# Service difficulty reports: Airbus Industrie A310-221

A list on [Airbus Industrie A310-221](https://openairdocs.org/model/airbus-industrie-a310-221.md).

Newest first. General aviation reporting is voluntary.

- [SDR FDEA201009273752](https://openairdocs.org/sdr/FDEA201009273752.md): Controller · malfunctioned · Sep 27, 2010 · N416FE · Airbus A310221 · Fuel Quantity Indicator
  > BEFORE DESCENT, NOTICED R INNER TANK QTY WAS DEPLEATING AT A MUCH HIGHER RATE THAN THE LT INNER TANK. SUSPECTED A FUEL LEAK AND CONSULTED THE QRH. IAW QRH PROCEDURE ACCOMPLISHED AN INFLIGHT SHUTDOWN. PERFORMED INSP ON NR 2 ENG FOR FUEL LEAK AND WET MOTORIN
- [SDR FDEA201005111507](https://openairdocs.org/sdr/FDEA201005111507.md): Actuator · leaking · May 11, 2010 · N416FE · Airbus A310221 · Drag Control Actuator
  > LT WING NR 6 SPOILER ACTUATOR LEAK. PRESSURED THE HYD SYS CK LEAKAGE IAW AMM 29-10-00-3. REPLACED THE LT NR 6 SPOILER ACTUATOR IAW AMM 27-64-14-4, RESULT:10 DROPS/10MIN CARRIED OUT OPS TEST OF ROLL TEST IAW AMM27-11-00-5 AND LEAK CHECK. TEST OK AND NO LE
- [SDR FDEA200911123938](https://openairdocs.org/sdr/FDEA200911123938.md): Actuator · worn · Nov 12, 2009 · N416FE · Airbus A310221 · Landing Gear Actuator
  > LDG GEAR WOULD NOT RETRACT AFTER T/O. REMOVED AND REPLACED LT MLG BOGIE BEAM PITCH DAMPER ACTUATOR IAW AMM 32-11- PERFORMED JACKING FOR ACFT MX OPERATION FOR LANDING GEAR EXTENSION AND RETRACTION TEST ON SYS 1 AND SYS 2. RET/EXT SATISFACTORY IAW AMM 07-
- [SDR FDEA200901300405](https://openairdocs.org/sdr/FDEA200901300405.md): Unknown · unknown · Jan 30, 2009 · N416FE · Airbus A310221 · Drag Control System
  > LOST SPOILER NR 7 FOLLOWED BY BLUE HYD PRESSURE/FLUID LOSS ON INITIAL T/O ROLL. RTO AT 50KTS. ON BLOCK PERFORM INSPECTION FOR SIGN OF LEAKAGE, NO LEAK FOUND. COCKPIT CHK BLUE HYD INDICATION AT LOWER BAND OF SVC RANGE. SERVICE TO TOP HAT RANGE AS PER SMP
- [SDR 08FDEA03220](https://openairdocs.org/sdr/08FDEA03220.md): Adapter · worn · Aug 3, 2008 · N430FE · Airbus A310221 · Fuselage Main, Structure
  > MDCC BETWEEN SEAT TRACK 2R AND 3R FRAME 38 CARGO LOADING SYSTEM ADAPTER HAS 2 EACH AREAS OF WORN SCALLOPS. REMOVED WORN CLS ADAPTER AND INSTALLED NEW CLS ADAPTER BETWEEN SEAT TRACK 2R AND 3R FRAME 38 IAW A310-200 SRM 51-40-21 AND SRM 51-72-10.
- [SDR 08FDEA00377](https://openairdocs.org/sdr/08FDEA00377.md): Skin · chafed · Feb 11, 2008 · N416FE · Airbus A310221 · Engine Thrust Reverser
  > NR 1 ENGINE INBOARD THRUST REVERSER INTERIOR SKIN CHAFED JUST BELOW DEOILER EXHAUST PORT, NAC STATION 385,4:00 POSITION. REPAIRED PER EA NR 6-7800-113019, EXHAUST, NR 1 ENGINE INBOARD T/R AFT BARREL SKIN DOUBLER, REPAIR.
- [SDR 08FDEA00316](https://openairdocs.org/sdr/08FDEA00316.md): Bracket · corroded · Jan 28, 2008 · N416FE · Airbus A310221 · Horizontal Stabilizer Miscellaneous Structure
  > THS LEFT LOWER BODY FAIRING FWD ATTACH BRACKET ANGLE CORRODED LOWER SURFACE, CENTER BOX AREA, ANGLE IS PART OF LEADING EDGE. REMOVED AND REINSTALLED LOWER APRON IAW A310-200 SRM 51-40-21. REMOVED AND REINSTALLED RIB ASSY IAW A310-200 SRM 51-40-21. REMOV
- [SDR 08FDEA00312](https://openairdocs.org/sdr/08FDEA00312.md): Bracket · corroded · Jan 28, 2008 · N416FE · Airbus A310221 · Horizontal Stabilizer Miscellaneous Structure
  > THS LEFT UPPER BODY FAIRING FWD ATTACH BRACKET ANGLE CORRODED, CENTER BOX AREA, ANGLE IS PART OF LEADING EDGE. REMOVED AND REINSTALLED UPPER APRON IAW A310-200 SRM 51-40-21. REMOVED AND REINSTALLED RIB ASSY IAW A310-200 51-40-21. REMOVED UPPER ATTACH PLATE
- [SDR 08FDEA00303](https://openairdocs.org/sdr/08FDEA00303.md): Seat Track · cracked · Jan 27, 2008 · N416FE · Airbus A310221 · Fuselage, Seat/Cargo Attach Fittings
  > NR 4 LT ARTICULATING SEAT TRACK IS CRACKED. REMOVED AND REPLACED LT NR 4 ARTICULATING SEAT TRACK PO NR 602215.2 REF FEDEX A310-200 W/C E-6-5310-7-3322 PT2 SEAT AND DUMMY TRACKS ATTACHMENT FITTINGS INSPECTION.
- [SDR 08FDEA00302](https://openairdocs.org/sdr/08FDEA00302.md): Seat Track · cracked · Jan 27, 2008 · N416FE · Airbus A310221 · Fuselage, Seat/Cargo Attach Fittings
  > NR 4 LT ARTICULATING SEAT TRACK IS CRACKED. REMOVED AND REPLACED LT NR 4 ARTICULATING SEAT TRACK PO NR 602215.2 REF FEDEX A310-200 W/C E-6-5310-7-3322 PT2 SEAT AND DUMMY TRACKS ATTACHMENT FITTINGS INSPECTION.
- [SDR 08FDEA00263](https://openairdocs.org/sdr/08FDEA00263.md): Heat Shield · cracked · Jan 24, 2008 · N416FE · Airbus A310221 · Nacelle/Pylon Miscellaneous Structure
  > PYLON NR 1 FWD ENG MOUNT, HEAT SHIELD CRACKED (MKD). REMOVED HEAT SHIELD NR 1 ENG PYLON IAW FEDEX A310-200 SRM 51-40-21 PAGE 1. RECEIVED NEW HEAT SHIELD P/N A2611501200200 S/N IC673554 PO 605041.1 FROM SUPPLY. INSTALLED NEW HEAT SHIELD IAW FEDEX A310-200 S
- [SDR 08FDEA00244](https://openairdocs.org/sdr/08FDEA00244.md): Skin · corroded · Jan 23, 2008 · N416FE · Airbus A310221 · Elevator, Plate/Skin
  > RT ELEVATOR APPROX STA 623 LOWER SKIN CORRODED. REPAIRED RT ELEVATOR LWR SKIN CORROSION BY REMOVING DAMAGED SKIN, AND FABING SKIN PLUG AND DOUBLER, BONDING SKIN PLUG AND DOUBLER, EDGE SEALING REPAIR, AND REFINISHING IAW A310-200 SRM 51-77-12 FIG 224.
- [SDR 08FDEA00243](https://openairdocs.org/sdr/08FDEA00243.md): Skin · corroded · Jan 23, 2008 · N416FE · Airbus A310221 · Elevator, Plate/Skin
  > RT ELEVATOR APPROX STA 529 TOP SURFACE SKIN CORRODED. REPAIRED RT ELEVATOR UPPER SKIN CORROSION BY REMOVING DAMAGED SKIN, AND FABING SKIN PLUG AND DOUBLER, BONDING SKIN PLUG AND DOUBLER, EDGE SEALING REPAIR, AND REFINISHING IAW A310-200 SRM 51-77-12 FIG 2
- [SDR 08FDEA00232](https://openairdocs.org/sdr/08FDEA00232.md): Skin · corroded · Jan 23, 2008 · N416FE · Airbus A310221 · Elevator, Plate/Skin
  > RT ELEVATOR APPROX STA 623 LOWER SKIN CORRODED.
- [SDR 08FDEA00231](https://openairdocs.org/sdr/08FDEA00231.md): Skin · corroded · Jan 23, 2008 · N416FE · Airbus A310221 · Elevator, Plate/Skin
  > RT ELEVATOR APPROX STA 529 TOP SURFACE SKIN CORRODED. REPAIRED RT ELEVATOR UPPER SKIN CORROSION BY REMOVING DAMAGED SKIN, AND FABING SKIN PLUG AND DOUBLER, BONDING SKIN PLUG AND DOUBLER, EDGE SEALING REPAIR, AND REFINISHING IAW A310-200 SRM 51-77-12 FIG 224
- [SDR 08FDEA00209](https://openairdocs.org/sdr/08FDEA00209.md): Rib · cracked · Jan 21, 2008 · N416FE · Airbus A310221 · Wing, Rib/Bulkhead
  > CRACKED, R/WING SPOILER NR 3 IBD BOX HINGE RIB. REMOVED PANEL IAW A310-200 SRM 51-40-21 PG 7. CUT AND REMOVED CRACKED END RIB IAW A310-200 SRM 57-51-11 PG 227 AND 228. LOCATED, DRILLED AND DEBURRED ITEM 1, ITEM 2, AND ITEM 3 IAW A310-200 SRM 57-51-11 PG 222
- [SDR 08FDEA00202](https://openairdocs.org/sdr/08FDEA00202.md): Sill · corroded · Jan 18, 2008 · N416FE · Airbus A310221 · Fuselage Miscellaneous Structure
  > BULK CARGO DOOR CUTOUT LOWER SILL CORROSION AFT SECTION. MARKED REMOVED AND REPLACED LOWER SILL BEAM IAW A310-200 SRM 53-17-18 FIG 6 SHT 8 AND 51-40-21.
- [SDR 08FDEA00119](https://openairdocs.org/sdr/08FDEA00119.md): Skin · misrepaired · Jan 13, 2008 · N416FE · Airbus A310221 · Fuselage Main, Plate/Skin
  > EVALUATION OF FUSELAGE NOSE REPAIR (AERODYNAMIC BODY FILLER) BETWEEN FRAMES 3 AND 4 CENTERLINE, JUST AFT OF LOWER EDGE OF RADOME. EVALUATED REPAIR, FOUND REPAIR NOT TO CONFORM TO FEDEX SRM. REMOVED DAMAGED AREA IAW 53-11-12 FIG 201. FABRICATED AND INSTALLED
- [SDR 08FDEA00027](https://openairdocs.org/sdr/08FDEA00027.md): Beam · corroded · Jan 3, 2008 · N416FE · Airbus A310221 · Nacelle/Pylon Miscellaneous Structure
  > NR 2 ENGINE PYLON AFT BEAM ATTACHMENT MOUNT HAS SEVERE RUST ON BOTTOM FACE OF MOUNT. CLEANED BEAM ASSY. IAW AMM 54-51-00-6.5 B-1. REMOVED CORROSION FROM BEAM SURFACE IAW 54-51-00-6.5 B-1 & SRM 51-74-10 ITEM 7 B-2, ITEM 5 A-5 & PMS 01-01-14-1. POLISHED REWORK
- [SDR 08FDEA00026](https://openairdocs.org/sdr/08FDEA00026.md): Beam · corroded · Jan 3, 2008 · N416FE · Airbus A310221 · Engine Mount Section
  > NR 2 ENGINE PYLON AFT BEAM ATTACHMENT MOUNT AFT SIDE, 2 PLACES, UPPER END EMITTING RUST. REMOVED & REPLACED NR 2 ENG. MOUNT SHIM REF AMM 54-54-86-4 2B-3. PRIMED SHIM REF AMM 54-51-00-6 PG. 5. MATCH DRILLED SHIM REF SRM 51-4-44. REMOVED & REINSTALLED PRE COOL
- [SDR 08FDEA00025](https://openairdocs.org/sdr/08FDEA00025.md): Mount · corroded · Jan 3, 2008 · N416FE · Airbus A310221 · Engine Mount Section
  > NR 1 ENGINE PYLON AFT ENGINE MOUNT LOWER SURFACE LIGHT CORROSION AROUND LEFT AND RIGHT OUTBOARD SIDES. CLEANED ASSY IAW AMM 54-51-00 6.5 B.P1 REMOVED CORRSION FROM ASSY SURFACE IAW SRM 51-74-10 ITEM 7 B-2 & PMS 01-01-14-1, POLISHWED REWORK AREA IAW AMM 54-51-0
- [SDR 08FDEA00022](https://openairdocs.org/sdr/08FDEA00022.md): Support Angle · cracked · Jan 3, 2008 · N416FE · Airbus A310221 · Wing Miscellaneous Structure
  > LEFT WING UPPER SURFACE TRAILING EDGE PANEL NR 575BT CUTOUT SUPPORT ANGLE CRACKED AT STATION 490. CLEANED AREA IAW FEDEX A310-200 SRM 51-23-10 PG 1. ACCOM. HFEC INSP. PER A310 NTM 51-10-08. VERIFIED AREA IS CRACKED. USED TOOL TWS 8209A. UNABLE TO MARK END OF
- [SDR 06FDEA1306](https://openairdocs.org/sdr/06FDEA1306.md): Selector Valve · malfunctioned · Apr 4, 2006 · N416FE · Airbus A310221 · Engine Thrust Reverser
  > SHORTLY AFTER T/O, NR 2 REVERSER UNLOCK LIGHT ILLUMINATED WITH ECAM WARNING LIGHT STAYED ON FOR APPROX 30 SEC, FLICKERED AND WENT OUT. THE LIGHT AND ECAM WARNING CAME ON AGAIN A FEW SECONDS LATER IT STAYED ILLUMINATED FOR SEVERAL MINUTES AND WENT OUT, AT NO T
- [SDR 01FDEA01000](https://openairdocs.org/sdr/01FDEA01000.md): Warning System · activated · Nov 17, 2001 · N416FE · Airbus A310221 · Engine EGT/TIT Indicating System
  > ON CLIMBOUT NR 1 EGT PEGGED AT MAX GAUGE NOSE GEAR SHOW UNSAFE.
- [SDR 00FDEA00625](https://openairdocs.org/sdr/00FDEA00625.md): Elevator · malfunctioned · Sep 5, 2000 · N448FE · Airbus A310221 · Elevator Control System
  > AFT 20 MIN OF FLT A/C HAD A AIR TURNBACK DUE TO TOO MUCH PRESS NEEDED TO OPERATE ELEVATOR. AC RETURN TO LAX.
- [SDR 00FDEA00464](https://openairdocs.org/sdr/00FDEA00464.md): Controller · failed · Jul 19, 2000 · N446FE · Airbus A310221 · Cabin Pressure Controller
  > AIR TURNBACK, FOR MULTIPLE FAILURES. NR 1, 2 PITCH TRIM, NR 2 A.T.S, NR 1, 2 TRANSPONDERS, NR 1 CABIN PRESS, CAPT TAT WARNING, CAPT A.S. & PFD. *S/D* REMOVED AND REPLACED RLY 10XE, PROX DET UNIT, NR 2 TRANSFORMER RECTIFIER MM 24-32-00-/5, MM 32-61-00/501.
- [SDR 00FDEA00406](https://openairdocs.org/sdr/00FDEA00406.md): Engine · failed · Jun 25, 2000 · N446FE · Airbus A310221 · Engine (Turbine/Turboprop)
  > AFT 20 MIN OF FLT, CREW HEARD LOUD BANG, NR 2 ENGINE FAILED. NO IND ON N1 OR N2 IND''S. AC RETURNED TO MEM.
- [SDR 99FDEA00236](https://openairdocs.org/sdr/99FDEA00236.md): Pitot System · dirty · Jun 24, 1999 · N448FE · Airbus A310221 · Pitot/Static System
  > 99-143 - NO AIRSPEED IND ON F/O SIDE PFD ON T/O. RTO AT 70 KNOTS. PERF ADC NR 2 OPS CK IAW MM 34-10-00 SYS CK GOOD. FLUSHED NR 2 PITOT SYS IAW 34-10-00, FOUND DEBRIS IN F/O PITOT TUBE, SYS OK FOR SERVICE.
- [SDR 99FDEA00233](https://openairdocs.org/sdr/99FDEA00233.md): Adc · inoperative · Jun 23, 1999 · N448FE · Airbus A310221 · Air Data Computer
  > NO AIRSPEED IND ON TAKEOFF ROLL. ALL PFD SYMBOLS WERE PRESENT BUT CAPT AIRSPEED TRIANGLE NEVER INCREASED FROM 0. REMOVED AND REPLACED NR 1 ADC IAW M/M 34-11-34, SYSTEM OK FOR SERVICE.
- [SDR 99FDEA00234](https://openairdocs.org/sdr/99FDEA00234.md): Airspeed Ind · inoperative · Jun 22, 1999 · N448FE · Airbus A310221 · Airspeed/Mach Indicator
  > CAPT HAD NO AIRSPEED INDICATION ON PFD DURING T/O. ABORTED AT 70 KNOTS. F/O AND STBY AIRSPEED INDICATE NORMAL.
- [SDR 98FDEA00480](https://openairdocs.org/sdr/98FDEA00480.md): Control Handle · failed · Jul 30, 1998 · N448FE · Airbus A310221 · Landing Gear Selector
  > 98-0188 STA-IND - AFTER T/O LANDING GEAR WOULD NOT RETRACT UNLOCK AND GREEN DIAMONDS ON ALL 6 INDICATORS. BOTH SYS 1 AND SYS 2 ON POSITION DETECTOR SWITCH TRIED MULTIPLE TIMES. REMOVED AND REPLACED LAND GEAR CONTROL HANDLE MODULE PER M/M 32-30. PERFORMED G
- [SDR 97FDEA00808](https://openairdocs.org/sdr/97FDEA00808.md): Engine · flamed out · Nov 6, 1997 · N446FE · Airbus A310221 · Engine (Turbine/Turboprop)
  > NR 1 ENGINE FLAMED OUT DURING CRUISE AT 5,000 FT, NO PRIOR INDICATIONS. CONT RELIGHT PLACED ON AND ENGINE RELIT IMMEDIATELY, N1 ROLLED BACK FROM APPROX 70 PERCENT TO 40 PERCENT BEFORE RELIGHT. FAILURE OCCURRED SHORTLY OR DURING AN AUTOTHROTTLE-COMMANDED POWE
- [SDR 97FDEA00561](https://openairdocs.org/sdr/97FDEA00561.md): Pitot Line · clogged · Aug 16, 1997 · N448FE · Airbus A310221 · Pitot/Static System
  > ON DEPARTURE CAPTS AIRSPEED TAPE WAS SHOWING ERRONEOUS SPD IND. SWIT TO ALT SPD TAPE RETURNED TO OPERATION BUT SPD WAS 300 KTS WHEN F/O WAS 160 KTS. SWITCHED TO ALT EFIS NO CHANGE. AFTER FLAP/SLAT RETRACT NR 1 YAW DAMPER FAILED AUTO THROTTLE SYS FAILED WOUL
- [SDR 97FDEA00170](https://openairdocs.org/sdr/97FDEA00170.md): Fuel Control · out of adjust · Mar 14, 1997 · N448FE · Airbus A310221 · Fuel Control/Turbine Engines
  > ON TAXI IN AT IDLE POWER, NR 1 ENG FLAMED OUT WITH CORRESPONDING ENG FAIL ECAM WARNINGS. FOR INFORMATION, 25-30 KT TAILWIND WAS PRESENT WHEN ENG FAILED. ENGINE RUN PERFORMED AND GROUND IDLE SPEED FOUND TO BE LOW. TEST NR 9 FUEL CONTROL TRIM PERFORMED IAW M/
- [SDR 96FDEA01696](https://openairdocs.org/sdr/96FDEA01696.md): Controller · malfunctioned · Dec 5, 1996 · N419FE · Airbus A310221 · Cabin Pressure Controller
  > CLIMBOUT APPROX 8,000 FT, RECEIVED RED ECAM WARNING LWR ACCESS DOOR NOT CLOSED, FOLLOWED BY EXCESSIVE CABIN RATE. ACCOMPLISHED ECAM. CABIN RATE CLIMBED AT SAME RATE AND ALTITUDE AS A/C DESCENDED TO 10,000 FT MADE PRECAUTIONARY LANDING KUL. LONG HISTORY OF P
- [SDR 96FDEA01687](https://openairdocs.org/sdr/96FDEA01687.md): Regulator · malfunctioned · Nov 21, 1996 · N419FE · Airbus A310221 · Pressure Regulator/Outflow Valve
  > AFTER NR 2 ENG START CABIN AUTO PRESS NR 2 AND NR 2 REGULATOR FAIL, NR 1 SYS OK. AFTER TAKEOFF UNABLE TO PRESSURIZE CABIN IN AUTO OR MANUAL. THE OVERRIDE AND ECAM OUTFLOW VALVE POSITION INDICATED CLOSED. RESET NR 2 AUTO FLOW VALVE AND CONTROLLER C/B'S. ALS
- [SDR 96FDEA01684](https://openairdocs.org/sdr/96FDEA01684.md): Tr Cowl · damaged · Nov 20, 1996 · N448FE · Airbus A310221 · Engine Thrust Reverser
  > UPON ARRIVAL, DURING WALKAROUND FOUND APPROX 18 DIA HOLE ON AFT INBD EDGE OF NR 2 ENGINE FAN COWL. ALSO, NOTED SEVERE DISCOLORATION ON INBD REVERSER HALF WITH BURN STREAKS AND STRUCTURAL DAMAGE TO THE REVERSER. *S/D* REMOVED AND REPLACED GROUND THRUST REV C
- [SDR 96FDEA01634](https://openairdocs.org/sdr/96FDEA01634.md): Actuator Rod · sheared · Oct 29, 1996 · N419FE · Airbus A310221 · Cargo/Baggage Doors
  > REPORTED BY RAMP PERSONNEL. WHILE OPENING THE MDC DOOR. A LOUD SOUND WAS HEARD. MX DISCOVERED THAT THE MDC DOOR ACTUATOR ROD-END SHEARED. *S/D* REMOVED AND REPLACED MDC DOOR ACTUATOR PER M/M 52-36-27 AND TESTED PER M/M 52-36-00, CHECK OK.
- [SDR 96FDEA01415](https://openairdocs.org/sdr/96FDEA01415.md): O-Ring · failed · Aug 28, 1996 · N419FE · Airbus A310221 · Hydraulic System, Main
  > STA SFS - APPROX 1 HOUR INTO CRUISE, ECAM REPORTED GREEN HYD SYS RESERVOIR LOW OVERHEAD AND SYS PAGE AGREED. ACCOMPLISHED PROCEDURE, SHUT DOWN GREEN SYSTEM. MANUALLY EXTENDED GEAR. CHECKED AND FOUND HYD GREEN SYS GREEN ELECTRO HYD SELECTOR FITTING LEAKING.
- [SDR 96FDEA01391](https://openairdocs.org/sdr/96FDEA01391.md): Gcu · malfunctioned · Aug 26, 1996 · N417FE · Airbus A310221 · AC Regulator
  > NR 1 GENERATOR FAULT WITH INTERMITTENT NR 1 IDG FAULT. GENERATOR DID RESET BUT STILL HAD NR 1 IDG FLASHING. *S/D* PERFORMED OPS CHECK OF AIR/COOLER, CHECKS GOOD. REMOVED AND REPLACED NR 1 GCU, OPS CK'D GOOD.
- [SDR 96FDEA01238](https://openairdocs.org/sdr/96FDEA01238.md): Hyd Line · leaking · Jul 11, 1996 · N418FE · Airbus A310221 · Hydraulic System, Main
  > STA KHH LOST GREEN HYD SYS DURING DESCENT PERFOMED ECAM ITEMS. WHEN A/C ARRIVED CK'D GREEN RSVR QTY AND FOUND LOWER THAN HAT ARC. T/S FOUND HYD FLUID LEAKING FROM LT INSIDE WING SPAR BETWEEN PYLON AND 1ST FLAP TRACK IT IS A RIDGID LINE FOR AILERON DROOP RUBB
- [SDR 96FDEA00037](https://openairdocs.org/sdr/96FDEA00037.md): Structure · vibration · Jan 10, 1996 · N416FE · Airbus A310221 · Aircraft Structures
  > AFTER TAKEOFF WITH GEAR UP, A/C STARTED VIBRATING. GEAR WAS CYC DOWN & UP WITH NO PROBLEMS. VIB CONTD. LEVEL OFF AT 5000 FEET. FLAPS/SLATS RETRACTED, VIBRATION STOPPED AT PWR REDUCTION (VIB WAS MOD). RETND FOR LANDING WITH NORMAL SLAT/FLAP EXTENSION & NO

## 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 = 'A310221'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/airbus-industrie-a310-221/reports

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