# Service difficulty reports: N472AS, cancelled Dec 9, 2008

A list on [N472AS, cancelled Dec 9, 2008](https://openairdocs.org/deregistered/N472AS-2008-12-09.md).

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

- [SDR XN0A1361](https://openairdocs.org/sdr/XN0A1361.md): Connector · dirty · Feb 8, 2007 · N472AS · Airbus A300B4203 · APU System Wiring
  > APU QUIT AT 22,000 FEET, RUNNING ON ONE GENERATOR TRIED TO RESTART, APU WOULD NOT START. DROPPED TO 20,000 FEET, RESTARTED APU AND IT QUIT AGAIN AT 20,000 FEET. RETURNED TO VHHH. CLEANED AND RESECURED CONNECTIONS AT ECB, APU OPS CHECKS GOOD ON GROUND IAW A3
- [SDR XN0A1360](https://openairdocs.org/sdr/XN0A1360.md): Control Unit · malfunctioned · Feb 3, 2007 · N472AS · Airbus A300B4203 · Rudder Tab Control System
  > RUDDER WILL ONLY GO.5 TO.6666 OR 20 UNITS TO THE LT DURING GROUND CONTROL CHECK. FOUND ARTIFICIAL FEEL AND TRIM UNIT CATCHING ON TRIM STOP. REMOVED AND REPLACED RUDDER ARTIFICIAL FEEL AND TRIM UNIT IAW AMM CHAPTER 27-23-11, OPS CHECKS GOOD IAW AMM CHAPTER 2
- [SDR XN0A1359](https://openairdocs.org/sdr/XN0A1359.md): Gcu · faulted · Feb 1, 2007 · N472AS · Airbus A300B4203 · AC Generation System
  > NR 1 PITCH TRIM TRIPPED BEFORE TAXI. ALL COCKPIT LIGHTS STARTED FLASHING WITH POWER-UP FOR TAXI. LOST VSI INDICATORS TEMPORARILY. LOST TAWS INDICATIONS. FOUND NR 1 GCU CAUSING POWER INTERRUPTIONS. R/R NR 1 GCU AND DISCONNECTED NR 2 CSD, OPS CK GOOD IAW AMM
- [SDR XN0A1353](https://openairdocs.org/sdr/XN0A1353.md): Hydraulic System · leaking · Sep 18, 2006 · N472AS · Airbus A300B4203 · Hydraulic System, Main
  > ON ENGINE START, BLUE HYDRAULIC SYSTEM LEVEL LOW LIGHT CAME ON. INSPECTED SYSTEM FOR LEAK, SERVICED BLUE SYSTEM WITH 2 GALLONS IAW A300 AMM CHAPTER 12-12-29.
- [SDR XN0A1352](https://openairdocs.org/sdr/XN0A1352.md): Indicator · sticking · Aug 31, 2006 · N472AS · Airbus A300B4203 · Elevator Tab Control System
  > FCPI INDICATOR STICKING, ELEV POSITION. FOUND C/P LOOSE ON FCPI IND. RESECURED C/P, OPS CHECK GOOD IAW A300 AMM 27-35-00.
- [SDR XN0A1351](https://openairdocs.org/sdr/XN0A1351.md): Uplock · damaged · Aug 22, 2006 · N472AS · Airbus A300B4203 · Landing Gear Position and Warning
  > AFTER GEAR RETRACTION, LT LIGHTS, DOOR AND GEAR UNSAFE STAYED ON. REMOVED AND REPLACED LT MLG UPLOCK ASSY IAW AMM CHAPTER 32-31-44, LEAK AND OPS CHECKS GOOD. PERFORMED FREE FALL EXTENSION TEST IAW AMM CHAPTER 32-30-00 PAGE 501, OPS CHECKS GOOD. PERFORMED NOR
- [SDR XN0A1348](https://openairdocs.org/sdr/XN0A1348.md): Warning Light · illuminated · Aug 4, 2006 · N472AS · Airbus A300B4203 · Pneumatic Distribution System
  > ON TAXI NR 2 MANIFOLD FAULT AND APU MANIFOLD FAULT LIGHT ILLUM, WILL NOT RESET. FOUND LT FLOW CONTROL VALVE LEAKING, R&R FLOW CONTROL VALVE IAW A300 AMM CHAPTER 21-51-12 OPS CKS GOOD, NO LEAKS NOTED. (CLOSED)
- [SDR XN0A1330](https://openairdocs.org/sdr/XN0A1330.md): Control Lever · malfunctioned · May 11, 2006 · N472AS · Airbus A300B4203 · Landing Gear Selector
  > ON TAKEOFF L/G WOULD NOT RETRACT- SYSTEM 1 OR SYSTEM 2, NO HELP. NORMAL LANDING ACCOMPLISHED. DURING TROUBLESHOOTONG FOUND LANDING GEAR LEVER CONTROL MODULE RESISTANCE MEASUREMENT 126 OHMS BETWEEN PIN K AND PIN H, ALSO FOUND BROKEN WIRE FROM PIN C OF C/P 150
- [SDR XN0A1323](https://openairdocs.org/sdr/XN0A1323.md): Wire · broken · Apr 27, 2006 · N472AS · Airbus A300B4203 · Navigation System Wiring
  > ON TAXI OUT F/O HSI HEADING FLAG APPEARS DURING ALL TURNS. FOUND BROKEN WIRE AT BACK OF COMPASS COUPLER RACK. REPAIRED AND OPS CHECK GOOD IAW A300 AMM CHAPTER 34-22-00.
- [SDR XN0A1319](https://openairdocs.org/sdr/XN0A1319.md): Shaft · sheared · Apr 19, 2006 · N472AS · Airbus A300B4203 · Engine Starter
  > AFTER BLOCK OUT, DURING CROSS START- NR 2 ENGINE WOULD NOT START. NO N1 OR N2 INDICATIONS. START VALVE OPEN LIGHT CAME ON BUT NO START. FOUND STARTER SHAFT SHEARED, REMOVED AND REPLACED NR 2 ENGINE STARTER ASSY AS REQUIRED IAW A300 AMM CHAPTER 80-10-00, OPE
- [SDR XN0A1315](https://openairdocs.org/sdr/XN0A1315.md): Flap · malfunctioned · Apr 1, 2006 · N472AS · Airbus A300B4203 · Leading Edge Slat Control System
  > FLASHING KRUEGER LIGHT AFTER SLATS RETRACTED WITH CONFIG LIGHT ILLUMINATED AND RT LOW-SPEED AILERON CROSSHATCHED. SLAT/FLAP HANDLE IN SLATS EXTEND, KRUEGER INDICATED EXTENDED AND LOW-SPEED AILERON INDICATED CONNECTED. REMOVED AND REPLACED RT KRUEGER FLAP PIC
- [SDR XN0A1313](https://openairdocs.org/sdr/XN0A1313.md): Controller · malfunctioned · Mar 29, 2006 · N472AS · Airbus A300B4203 · Central Warning
  > REJECTED T/O DUE TO MOMENTARY CONFIG LIGHT ON MAIN WARNING PANEL AND AUDIO CHIMES. R&R MASTER WARNING CONTROLLER IAW A300 AMM CHAPTER 33-15-11, OPS CK GOOD. WITH HOT BRAKES "BRAKE HOT" LIGHT ON MAIN WARNING PANEL ONLY ILLUMINATING WITH TAKEOFF CONFIG TEST P
- [SDR XN0A1309](https://openairdocs.org/sdr/XN0A1309.md): Warning Light · false indication · Mar 9, 2006 · N472AS · Airbus A300B4203 · Autopilot System
  > CONFIG LIGHT ILLUMINATED ON TAKEOFF ROLL WITH MASTER WARNING. PERFORMED OPERATIONAL CHECK OF MASTER WARNING AND TAKEOFF CONFIG, CHECKED PROX BOX FOR DEFECTS AND SLAT PROX SWITCHES. NO DEFECTS FOUND. T/O WARNING SYSTEM AND MASTER WARNING SYSTEM OPS CK GOOD I
- [SDR XN0A1285](https://openairdocs.org/sdr/XN0A1285.md): Gyro · inoperative · Dec 16, 2005 · N472AS · Airbus A300B4203 · Directional Gyro and Indicating System
  > NR 3 DG INOPERATIVE. PLACED NR3 DG ON DEFERRAL IAW MEL 34-11-07 CAT C DMI NR 51005 PLACARDS INSTALLED. (ORIG/OPEN)
- [SDR XN0A1238](https://openairdocs.org/sdr/XN0A1238.md): Indicator · failed · May 24, 2005 · N472AS · Airbus A300B4203 · Altimeter, Barometric/Encoder
  > BTB DUE FAIL FLAG ON NR 1 ALT FLAG IN VIEW. REMOVED AND REPLACED NR 1 ALT INDICATOR. OPS CK NORMAL IAW MM 34-12-21 (STATUS:ORIG/CLOSED)
- [SDR XN0A1224](https://openairdocs.org/sdr/XN0A1224.md): Control Box · malfunctioned · Jan 19, 2005 · N472AS · Airbus A300B4203 · Brake Anti-Skid Section
  > ON TAXI, GREEN BRAKES VERY SPONGY, ALT BRAKES NO BRAKING. REMOVED AND REPLACED ANTI-SKID CONTROL BOX IAW A300 MM 32-42-72. SERVICED EMERGENCY BRAKE RESERVOIR IAW MM 32-44-11. SYSTEM GREEN & YELLOW, OPS CHECK GOOD IAW A300 MM 32-42-00.
- [SDR XN0A1216](https://openairdocs.org/sdr/XN0A1216.md): Wire · chafed · Dec 14, 2004 · N472AS · Airbus A300B4203 · Flight Control System Wiring
  > NR 3 WITH SLAT RETRACTION LOW SPEED AILERONS (RED LIGHT) & CONFIG LIGHT ON FWD PANEL ILLUMINATED. TRANFERED TO DMI LIST IAW ENA A300 MEL 27-11-01, CAT "B" DMI 4824 S.P. 27-11-01 C/W. REPAIRED CHAFED WIRE ON HARNESS TO LSA SERVO OF THE LT WING, SYSTEM OPS CK N
- [SDR XNOA1191](https://openairdocs.org/sdr/XNOA1191.md): A/C Pack · shutdown · Jun 29, 2004 · N472AS · Airbus A300B4203 · Cabin Cooling System
  > ON TAXI, NR 1 PACK SHUT-OFF. RE-SEATED CIRCUIT BREAKER AND OPS CHECK GOOD IAW A300 AMM CHAPTER 21-51-00.
- [SDR XNOA01092](https://openairdocs.org/sdr/XNOA01092.md): Regulator · failed · Dec 3, 2002 · N472AS · Airbus A300B4203 · Aileron Control System
  > DURING FLIGHT CONTROL CHECK AILERONS CONTROL VERY HEAVY. WILL NOT RETURN TO NEUTRAL. REMOVED & REPLACED LT CONTROL CABLE TENSION REGULATOR ASSY IAW A300 MM 27-11-17. PERFORMED OPERATIONAL AND FUNCTIONAL INSPECTION.
- [SDR XNOA01042](https://openairdocs.org/sdr/XNOA01042.md): Engine · out of rig · Mar 29, 2002 · N472AS · Airbus A300B4203 · Engine (Turbine/Turboprop)
  > NR 1 ENGINE IS SLOW TO SPOOL. LAGS BEHIND NR 2 ENGINE BY 35 PERCENT N1. PERFORMED STATIC RIG CHECK VSV. NO FAULT FOUND. BOROSCOPED 1,5,6,13,14 COMPRESSOR, HPT-1 LPT-2. NO FAULTS FOUND ALL IAW A300 MM 71-00-00.
- [SDR XNOA01040](https://openairdocs.org/sdr/XNOA01040.md): Engine · out of trim · Mar 26, 2002 · N472AS · Airbus A300B4203 · Engine (Turbine/Turboprop)
  > NR 1 ENGINE IS SLOW TO SPOOL & WILL NOT OBTAIN MAX POWER. TRIMMED NR 1 ENGINE MEC IAW A300 MM 71-00-00. OPS & LEAK CHECK GOOD.
- [SDR XN0A01033](https://openairdocs.org/sdr/XN0A01033.md): Pump · failed · Dec 4, 2001 · N472AS · Airbus A300B4203 · Hydraulic Pump (Electric/Engine), Main
  > RETURNED TO THE GATE DUE NR 1 ENGINE GREEN HYD PUMP INOP. REMOVED AND REPLACED NR 1 ENGINE GREEN HYD PUMP IAW MM 29-11-00. OPS CHECK/LEAK CHECK GOOD.
- [SDR XN0A01025](https://openairdocs.org/sdr/XN0A01025.md): Uplock · out of adj · Sep 21, 2001 · N472AS · Airbus A300B4203 · Landing Gear Retraction/Extension System
  > NOSE DOOR AMBER LIGHT REMAINED ON AFTER GEAR RETRACTION AND NOSE DOOR OPENED UP AT GEAR NEUTRAL. ADJUSTED NLG RT FWD DOOR UPLOCK ASSEMBLY IAW A300 MM 32-22-11 LANDING GEAR SWING C/W IAW A300 32-30-00, OPS CHECK GOOD.
- [SDR XN0A01024](https://openairdocs.org/sdr/XN0A01024.md): Uplock · out of adj · Sep 20, 2001 · N472AS · Airbus A300B4203 · Landing Gear Retraction/Extension System
  > NOSE GEAR DOOR LIGHT ILLUMINATED AFTER TAKEOFF WHEN GEAR RETRACT. INSPECTED NOSE GEAR DOORS, FOUND NO DAMAGE. INSPECTED NOSE GEAR DOOR UPLOCK ASSY AND MECHANISM, FOUND OUT OF ADJUSTMENT. ADJUSTED NOSE GEAR DOOR UPLOCK ASSY IAW A300 MM 32-30-00 AND FREEFALL
- [SDR XN0A01022](https://openairdocs.org/sdr/XN0A01022.md): Uhf Comm · inoperative · Sep 19, 2001 · N472AS · Airbus A300B4203 · UHF Communications System
  > NUMBER 2 RADIO DOES NOT TRANSMIT. TRANSFERRED NR 2 UHF COMM TRANSMIT TO DMI LOG IAW ENA MEL 23-10-01.
- [SDR XNA01014](https://openairdocs.org/sdr/XNA01014.md): Warning Light · illuminated · Jul 25, 2001 · N472AS · Airbus A300B4203 · Leading Edge Slat Position Indicating System
  > ON TAXI, KRUEGER LIGHT FLASHING AND CONFIG LIGHT ON MWP. TRANSFERRED TO DMI 1421 IAW 27-84-01. DEACTIVATED LEFT NOTCH AND KRUEGER IAW SP 27-84-02. PLACARDS INSTALLED.
- [SDR XNA01012B](https://openairdocs.org/sdr/XNA01012B.md): Warning Light · illuminated · Jun 21, 2001 · N472AS · Airbus A300B4203 · Leading Edge Slat Position Indicating System
  > KRUEGER LIGHT FLASHING AND CONFIGURATION HORN/FLAPS O-SLATS 16. TRANSFERRED TO DMI LIST PER ENA A300 MEL 27-84-02. DMI 1352 PLACARDS INSTALLED. SP 27-84-02 COMPLIED WITH IAW A300 MM 27-00-00. RIGHT WING KRUEGER AND NOTCH FLAP DEACTIVATED.
- [SDR XNA01009](https://openairdocs.org/sdr/XNA01009.md): Engine · malfunctioned · May 15, 2001 · N472AS · Airbus A300B4203 · Engine (Turbine/Turboprop)
  > LOUD BANG RIGHT ENGINE AT 16000 FT. EGT WENT TO RED LINE. SHUT ENGINE DOWN AT 06:12 Z.

## 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 = 'N472AS' AND deregistration_id = 'N472AS-2008-12-09'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N472AS-2008-12-09/reports

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