frame · cracked · May 31, 2000 · N563AU · Boeing 737301 · Fuselage Main, Frame
  > CLT - FOUND FRAME CRACKED.5 INCHES, STATION 908, RIGHT O/H BIN ATTACH RAIL STRINGER 8 TO 9. FABRICATED DOUBLER PER TR 53-10-14A. (M)
- [SDR USAA000757](https://openairdocs.org/sdr/USAA000757.md): Skin · cracked · May 31, 2000 · N563AU · Boeing 737301 · Fuselage Main, Plate/Skin
  > CLT - FOUND SKIN CRACKED 1 INCH IN TWO PLACES, BS 178, WL 199 AND 202 AT LBL 5. INSTALLED REPAIR ANGLE PER TR 53-10-07. INSTALLED REPAIR ANGLE PER TR 53-10-07. (M)
- [SDR USAA000758](https://openairdocs.org/sdr/USAA000758.md): Skin · cracked · May 31, 2000 · N563AU · Boeing 737301 · Fuselage Main, Plate/Skin
  > CLT - FOUND SKIN CRACKED 1 INCH IN TWO PLACES, BS 178, WL 190, LBL 1 AND RBL 1. INSTALLED REPAIR ANGLE PER TR 53-10-08. (M)
- [SDR USAA000737](https://openairdocs.org/sdr/USAA000737.md): Floorbeam · corroded · May 24, 2000 · N563AU · Boeing 737301 · Fuselage Main, Floor Beam
  > CLT - FOUND FLOORBEAM CORRODED 1 INCH, RBBL 0, 9 AND 12 FLOORBEAM. INSTALLED NEW T-CAP PER SRM 53-10-57. CORROSION LEVEL 2. (M)
- [SDR USAA000732](https://openairdocs.org/sdr/USAA000732.md): Fitting · cracked · May 23, 2000 · N563AU · Boeing 737301 · Main Landing Gear Attach Section
  > CLT - FOUND FITTING CRACKED.375 INCH, LEFT MLG SUPPORT FITTING REAR SPAR WALKING BEAM. REPAIRED PER TR 57-40-13. (M)
- [SDR USAA000731](https://openairdocs.org/sdr/USAA000731.md): Skin · cracked · May 23, 2000 · N563AU · Boeing 737301 · Fuselage Main, Plate/Skin
  > CLT - FOUND SKIN CRACKED.375 INCH, KEEL BEAM SKIN STATION 661-727, TWO PLACES. INSTALLED FABRICATED DOUBLER PER SRM 53-60-12 FIG 202. (M)
- [SDR USAA000713](https://openairdocs.org/sdr/USAA000713.md): Splice · cracked · May 15, 2000 · N563AU · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - FOUND SPLICE STRINGER CRACKED.125 INCH, BS 908 STRINGER 4L SPLICE PLATE. INSTALLED NEW SPLICE AND TIE CLIP PER SRM 51-10-2. (M)
- [SDR USAA000526](https://openairdocs.org/sdr/USAA000526.md): Support Bracket · cracked · Mar 30, 2000 · N563AU · Boeing 737301 · Fuselage Miscellaneous Structure
  > PIT- FOUND SUPPORT BRACKET CRACKED 2 INCHES, STATION 727D-727E STRINGER NR 1 A/C CENTER LINE NR 3 VHF. DEFECTIVE PART REPLACED WITH IDENTICAL PART NUMBER. (M)
- [SDR USAASB00058](https://openairdocs.org/sdr/USAASB00058.md): Battery Pack · inoperative · Mar 3, 2000 · N563AU · Boeing 737301 · Emergency Lighting
  > CLT - MAINTENANCE FOUND THE AFT RIGHT SERVICE DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK NORMAL. (M0
- [SDR USAASB99279](https://openairdocs.org/sdr/USAASB99279.md): Controller · failed · Nov 26, 1999 · N563AU · Boeing 737301 · Cabin Pressure Controller
  > PHL - FLT 435 - EN ROUTE FROM BTV TO PHL, AT FL260, THE CABIN ALTITUDE WARNING HORN SOUNDED. CREW VERIFIED CABIN ALTITUDE READING AT 10,000 FT. CREW COMPLIED WITH ABNORMAL PROCEDURES AND ACCOMPLISHED A STEEP DESCENT TO FL120. NO OXYGEN MASKS WERE DEPLOYED.
- [SDR USAASB99178](https://openairdocs.org/sdr/USAASB99178.md): Tr Unit · malfunctioned · Jul 19, 1999 · N563AU · Boeing 737301 · Weather Radar System
  > BWI - FLT 0166 - DURING CRUISE, EN ROUTE PHX/PHL, THE WEATHER RADAR BECAME UNRELIABLE. TEST PAGE SHOWED 'R/T FAULT' FOLLOWED BY 'NO WXR'. SYSTEM WORKED FINE INITIALLY. FLIGHT DIVERTED TO BWI AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE OPERATIONALLY CH
- [SDR USAASB98289](https://openairdocs.org/sdr/USAASB98289.md): Lock Actuator · failed · Oct 29, 1998 · N563AU · Boeing 737301 · Landing Gear Retraction/Extension System
  > CLT - FLT 984 - AFTER TAKEOFF WITH GEAR LEVER IN THE UP POSITION, THE RED NOSE GEAR WARNING LIGHT ILLUMINATED. GEAR APPEARED TO BE UP. WHEN GEAR LEVER WAS PLACED TO THE OFF POSITION, NOSE GEAR DROPPED TO THE EXTEND POSITION. FLIGHT LANDED WITHOUT FURTHER IN
- [SDR USAASB98208](https://openairdocs.org/sdr/USAASB98208.md): Control Valve · failed · Aug 13, 1998 · N563AU · Boeing 737301 · Cabin Pressure Control System
  > DEN - FLT 136 - CREW WAS UNABLE TO PRESSURIZE AIRCRAFT UPON CLIMB-OUT FROM DEN. FLIGHT RETURNED TO FIELD AT DEN AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE LEFT PACK FLOW CONTROL VALVE. OPERATIONAL C
- [SDR USAASB98135](https://openairdocs.org/sdr/USAASB98135.md): Turbofan · failed · Jun 2, 1998 · N563AU · Boeing 737301 · Cabin Pressure Control System
  > PIT - FLT 1597 - CREW WAS UNABLE TO PRESSURIZE AIRCRAFT AFTER TAKEOFF FROM PIT. FLIGHT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE RIGHT TURBOFAN AND THE LEFT MIXING CONTROL VALVE AS
- [SDR 98ZZZM533](https://openairdocs.org/sdr/98ZZZM533.md): Control Valve · failed · Jun 2, 1998 · N563AU · Boeing 737301 · Cabin Pressure Control System
  > PIT - FLT 1597 - CREW WAS UNABLE TO PRESSURIZE AIRCRAFT AFTER TAKEOFF FROM PIT. FLIGHT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE RIGHT TURBOFAN AND THE LEFT MIXING CONTROL VALVE AS

Next page: https://openairdocs.org/deregistered/N563AU-2007-08-16/reports.md?page=2

## 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 = 'N563AU' AND deregistration_id = 'N563AU-2007-08-16'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N563AU-2007-08-16/reports

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