# Service difficulty reports: N240AU, cancelled Feb 28, 2017

A list on [N240AU, cancelled Feb 28, 2017](https://openairdocs.org/deregistered/N240AU-2017-02-28.md).

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

- [SDR RYAN20050018](https://openairdocs.org/sdr/RYAN20050018.md): Warning System · activated · Jun 12, 2005 · N240AU · Boeing 737201 · Engine Oil Indicating System
  > DURING CLIMB, ENGINE NR 1 HAD HIGH OIL PRESSURE AND SHORTLY THEREAFTER NR 1 OIL TEMPERATURE STARTED CLIMBING TOWARDS REDLINE. ON RETURN NR 1 ENGINE WAS SHUTDOWN.
- [SDR RYAN200500018](https://openairdocs.org/sdr/RYAN200500018.md): Bulb · faulty · Jun 12, 2005 · N240AU · Boeing 737201 · Engine Oil Temperature
  > DURING CLIMB, ENGINE NR 1 HAD HIGH OIL PRESSURE AND SHORTLY THEREAFTER NR 1 OIL TEMPERATURE STARTED CLIMBING TOWARDS REDLINE. ON RETURN, NR 1 ENGINE SHUTDOWN.
- [SDR 193](https://openairdocs.org/sdr/193.md): Bulb · malfunctioned · Jun 12, 2005 · N240AU · Boeing 737201 · Engine Oil Temperature
  > DURING CLIMB, ENGINE NR 1 HAD HIGH OIL PRESSURE AND SHORTLY THEREAFTER NR 1 OIL TEMPERATURE STARTED CLIMBING TOWARDS REDLINE. ON RETURN, NR 1 ENGINE SHUTDOWN.
- [SDR RYNA200500003](https://openairdocs.org/sdr/RYNA200500003.md): Intercostal · cracked · Jan 17, 2005 · N240AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR BEAM INTERCOSTAL CRACKED AT BS 328 TO 344, LBL 45. REPAIRED CRACKED INTERCOSTAL AT BS 328 TO 344, LBL 45.
- [SDR RYNA200500002](https://openairdocs.org/sdr/RYNA200500002.md): Floorbeam · corroded · Jan 17, 2005 · N240AU · Boeing 737201 · Fuselage Main, Floor Beam
  > MAIN CABIN FLOOR BEAM, UPPER CHORD, UPPER SURFACE CORRODED AT BS 1006, LBL 29. REMOVED CORROSION ON FLOOR BEAM, FABRICATED, TREATED AND INSTALLED REPAIR PARTS.
- [SDR 2004F00170](https://openairdocs.org/sdr/2004F00170.md): Line · leaking · Mar 14, 2004 · N240AU · Boeing 737201 · Hydraulic System, Main
  > DURING CRUISE FROM GSO-ACY, EXPERIENCED A LOSS OF THE A-SYSTEM HYDRAULICS. AN EMERGENCY WAS DECLARED AND AIRCRAFT LANDED AT ACY WITHOUT INCIDENT. REMOVED AND REPLACED NR 2 ENGINE HYDRAULIC FEED LINE. CONDUCTED 'A' SYSTEM TROUBLESHOOTING PROCEDURES FOR PUMP
- [SDR USAASB00177](https://openairdocs.org/sdr/USAASB00177.md): Indicator · failed · Jun 23, 2000 · N240AU · Boeing 737201 · Trailing Flap Position Indicating System
  > CLE - FLT 1231 - ON APPROACH TO CLE, CREW WAS UNABLE TO EXTEND FLAPS. CREW ACCOMPLISHED GO AROUND AND QUICK REFERENCE HANDBOOK PROCEDURES. CREW RECEIVED PARTIAL FLAPS USING ALTERNATE FLAP METHOD. HAD FULL LEADING EDGE DEVICES AND 15 DEGREES FLAPS ON TRAILIN
- [SDR USAASB00169](https://openairdocs.org/sdr/USAASB00169.md): Connector · damaged · Jun 17, 2000 · N240AU · Boeing 737201 · Trailing Flap Position Indicating System
  > IAD - FLT 797 - ON APPROACH TO IAD, THE FLAPS WOULD NOT EXTEND BEYOND 10 DEGREES. CRWE COMPLETED CHECK FOR FLAPS AND FIRST OFFICER WENT BACK INTO CABIN FOR VISUAL CHECK. INDICATOR REMAINED AT 10 DEGREES REGARDLESS OF FLAP HANDLE POSITION. FLIGHT LANDED WITH
- [SDR USAASB00066](https://openairdocs.org/sdr/USAASB00066.md): Light · inoperative · Mar 6, 2000 · N240AU · Boeing 737201 · Emergency Lighting
  > ORD - PILOT REPORTED THE EMERGENCY EVACUATION LIGHT AT SEAT ROW 16 ABC IS INOPERABLE AND THE WIRING UNDER SEAT 16C IS HANGING DOWN. MAINTENANCE REPAIRED WIRING AND RESECURED WIRING UNDER SEAT ROW 16C. OPERATIONAL CHECK OF EMERGENCY LIGHTS GOOD. (X)
- [SDR USAA000196](https://openairdocs.org/sdr/USAA000196.md): Skin · cracked · Feb 15, 2000 · N240AU · Boeing 737201 · Fuselage Main, Plate/Skin
  > CLT - FOUND SKIN CRACKED.5 INCH, BS 765, STRINGER 19R FUSELAGE SKIN. REPAIRED PER SRM 53-30-3 FIG 6. (M)
- [SDR USAASB98156](https://openairdocs.org/sdr/USAASB98156.md): Switch · failed · Jun 25, 1998 · N240AU · Boeing 737201 · Engine Oil Indicating System
  > PHL - FLT 452 - ON CLIMB-OUT FROM PHL, AT APPROX 5,000 FT, THE NR 1 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED. LIGHT REMAINED ON WHEN POWER WAS REDUCED TO IDLE THRUST ON THE NR 1 ENGINE. CREW SHUTDOWN THE NR 1 ENGINE IN FLIGHT AND RETURNED TO FIELD AT PHL W
- [SDR USAASB97327](https://openairdocs.org/sdr/USAASB97327.md): Wire · loose · Nov 28, 1997 · N240AU · Boeing 737201 · Light System Wiring
  > PHL - FLT 461 - PILOT REPORTED THAT THE SEAT LEVEL EMERGENCY EXIT LIGHTS BRIEFLY ILLUMINATED TWICE IN FLIGHT AND EXTINGUISHED ONTHEIR OWN. MAINTENANCE INSPECTED BATTERY PACKS AT ROWS 5, 11 AND 16L AND COULD NOT DUPLICATE FAULT. OPERATIONAL CHECK WAS NORMAL A
- [SDR USAASB97320](https://openairdocs.org/sdr/USAASB97320.md): Battery Pack · discharged · Nov 21, 1997 · N240AU · Boeing 737201 · Emergency Lighting
  > CLT - FLT 596 - PILOT REPORTED, THE OVERHEAD EMERGENCY EXIT LIGHTS WERE INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACKS. OPS CHECK GOOD. (M)
- [SDR USAASB97268](https://openairdocs.org/sdr/USAASB97268.md): Battery Pack · discharged · Sep 28, 1997 · N240AU · Boeing 737201 · Emergency Lighting
  > PHL - FOUND LEFT HAND ENTRY OVERHEAD EMERGENCY LIGHT INOPERABLE; BOTH EMERGENCY SLIDE LIGHTS (FORWARD LEFT) INOPERABLE AND THE LEFT HAND OVERWING EMERGENCY LIGHTS INOPERABLE. MAINTENANCE REPLACED THE BATTERY PACKS. OPERATIONAL CHECK GOOD. (X)
- [SDR USAA970264](https://openairdocs.org/sdr/USAA970264.md): Skin · cracked · Aug 15, 1997 · N240AU · Boeing 737201 · Fuselage Main, Plate/Skin
  > ROA - DURING 'A' CHECK VISUAL INSPECTION, FOUND 3 INCH CRACK IN A/C SKIN, SKIN WAS CRACKED AT STRINGER 24L BETWEEN STATION 924 AND 947. INSTALLED REPAIR DOUBLER, REPAIRED PER SRM 53-30-3. (M)
- [SDR USAA970263](https://openairdocs.org/sdr/USAA970263.md): Stringer · corroded · Aug 15, 1997 · N240AU · Boeing 737201 · Fuselage Main, Longeron/Stringer
  > ROA - DURING 'A' CHECK VISUAL INSPECTION, FOUND CORRODED AREA IN STRINGER 2 INCHES LONG STRINGER 28L, STATION 372. REPLACED DEFECTIVE PORTION OF STRINGER, REPAIRED PER SRM 53-10-3. (M)
- [SDR USAA970262](https://openairdocs.org/sdr/USAA970262.md): Skin · cracked · Aug 15, 1997 · N240AU · Boeing 737201 · Fuselage Main, Plate/Skin
  > ROA - DURING 'A' CHECK VISUAL/EDDY CURRENT INSPECTION, FOUND 1 INCH SKIN CRACK BS 378 BETWEEN BL 0 AND STRINGER 28L. INSTALLED DOUBLER REPAIR, REPAIRED PER TYPICAL REPAIR 53-30-04. (M)
- [SDR USAASB97190](https://openairdocs.org/sdr/USAASB97190.md): Link Assembly · broken · Jul 14, 1997 · N240AU · Boeing 737201 · Landing Gear Door Retract Section
  > RDU - FL 607 - IMMEDIATELY FOLLOWING ROTATION, DURING GEAR RETRACTION, THE FLIGHT CREW HEARD A LOUD BANG NOISE FOLLOWED BY A VERY LOUD RUSH OF AIR. THE FIRST OFFICER OBSERVED AND OBJECT TO GO PAST THE WINDSCREEEN. CREW ASSUMED IT WAS A BIRDSTRIKE AND RETURNE
- [SDR USAASB97158](https://openairdocs.org/sdr/USAASB97158.md): Power Supply · failed · Jun 10, 1997 · N240AU · Boeing 737201 · Emergency Lighting
  > CLT - FL354, EMERGENCY EXIT LIGHTS ON LEFT FORWARD SEATS COME ON DURING FLIGHT AND STAY ON, EVEN IF EMERGENCY EXIT SWITCH IS TURNED OFF. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY AT ROW 11 AND 16. OPERATIONAL CHECK GOOD. (M)
- [SDR USAASB97154](https://openairdocs.org/sdr/USAASB97154.md): Diode · failed · Jun 8, 1997 · N240AU · Boeing 737201 · Emergency Lighting
  > PHL - AFTER ENGINE SHUTDOWN, THE SEAT MOUNTED EMERGENCY LIGHTS ILLUMINATED. MAINTENANCE REPLACED A SYSTEM DIODE. (M)
- [SDR USAASB97153](https://openairdocs.org/sdr/USAASB97153.md): Batteries · discharged · Jun 7, 1997 · N240AU · Boeing 737201 · Emergency Lighting
  > BDL - FOUND FLOOR LEVEL EMERGENCY LIGHTS INOPERATIVE IN FORWARD AND MID CABIN AREAS. MAINTENANCE REPLACED TWO BATTERY PACKS. (M)
- [SDR USAASB97136](https://openairdocs.org/sdr/USAASB97136.md): Lights · malfunctioned · May 22, 1997 · N240AU · Boeing 737201 · Emergency Lighting
  > DCA - FLT 1727 - FLIGHT CREW REPORTED THAT THE EMERGENCY LIGHTS IN THE CABIN ILLUMINATED DURING FLIGHT. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT SWITCH, SEVERAL BATTERY PACKS AND CLEANED THE EMERGENCY EXIT SWITCHES. SYSTEMS OPS CHECK GOOD. (M)
- [SDR USAASB97133](https://openairdocs.org/sdr/USAASB97133.md): Battery · discharged · May 21, 1997 · N240AU · Boeing 737201 · Emergency Lighting
  > CLT - FLT 7900 - DURING TEST FLIGHT AFTER HEAVY MAINTENANCE VISIT, THE LOW LEVEL EMERGENCY EXIT LIGHTS FROM SEAT ROW 7 AND BACK ILLUMINATED. AFTER LANDING, THE AFT MOST LIGHTS WENT OUT. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACKS AT SE
- [SDR USAA970203](https://openairdocs.org/sdr/USAA970203.md): Stringer · corrosion · May 21, 1997 · N240AU · Boeing 737201 · Fuselage Main, Longeron/Stringer
  > INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION AT OUTER AREA OF STRINGER WHERE MATES W/SKIN 15 INCHES LONG BY 1 INCH WIDE, SOME AREAS COMPLETELY THROUGH STRINGER, STATION 360-375 STRINGER 25L. INSTALLED NEW SEGMENT OF STRINGER, REPAIRED PER SRM 53-
- [SDR USAA970202](https://openairdocs.org/sdr/USAA970202.md): Doubler · cracked · May 21, 1997 · N240AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND BELL CRANK CUTOUT DOUBLERS CRACKED STATION 677, RBL 25 AND LBL 25 STATION 677, RBL 25 AND LBL 25. INSTALLED NEW REINFORCEMENTS IN AREA, ACCOMPLISHED EO 5791G632, PART 3B. (M)
- [SDR USAA970201](https://openairdocs.org/sdr/USAA970201.md): Frame · cracked · May 21, 1997 · N240AU · Boeing 737201 · Fuselage Main, Frame
  > INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1.5 INCH CRACK BS 639 STRINGER 16L FRAME. INSTALLED REPAIR PER DRAWING 65C31658. (M)
- [SDR USAA970200](https://openairdocs.org/sdr/USAA970200.md): Skin · cracked · May 21, 1997 · N240AU · Boeing 737201 · Fuselage Main, Plate/Skin
  > INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND.125 INCH AND.25 INCH CRACK LOWER HINGE CUT OUT UPPER AND LOWER CORNERS (FWD ENTRY DOOR) SKIN. INSTALLED DOUBLERS, REPAIRED PER TR 52-10-05. (M)
- [SDR USAA970199](https://openairdocs.org/sdr/USAA970199.md): Skin · cracked · May 21, 1997 · N240AU · Boeing 737201 · Fuselage Main, Plate/Skin
  > INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND.5 INCH CRACK LOWER FORWARD CORNER OF FORWARD CARGO DOOR CUTOUT SKIN. INSTALLED DOUBLER, REPAIRED PER EA 42403. (M)
- [SDR USAA970198](https://openairdocs.org/sdr/USAA970198.md): Stringer · corroded · May 21, 1997 · N240AU · Boeing 737201 · Fuselage Main, Longeron/Stringer
  > INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 2 INCH CORRODED AREA BS 919, STRINGER 25L. SPLICED STRINGER, REPAIRED PER SRM 53-10-3. (M)
- [SDR USAA970197](https://openairdocs.org/sdr/USAA970197.md): Skin · cracked · May 21, 1997 · N240AU · Boeing 737201 · Fuselage Main, Plate/Skin
  > INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND.125 INCH CRACK AFT SERVICE DOOR UPPER HINGE CUTOUT UPPER FORWARD CORNER SKIN. INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3. (M)
- [SDR USAA970196](https://openairdocs.org/sdr/USAA970196.md): Skin · cracked · May 21, 1997 · N240AU · Boeing 737201 · Fuselage Main, Plate/Skin
  > INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CRACKS 4 INCHES AND 2 INCHES AT STRINGER 18R STATION 727 A PLUS 16 INCHES AND STRINGER 18R STATION 727 A PLUS 3 INCHES SKIN. INSTALLED ONE DOUBLER FOR BOTH CRACKS PER SRM 53-30-03 FIG 6. (M)
- [SDR USAA970195](https://openairdocs.org/sdr/USAA970195.md): Skin · cracked · May 21, 1997 · N240AU · Boeing 737201 · Fuselage Main, Plate/Skin
  > INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND.25 INCH CRACK LEFT UPPER CORNER OF CAPTAINS NR 1 WINDOW FRAME FLIGHT COMPARTMENT SKIN. STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR, REPAIRED PER SRM 53-30-3 FIG 11. (M)
- [SDR USAA970058](https://openairdocs.org/sdr/USAA970058.md): Bracket · cracked · Feb 10, 1997 · N240AU · Boeing 737201 · Landing Gear Actuator
  > CLT - I NSPECTION VISUALLY FOUND A 3 INCH CRACK LOCATED AT RADIUS OF SUPPORT BRACKET, FOR NLG ACTUATOR SUPPORT BEAM AFT END. FABRICATED REPAIR BRACKET AS PER SRM 51-40-03. (M)
- [SDR USAA960693](https://openairdocs.org/sdr/USAA960693.md): Skin · corrosion · Oct 26, 1996 · N240AU · Boeing 737201 · Fuselage Main, Plate/Skin
  > ROA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 6 INCH CORROSION STRINGER 26R BS 797 FUSELAGE SKIN. REMOVED CORROSION AND INSTALLED DOUBLER. REPAIRED PER SRM 53-30-3 FIG 6. CORROSION TASK NR C53-100-01, CORROSION LEVEL 2. (M)
- [SDR USAASB96109](https://openairdocs.org/sdr/USAASB96109.md): Oil Press Ind · failed · Jun 15, 1996 · N240AU · Boeing 737201 · Engine Oil Pressure
  > BWI - FLT 2539 - ABOUT 50 MILES OUT OF BWI, THE CREW OBSERVED ZERO OIL PRESSURE ON THE NR 1 ENGINE. ALL OTHER INDICATIONS WERE NORMAL. FLIGHT RETURNED TO FIELD AT BWI. THE ENGINE WAS NOT SHUT DOWN AND NO EMERGENCY EQUIPMENT WAS CALLED OUT. THE FLIGHT LANDE
- [SDR USAA951134](https://openairdocs.org/sdr/USAA951134.md): Stringer · corrosion · Sep 18, 1995 · N240AU · Boeing 737201 · Fuselage Main, Longeron/Stringer
  > CLT - DURING A PCI INSPECTION, A 10 INCH BY 1 INCH CORROSION WAS FOUND AT STRINGER 28R, RBL 6 BETWEEN BS 350 AND 360. REPLACED END STRINGER 28R, RBL 6. (M)
- [SDR USAA951089](https://openairdocs.org/sdr/USAA951089.md): Stringer · corroded · Sep 18, 1995 · N240AU · Boeing 737201 · Fuselage Main, Longeron/Stringer
  > CLT - DURING A PCI INSPECTION, FOUND CORROSION 10 INCHES BY 1 INCH ON STRINGER 28R, RBL 6 BETWEEN BS 350 AND 360. CORROSION TASK NR C53-202-02/PCI 1227, CORROSION LEVEL 2. REPLACED END STRINGER 28R, RBL 6. (M)
- [SDR USAA950748](https://openairdocs.org/sdr/USAA950748.md): Hydraulic Line · leaking · Jul 8, 1995 · N240AU · Boeing 737201 · Hydraulic System, Main
  > ROC - FLT 2274 - UPON GEAR RETRACTION ON TAKEOFF, A-SYSTEM QUANTITY WENT TO ZERO AND A-SYSTEM LOW PRESSURE LIGHTS CAME ON. FLIGHT RETURNED TO ROC WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND HYDRAULIC LINE LEAKING AT RT MAIN GEAR UPLOCK CYC

## 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 = 'N240AU' AND deregistration_id = 'N240AU-2017-02-28'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N240AU-2017-02-28/reports

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