# Service difficulty reports: Airbus Industrie A300 B4-203

A list on [Airbus Industrie A300 B4-203](https://openairdocs.org/model/airbus-industrie-a300-b4-203.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 28 · 1,357 reports

- [SDR WRNA201200006](https://openairdocs.org/sdr/WRNA201200006.md): Gyro · unserviceable · May 11, 2012 · N821SC · Airbus A300B4203 · Speed-Attitude Correction System
  > BOTH NR 1 & NR 2 YAW DAMPERS WOULD NOT ENGAGE. AIRCRAFT RETURNED TO AIRFIELD. LANDING NORMAL. MX FOUND NR 1 & NR 2 YAW RATE GYRO'S AT FAULT. REMOVED AND REPLACED NR 1 & NR 2 YAW RATE GYROS IAW 22-21-45. OP'S CHECK SATISFACTORY. A/C RETURNED TO SERVICE.
- [SDR WRNA201110210010](https://openairdocs.org/sdr/WRNA201110210010.md): Gps · malfunctioned · Oct 21, 2011 · N821SC · Airbus A300B4203 · Global Positioning System
  > NR 1 GPS MESSAGE "HEADING REQUIRED" RENDERING, GPS AND NR 1 AUTOPILOT INOPERATIVE. VECTORED SO ACFT STAYED ON HEADING MODE. AUTOPILOT NR 2 SELECTED BUT DID NOT ENGAGE. NOT SUCCESSFUL AFTER SEVERAL ATTEMPTS. RETURN TO AIRPORT. LANDED NORMAL. MX CHECKED W
- [SDR WRNA2009004](https://openairdocs.org/sdr/WRNA2009004.md): Pitot Line · clogged · Dec 30, 2009 · N821SC · Airbus A300B4203 · Pitot/Static System
  > ON TAKEOFF ROLL, DEPARTING FROM SJU, CREW NOTICED THAT THERE WAS NO AIRSPEED INDICATION FROM F/O INDICATOR. CAPTAIN INDICATOR SHOWING BETWEEN 75-80 KTS AND FLUCTUATING. ABORTED T/O PROCEDURES FOLLOWED. RETURNED TO GATE. MAINT FOUND PITOT LINES CLOGGED WITH
- [SDR DHLA200900025](https://openairdocs.org/sdr/DHLA200900025.md): Coalescer Bag · dirty · Apr 14, 2009 · N364DH · Airbus A300B4203 · Humidity Control System
  > REPLACED NR 2 COALESCER P/N 20D10-3 IAW MM 21-51-16. THIS DOES NOT CLOSE DMI.
- [SDR DHLA200900021](https://openairdocs.org/sdr/DHLA200900021.md): Unknown · odor · Apr 1, 2009 · N364DH · Airbus A300B4203 · Air Distribution System
  > ACFT HAS AN UNUSUAL ODOR COMING THRU THE A/C PACKS FLT DECK DUCT TEMP WAS AT 150 COMPT TEMP 68. RAN NR 1 AND NR 2 PACK SYS OPS CKED NORMAL ON GROUND IAW AMM 21-00-00 COULD NOT DUPLICATE NO UNUSUAL ODORS
- [SDR WRNA2009001](https://openairdocs.org/sdr/WRNA2009001.md): Ground Wire · loose · Mar 17, 2009 · N501TR · Airbus A300B4203 · Flight Control System Wiring
  > AFTER TAKEOFF, KRUEGER FLAP FAILED TO RETRACT. CREW REPORTED A "CONFIG" LIGHT ON MWP. ALSO, FLIGHT CHARACTERISTICS OF AIRCRAFT SEEMED DIFFERENT. DECISION MADE TO RETURN TO AIRFIELD. AIRCRAFT LANDED NORMAL, NO FUEL WAS DUMPED. MAINTENANCE UPON TROUBLESHOOT
- [SDR DHLA200800011A](https://openairdocs.org/sdr/DHLA200800011A.md): Engine · power loss · Feb 12, 2009 · N365DH · Airbus A300B4203 · Engine Fuel and Control
  > DURING T/O ENG. 1 & 2 SPOOLED TO 60% N1, GO LEVERS SELECTED NR 1 ENG SPOOLED TO 80% N1 MAX, THROTTLE FULL FORWARD NO RESPONSE. OAT +5º C TAS LESS THAN 60KTS. REMOVED. CLEANED & INSTALLED PS-4 LINE. PERFORMED ACCELERATION CK ON NR 1 ENG. ENG. RUN OPS GOOD PE
- [SDR WRN2009F00000](https://openairdocs.org/sdr/WRN2009F00000.md): Fire Loop · defective · Dec 19, 2008 · N510TA · Airbus A300B4203 · Fire Detection
  > ENGINE NR 1 SHUT DOWN IN FLIGHT DUE TO A FIRE INDICATION DURING FLIGHT FROM BDL TO BQN. BOTH FIRE BOTTLES WERE DISCHARGED. WARNING LIGHT EXTINGUISHED. ACFT LANDED NORMALLY. NO FUEL DUMPED. MX REPLACED 3 FIRE LOOPS AND AN AMPLIFIER. RUN UP CHECK OK. ACFT
- [SDR DHLA200800137](https://openairdocs.org/sdr/DHLA200800137.md): Battery Pack · discharged · Dec 15, 2008 · N366DH · Airbus A300B4203 · Emergency Lighting
  > EMERGENCY LIGHTS BATTERIES 0 VOLTS.
- [SDR DHLA200800108](https://openairdocs.org/sdr/DHLA200800108.md): Battery Pack · inoperative · Sep 30, 2008 · N367DH · Airbus A300B4203 · Emergency Lighting
  > ON PRE-DEPARTURE CHECK, EMERGENCY LIGHT OVER R1 DOOR INOPERATIVE, ACFT GROUNDED. R&R POWER SUPPLY IAW MM 33-51-14. OPS CHECKED OK IAW 33-51-00.
- [SDR DHLA200800107](https://openairdocs.org/sdr/DHLA200800107.md): Battery Pack · inoperative · Sep 30, 2008 · N367DH · Airbus A300B4203 · Emergency Lighting
  > ON PRE-DEPARTURE CHECK, EMERGENCY LIGHT OVER R1 DOOR INOPERATIVE, ACFT GROUNDED. R&R POWER SUPPLY IAW MM 33-51-14. OPS CHECKED OK IAW 33-51-00.
- [SDR DHLA200800106](https://openairdocs.org/sdr/DHLA200800106.md): Power Supply · inoperative · Sep 30, 2008 · N367DH · Airbus A300B4203 · Emergency Lighting
  > ON PRE-DEPARTURE CHECK, EMERGENCY EXIT LIGHT AT R1 DOOR INOPERATIVE, ACFT GROUNDED. R&R POWER SUPPLY IAW MM 33-51-14. OPS CHECKED GOOD IAW 33-51-00.
- [SDR WRN2008F00004](https://openairdocs.org/sdr/WRN2008F00004.md): Sill · fod · Jun 23, 2008 · N510TA · Airbus A300B4203 · Fuselage Miscellaneous Structure
  > AC AFTER TAKEOFF, LOUD WHISTLING NOISE HEARD AND AC HAD PROBLEMS PRESSURIZING. AC MADE UNSCHEDULED STOP, WITH NORMAL LANDING. FOUND F.O.D. AND DEBRIS IN MAIN CARGO DOOR SILL AREA. REMOVED F.O.D. AND DEBRIS FROM CARGO DOOR SEAL AREA IAW 52-70-00. SEAL FOR MAIN
- [SDR WRN2008F00003](https://openairdocs.org/sdr/WRN2008F00003.md): Indicator · unserviceable · Jun 18, 2008 · N501TR · Airbus A300B4203 · Engine EGT/TIT Indicating System
  > DURING CRUISE, ENG NR1 EGT OFF SCALE HIGH INDICATION. POINTER AT 6 O`CLOCK POSITION. POINTER AND DIGITAL READOUT AGREED. AMBER EGT LIGHT ON, ENGINE EGT LIGHT ON MWP, AND SSC. AC RETURNED TO FIELD, ABNORMAL PROCEDURES WERE PERFORMED AND APPROX. 8500 LBS OF FUEL
- [SDR WRN2008F00002](https://openairdocs.org/sdr/WRN2008F00002.md): Valve · stuck · Jun 16, 2008 · N510TA · Airbus A300B4203 · Cabin Pressure Control System
  > AFTER TAKEOFF, PRESSURIZATION MALFUNCTION OCCURRED. ACCOMPLISHED ABNORMAL PROCEDURES. AC RETURNED TO FIELD. LANDING NORMAL. MX FOUND GROUND VENT VALVE STUCK CLOSED. MX CLEANED AND RESET GROUND VENTING VALVE IAW 21-31-17, PG 501. OPS CHECKED SATISFACTORY
- [SDR WRN2008F00001](https://openairdocs.org/sdr/WRN2008F00001.md): Connector · dirty · Jun 16, 2008 · N505TA · Airbus A300B4203 · Global Positioning System
  > AFTER TAKEOFF, APPROX 40 MINUTES INTO FLIGHT, AC TURNED BACK DUE TO NAV PROBLEMS WITH GPS SYSTEM. GPS SYS NR 2 PREVIOUSLY MEL, NR 1 GPS SYS WENT TO DR MODE. AIRCRAFT RETURNED TO BASE, NORMAL LANDING ACCOMPLISHED. MX CLEANED AND RESET CONNECTION ON GPS ANTEN
- [SDR WRN2008F00000](https://openairdocs.org/sdr/WRN2008F00000.md): Gearbox · contaminated · Jun 7, 2008 · N501TR · Airbus A300B4203 · Turbine Engine Reduction Gear
  > ON CLIMBOUT STJ FL230, OIL QTY DECREASING RAPIDLY. PERFORMED PRECAUTIONARY SHUTDOWN PROCEDURES, OIL PRESSURE WAS NOT LOST, OIL TEMP RISE TO 130 DEGREES. REPLACED GEARBOX IAW MM 72-60-01. OPS CHECK GOOD ON NR 2 ENGINE. (K)
- [SDR WRNA20080039](https://openairdocs.org/sdr/WRNA20080039.md): Control Valve · faulty · May 26, 2008 · N504TA · Airbus A300B4203 · Landing Gear Retraction/Extension System
  > DURING APPROACH TO BQN, LANDING GEAR FAILED TO EXTEND WITH SYSTEM 1 OR 2, RETURNED TO 2,000 FEET TO HOLD WHILE LOWERING GEAR MANUALLY. AFTER SUCCESSFUL EXTENSION OF GEAR, A SAFE LANDING WAS MADE. FIM 32-30-00 /107 INDICATED A FAULTY LANDING GEAR ELECTROVALVE
- [SDR WRNA20080038](https://openairdocs.org/sdr/WRNA20080038.md): Uplock · unserviceable · May 2, 2008 · N504TA · Airbus A300B4203 · Landing Gear Retraction/Extension System
  > AFTER TAKEOFF, NOSE LANDING GEAR FAILED TO RETRACT. DUMPED FUEL AND RETURNED TO FIELD FOR A SAFE LANDING. REPLACED NOSE GEAR UP-LOCK ASSY IAW MM 32-31-14 PG 401. OPS CHECK GOOD IAW MM 32-30-00 PG 501. AIRCRAFT RELEASED FOR SERVICE.
- [SDR WRNA200800037](https://openairdocs.org/sdr/WRNA200800037.md): Csd · malfunctioned · Apr 29, 2008 · N510TA · Airbus A300B4203 · AC Generator-Alternator
  > DURING FLIGHT, NR 1 CONSTANT SPEED DRIVE LOW OIL PRESSURE LIGHT ILLUMINATED FOLLOWED BY RISING OIL TEMPERATURE. DISCONNECTED CSD AND RETURNED TO MFM FOR A SAFE LANDING. REPLACED CSD IAW MM 24-11-11 PG 401 AND CSD OIL COOLER IAW 24-11-21 PAGE 401. AIRCRAFT R
- [SDR WRNA20080011](https://openairdocs.org/sdr/WRNA20080011.md): Slide · no test · Apr 8, 2008 · N506TA · Airbus A300B4203 · Escape Slide
  > DURING OPERATIONAL TEST, THE R-1 DOOR ESCAPE SLIDE/RAFT FAILED TEST, DID NOT FULLY INFLATE. REPLACED ESCAPE SLIDE/RAFT CONTACTED MAINTENANCE STATION WERE TEST WAS ACCOMPLISHED. SLIDE BOTTLE PRESSURE INDICATOR WAS IN THE 'GREEN', SLIDE DEPLOYED BUT DID NOT FU
- [SDR WRNA20080010](https://openairdocs.org/sdr/WRNA20080010.md): Duct · cracked · Apr 8, 2008 · N504TA · Airbus A300B4203 · Engine Bleed Air System
  > AFTER TAKEOFF, NR 1 AND NR 2 BLEED FAULT LIGHTS AND APU MANIFOLD LIGHTS CAME ON AND WOULD NOT RESET. DUMPED 18,000 POUNDS OF FUEL AND RETURNED TO FIELD FOR A SAFE LANDING. FOUND NR 2 ENGINE BLEED AIR DUCT IN AIR CONDITIONING BAY CRACKED. REPLACED DUCT IAW
- [SDR WRNA20080009](https://openairdocs.org/sdr/WRNA20080009.md): Pin · disconnected · Mar 28, 2008 · N821SC · Airbus A300B4203 · Light System Wiring
  > DURING DAILY CHECK, MAINTENANCE FOUND R1 EMERGENCY EXIT LIGHTS INOP. FOUND PIN NR 3 DISCONNECTED FROM LIGHT ASSY, RECONNECTED, OPS CHECKED GOOD. AIRCRAFT RELEASED FOR SERVICE.
- [SDR WRNA200800014](https://openairdocs.org/sdr/WRNA200800014.md): Skin · corroded · Mar 26, 2008 · N501TR · Airbus A300B4203 · Fuselage Main, Plate/Skin
  > DURING M96 CHECK, FOUND OUT OF LIMIT CORROSION ON FUSELAGE AT STR 6 TO FRAME 76. CUT OUT DAMAGED AREA 2.75 INCHES BY.75 INCHES AND INSTALLED FILLER FABRICATED FROM 2024 T3 0.090 AND REPAIR DOUBLER FABRICATED FROM 2024 T3 0.100 IAW A300 SRM 53-10-10.
- [SDR DHLA200800035](https://openairdocs.org/sdr/DHLA200800035.md): Apu · leaking · Mar 18, 2008 · N362DH · Airbus A300B4203 · APU Oil System
  > BEFORE FLIGHT 102 ON GROUND IN SFO, 3 CABIN SMOKE DETECTORS ILLUMINATED ON THE GROUND. ON INSP FOUND APU TO BE LEAKING OIL. INGESTED INTAKE, SMOKE DET OK IAW AMM 26-10-0 DEFERRRED IAW MEL 49-11-01 DMI NR 32097. AIRCRAFT WAS GROUNDED.
- [SDR WRNA200800006](https://openairdocs.org/sdr/WRNA200800006.md): Engine · failed · Mar 16, 2008 · N505TA · Airbus A300B4203 · Engine (Turbine/Turboprop)
  > AFTER TAKEOFF FROM MFM, CLIMBING THROUGH 15,000 FEET A LOUD EXPLOSION WAS HEARD FROM NR 1 ENGINE FOLLOWED BY SEVERE VIBRATION, ENGINE WAS RETARDED TO IDLE POWER, VIBRATION CONTINUED FOLLOWED BY LOW OIL PRESS LIGHT AND EGT INCREASE TO 963 DEGREES C. ENGINE WAS
- [SDR WRNA200800022](https://openairdocs.org/sdr/WRNA200800022.md): Seat Track · cracked · Mar 3, 2008 · N501TR · Airbus A300B4203 · Fuselage, Seat/Cargo Attach Fittings
  > DURING M96 CHECK, MAIN CABIN SEAT TRACK AT FRAME 40 RBL 54 WAS FOUND CRACKED. REPLACED SEAT TRACK AT RBL 54 FROM FRAME 40 TO FRAME 44 +12 INCHES IAW SRM 53-10-10.
- [SDR DHLA200800019](https://openairdocs.org/sdr/DHLA200800019.md): Bottle · reads low · Mar 1, 2008 · N365DH · Airbus A300B4203 · Escape Slide
  > R1 DOOR ESCAPE SLIDE PRESSURE IN RED. REMOVED AND REPLACED SLIDE ASSY. AIRCRAFT WAS GROUNDED.
- [SDR WRNA200800020](https://openairdocs.org/sdr/WRNA200800020.md): Track · corroded · Feb 28, 2008 · N501TR · Airbus A300B4203 · Fuselage, Seat/Cargo Attach Fittings
  > DURING M96 CHECK WHILE ACCOMPLISHING CPCP TASK CARD ZL-150-L403-501, CORROSION WAS FOUND ON LT INBOARD ROLLER TRACK IN AFT CARGO COMPARTMENT AT FRAME 57. REMOVED AND REPLACED ROLLER TRACK IAW SRM 51-30-30.
- [SDR WRNA200800019](https://openairdocs.org/sdr/WRNA200800019.md): Track · corroded · Feb 28, 2008 · N501TR · Airbus A300B4203 · Fuselage, Seat/Cargo Attach Fittings
  > DURING M96 CHECK WHILE ACCOMPLISHING CPCP TASK CARD Z:-150-L403-5-01, CORROSION WAS FOUND ON LT INBOARD ROLLER TRACK IN AFT CARGO COMPARTMENT BETWEEN FRAMES 58 TO 59. REMOVED AND REPLACED ROLLER TRACK IAW SRM 51-30-30.
- [SDR WRNA200800021](https://openairdocs.org/sdr/WRNA200800021.md): Track · corroded · Feb 28, 2008 · N501TR · Airbus A300B4203 · Fuselage, Seat/Cargo Attach Fittings
  > DURING M96 CHECK WHILE ACCOMPLISHING CPCP TASK CARD ZL-150-L403-501, CORROSION WAS FOUND ON LT INBOARD ROLLER TRACK IN AFT CARGO COMPARTMENT AT FRAMES 54 TO 57. REMOVED AND REPLACED ROLLER TRACK IAW SRM 51-30-30.
- [SDR WRNA200800018](https://openairdocs.org/sdr/WRNA200800018.md): Skin · corroded · Feb 26, 2008 · N501TR · Airbus A300B4203 · Elevator, Plate/Skin
  > DURING M96 CHECK, WHEN ACCOMPLISHING CPCP TASK CARD 55-2007-0602-1-01 SEVERAL AREAS OF CORROSION WERE FOUND OUT OF LIMITS ON LT ELEVATOR SKIN FROM CENTER LINE RIVETS TO I/B END CAP. REPLACED ELEVATOR IAW A300 MM 27-31-24.
- [SDR WRNA200800017](https://openairdocs.org/sdr/WRNA200800017.md): Seat Track · corroded · Feb 26, 2008 · N501TR · Airbus A300B4203 · Fuselage, Seat/Cargo Attach Fittings
  > DURING M96 CHECK, WHEN ACCOMPLISHING CPCP TASK CARD ZL-220-L403-9-01, CABIN SEAT TRACK WAS FOUND CORRODED AT FRAME 13B - 14C LBL 55. REMOVED AND REPLACED SEAT TRACK SECTION BETWEEN FRAME 13B - 14C LBL 55 IAW A300 SRM 51-30-30 WITH SEAT TRACK FABRICATED FROM E
- [SDR WRNA200800016](https://openairdocs.org/sdr/WRNA200800016.md): Skin · damaged · Feb 26, 2008 · N501TR · Airbus A300B4203 · Fuselage Main, Plate/Skin
  > DURING M96 CHECK, A 8 INCH BY 2 INCH CUT WAS FOUND IN SKIN BETWEEN FRAME 51 AND 52 AT STRINGER 36R TO 39R AFT OF RMLG DOOR CUT OUT. INSTALLED SKIN REPAIR DOUBLER AT FUSELAGE FRAME 51 TO 52 AND STRINGER 36R TO 39R IAW A300 SRM 53-10-10.
- [SDR WRNA200800023](https://openairdocs.org/sdr/WRNA200800023.md): Attach Fitting · corroded · Feb 23, 2008 · N501TR · Airbus A300B4203 · Elevator Tab, Attach Fittings
  > DURING M96 CHECK, CORROSION WAS FOUND OUT OF LIMITS ON NR 3 (FROM OUTBOARD END) LEFT ELEVATOR ATTACH HINGE AT BONDING WIRE ATTACH POINT. REPLACED HINGE ATTACH IAW A300 M/M 55-51-31.
- [SDR WRNA200800003](https://openairdocs.org/sdr/WRNA200800003.md): Damper · failed · Jan 25, 2008 · N501TR · Airbus A300B4203 · Main Landing Gear
  > AFTER TAKEOFF FROM IND, GEAR FAILED TO RETRACT ON BOTH SYSTEM A AND B, DIVERTED TO GSO, DUMPED APPROX 15,000 POUNDS OF FUEL AND MADE A SAFE LANDING. FOUND LEFT INBOARD PITCH DAMPER AT FAULT, REPLACED INBOARD PITCH DAMPER IAW A300 MM 32-11-15 PG 410, LEAK CHEC
- [SDR DHLA200800004](https://openairdocs.org/sdr/DHLA200800004.md): Uplock Switch · malfunctioned · Jan 10, 2008 · N364DH · Airbus A300B4203 · Landing Gear Door Retract Section
  > FLT 165, RIGHT MAIN GEAR DOOR DID NOT RETRACT AFTER GEAR EXTENDED. ABNORMAL PROCEDURE ACCOMPLISHED. CLEANED AND RESECURED RT MLG INBD DOOR UPLOCK SWITCHES, OPERATED GEAR DOORS. NO DEFECTS NOTED, REF M/M 32-30-00. OPS NORMAL AT THIS TIME. ACFT GROUNDED.
- [SDR DHLA200800003](https://openairdocs.org/sdr/DHLA200800003.md): Skin · damaged · Jan 6, 2008 · N365DH · Airbus A300B4203 · Fuselage Main, Plate/Skin
  > LOWER FORWARD CARGO DOOR FUSELAGE LOWER FORWARD FRAME IS SCUFFED. DEFERRED IAW GMM 3.5 CAT I & LETTER REF. 942-057506/014/2008 ACCEPTABLE FOR 10 F.C. PLACARD INSTALLED.
- [SDR WRNA200700064](https://openairdocs.org/sdr/WRNA200700064.md): Damper · malfunctioned · Dec 28, 2007 · N510TA · Airbus A300B4203 · Landing Gear Retraction/Extension System
  > AFTER DEPARTURE WHEN RAISING GEAR, LEVER WOULD NOT GO PAST THE MID POSITION, GEAR POSITION LIGHTS REMAINED 'GREEN'. RETURNED TO FIELD AND MADE A SAFE LANDING. AIRCRAFT MAINTENANCE FERRIED TO CTS IN JAPAN FOR CORRECT ACTION. REPLACED LT GEAR PITCH DAMPER, AI
- [SDR DHLA200700095](https://openairdocs.org/sdr/DHLA200700095.md): Power Supply · no test · Dec 27, 2007 · N367DH · Airbus A300B4203 · Emergency Lighting
  > EMERGENCY EXIT LIGHT OVER THE R1 WILL NOT TEST. REPLACED R1 EMERGENCY LIGHT POWER SUPPLY AS PER MM 33-51-14. OPS NORM.
- [SDR WRNA200700062](https://openairdocs.org/sdr/WRNA200700062.md): B-Nut · loose · Dec 18, 2007 · N504TA · Airbus A300B4203 · Turbine Engine Oil System
  > AFTER LEVELING OFF AT 27,000' OBSERVED STEADY DECLINE IN OIL QUANTITY OF NUMBER 1 ENGINE, RETURNED TO FIELD AND MADE A SAFE LANDING, NO LOSS OF OIL PRESSURE. FOUND AND SECURED A LOOSE 'B' NUT AT AFT BEARING LINE, RE-SERVICED OIL AND ACCOMPLISHED LEAK CHECK, N
- [SDR DHLA200700081](https://openairdocs.org/sdr/DHLA200700081.md): Autobrake Sys · malfunctioned · Dec 12, 2007 · N367DH · Airbus A300B4203 · Brake
  > DURING ROLL OUT WITH AUTOBRAKES ENGAGE (MIN) AFTER PRESSING BRAKES AUTO BRAKES CONTINUED TO BRAKE THE AIRCRAFT EVEN WITH THE AUTO BRAKE OFF LIGHT ILLUMINATED AND NO PRESSURE ON BRAKE PEDALS. PERFORMED OPERATIONAL CK OF AUTOBRAKE AND LIFT DUMPING CKS NORMAL IA
- [SDR DHLA200700079](https://openairdocs.org/sdr/DHLA200700079.md): Sequence Valve · malfunctioned · Dec 8, 2007 · N364DH · Airbus A300B4203 · Landing Gear Retraction/Extension System
  > UPON GEAR RETRACTION, RT MAIN GEAR WOULD NOT RETRACT. UNSAFE LIGHT AND GEAR DOOR LIGHTS BOTH ILLUMINATED. PERFORMED LANDING GEAR UNSAFE INDICATION ABNORMAL PROCEDURE. LOWERED GEAR. GOT ALL 3 GREEN. CONTACTED MAINT AND FLIGHT CONTROL. RETURNED TO JFK.
- [SDR DHLA200700067](https://openairdocs.org/sdr/DHLA200700067.md): Light · inoperative · Nov 23, 2007 · N363DH · Airbus A300B4203 · Emergency Lighting
  > EMERGENCY EXIT LIGHT DISARM WARNING DOES NOT ILLUMINATE. REPLACED LIGHT BULBS ON DISARM CAPSULE PER MM 33-51-00. OPS TEST OK.
- [SDR WRNA200700060](https://openairdocs.org/sdr/WRNA200700060.md): Duct · broken · Oct 31, 2007 · N506TA · Airbus A300B4203 · Pneumatic Distribution System
  > DURING TAKE OFF, NR 2 ENGINE EGT EXCEEDED 960 C, POWER WAS REDUCED BELOW TAKEOFF SETTING, EGT DROPPED BELOW 945 C. DURING CLIMB, NR 2 ENGINE MANIFOLD PRESS 10 PSI, BLEED VALVE REGULATOR LIGHT ON, THEN NR 2 -B- LOOP LIGHT ILLUMINATED, SWITCHED TO -A- LOOP, -A-
- [SDR WRNA200700058](https://openairdocs.org/sdr/WRNA200700058.md): Line · obstructed · Oct 23, 2007 · N510TA · Airbus A300B4203 · Airspeed/Mach Indicator
  > DURING TAKEOFF ROLL, FIRST OFFICERS AIR SPEED LAGGED BEHIND CAPTAINS BY 40-60 KNOTS, ABORTED TAKEOFF. FLUSHED DEBRIS FROM PITOT PRESSURE LINES, ACCOMPLISHED PITOT/STATIC TEST IAW 34-11-10 PAGE 501. TEST NORMAL. AIRCRAFT RELEASED FOR SERVICE.
- [SDR WRNA200700057](https://openairdocs.org/sdr/WRNA200700057.md): Pitot Tube · leaking · Oct 23, 2007 · N510TA · Airbus A300B4203 · Airspeed/Mach Indicator
  > DURING TAKEOFF THE FIRST OFFICERS AIRSPEED INDICATOR LAGGED 40-60 KNOTS BEHIND CAPTAINS AIRSPEED INDICATOR. FOUND RT PITOT PROBE LEAKING, REPLACED RT PITOT PROBE IAW A300 MM 34-11-15 PAGE 401. ACCOMPLISHED LEAK CHECK IAW A300 MM 34-11-10 PAGE 501. AIRCRAFT
- [SDR WRNA200700051](https://openairdocs.org/sdr/WRNA200700051.md): Circuit Breaker · weak · Oct 18, 2007 · N510TA · Airbus A300B4203 · Electrical Power System Wiring
  > AFTER TAKEOFF, FUEL PUMP NR 1; 1A; 2 CIRCUIT BREAKERS POPPED, AND AFCS AND FLIGHT ENGINEER PANEL LIGHTS WENT OFF. RETURNED TO FIELD AND MADE A SAFE LANDIBG. REPLACED FAULTY BREAKER IN 101VU PANEL.
- [SDR DHLA200700053](https://openairdocs.org/sdr/DHLA200700053.md): Hydraulic System · contaminated · Oct 12, 2007 · N362DH · Airbus A300B4203 · Hydraulic System, Main
  > WITH ANTI-SKID IN ON /ALT THE LEFT BRAKES GRAB AND PULL AIRCRAFT TO THE LEFT. BLED BRAKING SYS GREEN AND YELLOW AND OPS CK NORMAL PER MM 32-42-00.
- [SDR WRNA200700065](https://openairdocs.org/sdr/WRNA200700065.md): Bulkhead · cracked · Oct 11, 2007 · N510TA · Airbus A300B4203 · Fuselage Main, Bulkhead
  > DURING ACCOMPLISHMENT OF CPCP TASK C53-310-02-00 AT M96 CHECK, LEVEL II CORROSION WAS FOUND ON AFT PRESSURE BULKHEAD AT STR TIE END ANGLE FITTING AT 35R. FABRICATED FITTING FROM 7076 T6511 EXTRUSION IAW SRM 51-10-40. APPLIED PROTECTIVE COATINGS IAW SRM 51-40

Next page: https://openairdocs.org/model/airbus-industrie-a300-b4-203/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 aircraft_model_key = 'A300B4203'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/airbus-industrie-a300-b4-203/reports

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