# Service difficulty reports: N515AU, cancelled Feb 14, 2008

A list on [N515AU, cancelled Feb 14, 2008](https://openairdocs.org/deregistered/N515AU-2008-02-14.md).

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

- [SDR SB07083](https://openairdocs.org/sdr/SB07083.md): Battery Pack · discharged · Sep 26, 2007 · N515AU · Boeing 7373B7 · Emergency Lighting
  > BFM - MAINTENANCE REPORTED THE EMERGENCY EXIT SIGNS AT THE LEFT-HAND AND RIGHT-HAND FORWARD DOORS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK PER MM 33-51-51. OPERATIONAL CHECK GOOD.
- [SDR USAA200705U04](https://openairdocs.org/sdr/USAA200705U04.md): Skin · cracked · May 8, 2007 · N515AU · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > APPROX 15.5 INCH CRACK IN FUSELAGE RUNS LONGITUDINAL, LOCATED BETWEEN STA 482 & 500, BETWEEN STR 28L & 28R. INSTALLED DOUBLER REPAIR & INSTALLED NEW ANTENNA SUPPORT KIT PER EA 84528.
- [SDR SB06103](https://openairdocs.org/sdr/SB06103.md): Windshield · cracked · Oct 21, 2006 · N515AU · Boeing 7373B7 · Flight Compartment Windows
  > ORD FLT 1623 DURING CRUISE AT FL340, EN ROUTE FROM CLT TO MSP, THE CAPTAIN'S L1 WINDSHIELD OUTER PANE CRACKED. PRESSURIZATION HELD OK. WINDOW HEAT WAS TURNED OFF AND NO FURTHER CRACKING WAS NOTED. FLIGHT DIVERTED TO ORD AND LANDED WITHOUT FURTHER INCIDENT.
- [SDR USAA200608002](https://openairdocs.org/sdr/USAA200608002.md): Skin · cracked · Aug 24, 2006 · N515AU · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > A 2.5 INCH CRACK FOUND ON FUSELAGE SKIN STA 727E AT STR 25R. INSTALLED TRIPLER PER SRM 53-00-01 PROCEDURES II & V.
- [SDR USAA200607001](https://openairdocs.org/sdr/USAA200607001.md): Skin · cracked · Jun 9, 2006 · N515AU · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > A 2 INCH LONG CRACK AT STA 727 S-24R. CUT OUT DAMAGE, ACCOMPLISHED HF/EC AND INSTALLED DOUBLER WITH SHIMS FOR FILLET FAIRING PER SRM 53-00-01 FIG 201, DETAIL XI AND EA 82696.
- [SDR SB06038](https://openairdocs.org/sdr/SB06038.md): Sign · inoperative · Apr 20, 2006 · N515AU · Boeing 7373B7 · Emergency Lighting
  > PIT - THE LEFT EMERGENCY EXIT LOW LEVEL SIGN WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD.
- [SDR SB05106](https://openairdocs.org/sdr/SB05106.md): Battery Pack · discharged · Sep 1, 2005 · N515AU · Boeing 7373B7 · Emergency Lighting
  > CLT - MAINTENANCE REPORTED THE FORWARD RIGHT EMERGENCY LIGHT AT THE SERVICE DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD.
- [SDR SB05064](https://openairdocs.org/sdr/SB05064.md): Light · inoperative · May 26, 2005 · N515AU · Boeing 7373B7 · Emergency Lighting
  > MAINTENANCE FOUND THE INTERIOR EMERGENCY EXIT LIGHT ASSEMBLY, FORWARD OF THE FORWARD SERVICE DOOR, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EXIT LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD.
- [SDR USAA040976](https://openairdocs.org/sdr/USAA040976.md): Support Angle · cracked · Nov 16, 2004 · N515AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > PIT - C5 - SUPPORT ANGLE, 1 INCH LONG CRACK AT STA 540 S - 22L. SPLICE ANGLE IAW TYP REP 53-50-03.
- [SDR USAA040709](https://openairdocs.org/sdr/USAA040709.md): Skin Panel · cracked · Sep 14, 2004 · N515AU · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > UNSCHEDULED MAINTENANCE, KEEL BEAM SKIN PANEL, 3 INCH CRACK, BS 690 KEEL BEAM PANEL. INSTALLED DOUBLER (TEMP REPAIR) IAW SRM 53-60-12, FIG 202.
- [SDR USAASB04090](https://openairdocs.org/sdr/USAASB04090.md): Sensor · malfunctioned · Jul 12, 2004 · N515AU · Boeing 7373B7 · Leading Edge Slat Position Indicating System
  > PIT - FLT 1058 - AFTER TAKEOFF FROM PIT, EN ROUTE TO PVD, CREW REPORTED THE NR 4 LEADING EDGE FLAP WOULD NOT RETRACT AND THE LEADING EDGE FLAP TRANSIT AMBER LIGHT WAS ILLUMINATED. FLIGHT RETURNED TO FIELD AT PIT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGE
- [SDR USAA040006](https://openairdocs.org/sdr/USAA040006.md): Keelbeam · chafed · Jan 12, 2004 · N515AU · Boeing 7373B7 · Fuselage Main, Keel
  > PIT - FOUND KEELBEAM CHAFFING 16 INCH AREA, STATION 727 FORWARD TO 711 RT OUTBOARD FLANGE OF LT KEELBEAM BY FAIRING AND ATTACH FAST. INSTALLED DOUBLERS, STRAP AND NUT PLATES PER TYPICAL REPAIR 53-60-05 AND EA 77518. (M)
- [SDR USAA040005](https://openairdocs.org/sdr/USAA040005.md): Keelbeam · chafed · Jan 1, 2004 · N515AU · Boeing 7373B7 · Fuselage Main, Keel
  > PIT - FOUND KEEL BEAM CHAFING 16 INCH AREA, STATION 727 FORWARD TO 711 LEFT OUTBOARD FLANGE OF LT KEEL BEAM BY FASTENERS AND PANELS. INSTALLED DOUBLERS, STRAPS AND NUTPLATES PER TYPICAL REPAIR EA 77719, T/R 53-60-05. (M)
- [SDR USAA030321](https://openairdocs.org/sdr/USAA030321.md): Door Frame · cracked · Dec 30, 2003 · N515AU · Boeing 7373B7 · Fuselage Main, Structure
  > PIT - FOUND DOOR FRAME SKIN CRACKED.5 INCH LONG, FORWARD SERVICE DOOR FRAME CRACK AT DOOR STOP NR 4. DOUBLER INSTALLED AT DOOR STOP NR 4 PER TR 52-10-11. (M)
- [SDR USAA030320](https://openairdocs.org/sdr/USAA030320.md): Door Frame · cracked · Dec 29, 2003 · N515AU · Boeing 7373B7 · Fuselage Main, Structure
  > PIT - FOUND DOOR FRAME CRACKED 1 INCH, LOWER AFT FORWARD SERVICE DOOR CORNERS. INSTALLED DOUBLER PER EA 77600. (M)
- [SDR USAASB03125](https://openairdocs.org/sdr/USAASB03125.md): Socket · shorted · Aug 1, 2003 · N515AU · Boeing 7373B7 · Emergency Lighting
  > CLT - MAINTENANCE FOUND THE EMERGENCY LIGHT AT SEAT ROW 12 INOPERATIVE. MAINTENANCE FOUND THE LIGHT SOCKET SHORTED. REMOVED AND REPLACED LIGHT SOCKET AT SEAT ROW 12 AND REPLACED BATTERY PACK, P/N 2013-1A, AS PRECAUTIONARY. OPERATIONAL CHECK GOOD. (M)
- [SDR USAASB03116](https://openairdocs.org/sdr/USAASB03116.md): Programming Arm · out of adjust · Jul 19, 2003 · N515AU · Boeing 7373B7 · Service Doors
  > AFTER TAKEOFF FROM PHL, CREW REPORTED THE AIRCRAFT WOULD NOT PRESSURIZE IN AUTO, STANDBY OR MANUAL PRESSURIZATION MODES. OUTFLOW VALVE WAS SHOWING CLOSED. FLIGHT RETURNED TO FIELD AT PHL AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINT
- [SDR USAASB02171](https://openairdocs.org/sdr/USAASB02171.md): Uplock Sensor · faulty · Sep 14, 2002 · N515AU · Boeing 7373B7 · Landing Gear Position and Warning
  > ON CLIMB OUT, ENROUTE, CREW RECEIVED A RIGHT MAIN LANDING GEAR RED UNSAFE LIGHT AFTER GEAR RETRACTION. CREW FOLLOWED QUICK REFERENCE HANDBOOK PROCEDURES AND CYCLED THE GEAR. THEY RECEIVED THREE GEAR GREEN LIGHTS WHEN EXTENDING GEAR BUT RECEIVED RIGHT MAIN LA
- [SDR USAASB01237](https://openairdocs.org/sdr/USAASB01237.md): Control Panel · failed · Aug 19, 2001 · N515AU · Boeing 7373B7 · Autopilot System
  > CLT - FLT 572 - APPROACH TO CLT,'B' A/P ON, A/C MADE UNCOMMANDED 30 DEGREE ROLL TO THE RT. AFTER A 20 DEGREE HEADING CHANGE (30 DEGREE AOB SELECTED ON TURN KNOB), A/P CORRECTED TO HEADING SELECTED. NO DEFLECTION WAS NOTED ON RUDDER PEDALS. AFTER CORRECTION
- [SDR USAA010455](https://openairdocs.org/sdr/USAA010455.md): Skin · damaged · Apr 25, 2001 · N515AU · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > TPA - FOUND FUSELAGE SKIN DAMAGED 4 INCHES, BS 747, BETWEEN S18L AND S19L. INSTALLED DOUBLER PER SRM 53-00-01, FIG 202. (M)
- [SDR USAA010454](https://openairdocs.org/sdr/USAA010454.md): Skin · cracked · Apr 25, 2001 · N515AU · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > FOUND FUSELAGE SKIN CRACKED.25 INCH, BS 360, LOWER BELLY, BL 0. INSTALLED DOUBLER PER TYPICAL REPAIR 53-30-07. (M)
- [SDR USAASB99248](https://openairdocs.org/sdr/USAASB99248.md): Relay · failed · Oct 12, 1999 · N515AU · Boeing 7373B7 · Integrated Flight System
  > PHL - FLT 346 - AFTER TAKEOFF THE CREW REPORTED THAT EVERYTIME THE STAB TRIM SWITCH WAS ACTUATED FROM EITHER YOKE, THE FIRST OFFICERS HSI HEADING FLAGS APPEARED. RELEASING THE SWITCH CAUSES THE FLAGS TO DISAPPEAR. DECISION WAS MADE TO RETURN TO FIELD AT PHL.
- [SDR USAASB99121](https://openairdocs.org/sdr/USAASB99121.md): Indicator · failed · May 6, 1999 · N515AU · Boeing 7373B7 · Trailing Flap Position Indicating System
  > LGA - FLT 420, ON APPROACH, TRAILING EDGE FLAPS WOULD NOT EXTEND MORE THAN FLAPS 10. ACCOMPLISHED GO AROUND AND FLAPS EXTENDED TO FLAPS 15 WITH FLAP HANDLE AT 15. FLAPS RETRACTED NORMALLY. DURING SECOND APPROACH, FLAPS EXTENDED NORMALLY. FLIGHT LANDED WITH
- [SDR USAASB97024](https://openairdocs.org/sdr/USAASB97024.md): Connector · dirty · Jan 22, 1997 · N515AU · Boeing 7373B7 · Fire Detection
  > ALB - FL 561 - ON CLIMB-OUT FROM ALB, CREW RECEIVED A FAULT LIGHT FOR THE NR 2 ENG ON THE FIRE WARNING PNL. CREW FOLLOWED ISOLATION PROCEDURES AND DETERMINED THAT THE FIRE DETECT 'B' LOOP WAS INOP. 'A' LOOP TESTED GOOD. MOMENTS LATER, CREW RECEIVED A FAULT
- [SDR USAA960473](https://openairdocs.org/sdr/USAA960473.md): Floor Beam · corrosion · Jun 14, 1996 · N515AU · Boeing 7373B7 · Fuselage Main, Floor Beam
  > CLT - INSPECTION VISUALLY FOUND LEVEL 2 CORROSION AT NUT PLATE HOLES, ACROSS FLOORBEAM LOCATED AT STATION 986.5. INSTALLED NEW CHORD AND REPAIR ANGLES AS PER T/R 53-10-05. (M)
- [SDR USAA960472](https://openairdocs.org/sdr/USAA960472.md): Floor Beam · corrosion · Jun 14, 1996 · N515AU · Boeing 7373B7 · Fuselage Main, Floor Beam
  > CLT - INSPECTION VISUALLY FOUND LEVEL 2 CORROSION, AT NUT PLATE HOLES ACROSS FLOORBEAM, LOCATED AT STATION 967. INSTALLED NEW CHORD AND REPAIR ANGLES PER T/R 53-15-91A. (M)

## 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 = 'N515AU' AND deregistration_id = 'N515AU-2008-02-14'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N515AU-2008-02-14/reports

---
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