# Service difficulty reports: Airbus Industrie A300 B4-2C

A list on [Airbus Industrie A300 B4-2C](https://openairdocs.org/model/airbus-industrie-a300-b4-2c.md).

Newest first. General aviation reporting is voluntary.

- [SDR DHLA200900038](https://openairdocs.org/sdr/DHLA200900038.md): Battery Pack · failed · Jun 25, 2009 · N367DH · Airbus A300B42C · Emergency Lighting
  > L1-DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED NR1 BATTERY PACK AND OPS CHECKED NORMAL IAW AMM CHAP. 33-51-00.
- [SDR DHLA200900036](https://openairdocs.org/sdr/DHLA200900036.md): Oil Filter · clogged · Jun 16, 2009 · N364DH · Airbus A300B42C · Turbine Engine Oil System
  > FILTER CLOG LIGHT ILLUMINATED ON MWP. FILTER NR 2 OIL CLOG LIGHT ILLUMINATED ON S/O PANEL AFTER TAKEOFF. REMOVED AND REPLACED MAIN ENGINE OIL FILTER P/N AC9380F4010 IAW MM 79-22-01. OPS AND LEAKS CK GOOD IAW JRH 18.1.
- [SDR DHLA200900032](https://openairdocs.org/sdr/DHLA200900032.md): Switch · failed · May 26, 2009 · N364DH · Airbus A300B42C · Engine Oil System (Airframe Furnished)
  > ENGINE NR 2 "OIL CLOG" LIGHT ILLUMINATED INFLIGHT ENGINE 2 WAS SHUTDOWN WITH INFLIGHT ENGINE SHUTDOWN ABNORMAL PROCEDURE ALL ENG IND NORMAL. REPLACED NR 2 ENG OIL FILTER CLOGGING SWITCH PER MM 79-35-11. RAN NR 2 ENG PER JRH 16.5. SYS OPS TEST NORMAL. FOLLO
- [SDR DHLA200900030](https://openairdocs.org/sdr/DHLA200900030.md): Fan · failed · May 17, 2009 · N363DH · Airbus A300B42C · Landing Gear Brake System
  > ON LAST TAKEOFF 3RD HOT BRAKES ILLUM AT 80KTS REJECTED TAKEOFF PERF APPROP CHECKLISTS TAXI IN. REPLACED NR 3 BRAKE IAW MM 32-42-27, OPS CK NORMAL.
- [SDR DHLA200900023](https://openairdocs.org/sdr/DHLA200900023.md): Coalescer Bag · contaminated · Apr 8, 2009 · N364DH · Airbus A300B42C · Humidity Control System
  > NR 2 PACK STILL HAS AN OILY ODOR 25 MIN INTO FLT R FWD CABIN SMOKE LIGHT ILLUM COMPLIED WITH EMERGENCY CHECK LIST SMOKE LIGHT WENT OUT WHEN NR 2 PACK SELECTED OFF RESOLUTION: FOUND RESIDUAL OIL IN WATER SEPARATOR BAGS (RT). PURGED RT A/C SYSTEM IAW MM 21-51-0
- [SDR DHLA200900022](https://openairdocs.org/sdr/DHLA200900022.md): Engine · leaking · Apr 4, 2009 · N364DH · Airbus A300B42C · Turbine Engine Oil System
  > STRONG OIL ODOR FROM PACK NR 2 WHEN THROTTLE AT IDLE AND HP VALVE ON ENGINE NR 2 OPEN. ALL PRESS AND TEMPS NORMAL. PLACED NR 2 PACK ON DMI LIST PER MEL 21-51-01, CAT C, DDD 4-14-09. CONTROL NR 34715. PLACARD INSTALLED. BOROSCOPE ENGINE FOUND OIL WETTING,
- [SDR DHLA200900018](https://openairdocs.org/sdr/DHLA200900018.md): Brake Assy · overheated · Mar 25, 2009 · N367DH · Airbus A300B42C · Landing Gear Brake System
  > BRAKES HOT LIGHT NR 8 BRAKE AT START OF TAKEOFF ROLL, REJECTED TAKEOFF AT 60 KTS, BRAKE TEMP REACHED 560 DEG WITH BRAKE FANS ON. ABNORMAL COMPLETED. PLACED NR 8 MAIN BRAKE ON DMI NR 34675 AS PER MEL 32-42-09-1. NR 8 MAIN BRAKE DEACTIVATED PER SP 32-42-09.
- [SDR DHLA200800013](https://openairdocs.org/sdr/DHLA200800013.md): Mec · failed · Feb 18, 2009 · N365DH · Airbus A300B42C · Fuel Controlling System
  > NR 1 ENGINE FAILED TO ACCELERATE WHEN TAKEOFF POWER WAS APPLIED. REJECTED PRIOR TO 70 KTS AT 5 DEGREE AMBIENT TEMP PRESS ALT 1360'. REMOVED AND REPLACED NR 1 MEC IAW MM 73-21-01. OPS CHECKS SERVICEABLE, NO LEAKS NOTED. MPA C/W IAW JRH.
- [SDR DHLA200800003A](https://openairdocs.org/sdr/DHLA200800003A.md): Line · loose · Jan 30, 2009 · N366DH · Airbus A300B42C · Aircraft Fuel Distribution System
  > DURING CLIMB AT APPROX FL 250 FELT 2 PRONOUNCED THUMPS THEN CONTINUOUS VIBRATION. 1ST AND 2ND OFFICER OBSERVED FLUID VENTING FROM RIGHT WING. LOST APPROX 1200 OF FUEL FROM TANK 2A. RAN ABNORMAL PROC. RETURNED JFK. NO ABNORMAL ENGINE INDICATIONS. FOUND EVIDEN
- [SDR DHLA200800138](https://openairdocs.org/sdr/DHLA200800138.md): Nose Cowl · damaged · Dec 28, 2008 · N365DH · Airbus A300B42C · Engine Air Intake System
  > RAMP DAMAGE TO INB D TOP SIDE OF NR 1 ENGINE NOSE COWL. ACFT STRUCK BY PORTABLE AIRSTAIRS WHILE PARKED ON RAMP. NR1 ENG COWL P/N NSL6051-533 REQUIRING REPLACEMENT.
- [SDR DHLA200800130](https://openairdocs.org/sdr/DHLA200800130.md): Battery Pack · failed · Nov 15, 2008 · N362DH · Airbus A300B42C · Emergency Lighting
  > LT EMERGENCY LIGHT INOP AT ENTRANCE AREA. TROUBLESHOT LT EMERGENCY LIGHT AND FOUND 3 BATTERIES PACKS DEFECTIVE. REMOVED AND REPLACED ALL 3 BATTERIES PACKS AND EMERGENCY LIGHT RT AND LT ENTRANCE AREA CHECKED NORMAL IAW A300 AMM 33-51-14, PN OFF 3117-01 S/N'S
- [SDR DHLA200700075](https://openairdocs.org/sdr/DHLA200700075.md): Proximity Sensor · malfunctioned · Dec 7, 2007 · N366DH · Airbus A300B42C · Landing Gear Position and Warning
  > LANDING GEAR FAILED TO RETRACT (LOCKED OUT) IN WARNING SYSTEM NR 1 PERFORMED ABNORMAL PER AOM RETRACTED IN SYSTEM 2. REMOVED AND REPLACED PROX SENSORS 63GB AND 65 GB. OPS CK GOOD PER M/M 32-61-00 AND 32-00-00 P/N DSF00201-1.
- [SDR 97ZZZX4220](https://openairdocs.org/sdr/97ZZZX4220.md): Uplock Actuator · leaking · Sep 11, 1997 · N864PA · Airbus A300B42C · Landing Gear Door Actuator
  > JFK/MIA - FLT 21 - DURING CRUISE AT 350 GREEN HYD SYSTEM FLUID LOSS, PUMPS FEATHERED IMMEDIATELY, QUANTITY INDICATED ZERO. PUMPS WERE FEATHERED FOR APPROXIMATELY 1.20 HOURS. ALL CHECK LISTS COMPLETED, MANUAL GEAR EXTENSION PROCEDURE SUCCESSFUL. AFTER NORMAL
- [SDR 97ZZZM897](https://openairdocs.org/sdr/97ZZZM897.md): Shaft · loose · Aug 14, 1997 · N864PA · Airbus A300B42C · Passenger/Crew Doors
  > FLT 22 - JFK-MIA - R-4 DOOR LIGHT CAME ON THE MASTER WARNING PANEL, WITH DIFFERENTIAL PRESSURE ABOVE 7 PSI. LIGHT EXTINGUISHED ON DESCENT WITH PRESSURE LESS THAN 7 PSI. CHECKED DOOR AND FOUND LOCK INDICATOR ONE HALF RED, AND ONE HALF GREEN, WITH THE HANDLE F
- [SDR 97ZZZX3392](https://openairdocs.org/sdr/97ZZZX3392.md): Frame · cracked · Jul 11, 1997 · N864PA · Airbus A300B42C · Fuselage Main, Frame
  > JFK/MIA - FLT 25 - AIR TURN BACK. AFTER TAKEOFF, NOSE GEAR WOULD NOT RETRACT. DUMPED FUEL AND RETURNED TO JFK WITH NO FURTHER EVENTS. FOUND LEFT NLG DOOR ACTUATOR UPPER ATTACH BRACKET ATTACHMENT AT FRAME 14A DAMAGED. MADE INTERIM REPAIR IAW AIRBUS REPAIR D
- [SDR 97ZZZX3319](https://openairdocs.org/sdr/97ZZZX3319.md): Skin · dented · Jun 28, 1997 · N864PA · Airbus A300B42C · Horizontal Stabilizer, Plate/Skin
  > JFK - FLT 73 - AT DEPARTURE, A DENT APPROXIMATELY 19 INCHES LONG BY 2 TO 5 INCHES WIDE WAS FOUND ON THE LEFT HORIZONTAL STABILIZER LEADING EDGE. DETERMINED THAT LAVATORY WATER FROM A LAVATORY CAUSED DAMAGE. REPLACED STABILIZER LEADING EDGE. EA 97-3800-01 WH
- [SDR 97ZZZM703](https://openairdocs.org/sdr/97ZZZM703.md): Switch Wire · broken · May 28, 1997 · N864PA · Airbus A300B42C · Leading Edge Slat Position Indicating System
  > FLT 22 - MIA-JFK - AIR TURNBACK DUE TO KRUGER FLAP LIGHT FLASHING AND CONFIGURATION LIGHT ON AFTER FLAP RETRACTION. NO EMERGENCY DECLARED. FOUND BROKEN WIRE AT LEFT KRUEGER FLAP PICKUP SWITCH 11CQ, REPAIRED WIRE AND MADE OPERATIONAL CHECK, FOUND NORMAL. AIR
- [SDR 97ZZZM702](https://openairdocs.org/sdr/97ZZZM702.md): Link · missing · May 27, 1997 · N864PA · Airbus A300B42C · Emergency Exits
  > MIA - DURING SERVICE CHECK FOUND MISSING LINK IN THE EXTERNAL HANDLE RELEASE MECHANISM FOR THE R-4 DOOR. INSTALLED MISSING LINK, OPERATED DOOR FOUND NORMAL. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR 97ZZZM701](https://openairdocs.org/sdr/97ZZZM701.md): Pin · loose · May 26, 1997 · N864PA · Airbus A300B42C · Emergency Exits
  > FLT 3 - JFK-MIA - AT DEPARTURE TIME THE R-4 DOOR WOULD NOT ARM. FOUND R-4 DOOR NOT CLOSING ALL THE WAY, DUE TO EXTERIOR HANDLE LINK PIN BACKED OUT REINSTALLED PIN CYCLED HANDLE DOOR OPERATED NORMAL. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR 97ZZZM700](https://openairdocs.org/sdr/97ZZZM700.md): Mechanism · out of adjust · May 18, 1997 · N864PA · Airbus A300B42C · Emergency Exits
  > FLT 3 - JFK-LAX - AT DEPARTURE TIME THE R-4 DOOR WOULD NOT CLOSE. FOUND OUTSIDE HANDLE OUT OF SEQUENCE, RECYCLED HANDLE AND THE DOOR CLOSED NORMALLY. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR 97ZZZX2600](https://openairdocs.org/sdr/97ZZZX2600.md): Battery Pack · discharged · May 11, 1997 · N864PA · Airbus A300B42C · Emergency Lighting
  > DURING ROUTINE SERVICE CHECK, FOUND R-3 AND R-4 EMERGENCY LIGHT BATTERY PACK INOPERATIVE. REMOVED AND REPLACED R-3 AND R-4 BATTERY PACKS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR 97ZZZX2568](https://openairdocs.org/sdr/97ZZZX2568.md): Sequence Box · failed · Apr 26, 1997 · N864PA · Airbus A300B42C · Cabin Pressure Control System
  > JFK/MIA - FLT 23 - AT FL 22,000, PRESSURIZATION SYSTEM COULD NOT BE CONTROLLED BY SYSTEM NR 2. SWITCHED TO SYSTEM NR 1 AND CABIN CONTINUED TO CLIMB, DESCENDED TO 10,000 FEET AND RETURNED TO JFK. NO EMERGENCY DECLARED, NORMAL LANDING. TROUBLESHOT SYSTEM, FOU
- [SDR 97ZZZX2566](https://openairdocs.org/sdr/97ZZZX2566.md): Uplock Release · stuck · Apr 1, 1997 · N864PA · Airbus A300B42C · Landing Gear Retraction/Extension System
  > JFK/MIA - FLT 23 - 17:45 AFTER TAKEOFF THE LANDING GEAR WOULD NOT RETRACT IN EITHER NR 1 OR NR 2 SYSTEMS. RETURNED TO JFK, NO FUEL DUMPED AND NORMAL LANDING, NO EMERGENCY DECLARED. UPON INSPECTION OF THE NOSE GEAR, FOUND GROUND MANUAL RELEASE HANDLE TO BE I
- [SDR 97ZZZX2567](https://openairdocs.org/sdr/97ZZZX2567.md): Wire · broken · Mar 9, 1997 · N864PA · Airbus A300B42C · Light System Wiring
  > MIA - PILOT REPORTS DURING PRE-FLIGHT CHECK LIST THE EMERGENCY LIGHTS WERE INOPERABLE. FOUND WIRE AT 39WL SWITCH BOX EMERGENCY LIGHT CONTROL. ATTENDANT PANEL 818 VU, ZONE 22. REPAIRED WIRE IAW 20-27-17 AND OPS CHECK OK.

## 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 aircraft_model_key = 'A300B42C'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/airbus-industrie-a300-b4-2c/reports

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