# Service difficulty reports: Airbus Industrie A310-222

A list on [Airbus Industrie A310-222](https://openairdocs.org/model/airbus-industrie-a310-222.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 26 · 1,281 reports

- [SDR FDEA201512194038](https://openairdocs.org/sdr/FDEA201512194038.md): Fairing · damaged · Dec 19, 2015 · N453FE · Airbus A310222 · Trailing Edge Flaps
  > LEFT WING INBD FLAP FAIRING HANGING DOWN ON ARRIVAL. RELEASED FOR SERVICE IAW CDL 27-01, B CATEGORY. FLAP TRACK FAIRING MISSING, REFER TO CDL 27-01-B FOR RESTRICTIONS. REMOVED LT WING FARING NR 2 WITH ASSOCIATED HARDWARE & SENT TO STRUCTURES FOR POSSIBLE RE
- [SDR FDEA201512023853](https://openairdocs.org/sdr/FDEA201512023853.md): Adapter · loose · Dec 2, 2015 · N453FE · Airbus A310222 · Fuel Indicating System
  > DEPARTED WITH 62,000 POUNDS OF FUEL, AT LANDING FUEL QTY INDICATES 61,400 POUNDS OF FUEL. REMOVED AND REPLACED LEFT OUTER ADAPTER PLUGS 42QT1 & 43QT1 PER AMM 28-42-37-04.
- [SDR FDEA201511043464](https://openairdocs.org/sdr/FDEA201511043464.md): Computer · failed · Nov 4, 2015 · N453FE · Airbus A310222 · Central Warning
  > SHORTLY AFTER CLEANUP ON TAKEOFF, MULTIPLE & VARIOUS AURAL & ECAM ALERTS & WARNINGS BEGAN. DECLARED AN EMER & RETURNED, WARNINGS CONTINUED ALL THE WAY TO BLOCK IN. REPLACED NR 1 AND NR 2 FLIGHT WARNING COMPUTERS 1WW1 & 1WW2 IAW AMM 31-53-34-04. PERFORMED FW
- [SDR FDEA201507092174](https://openairdocs.org/sdr/FDEA201507092174.md): Seat Track · damaged · Jul 9, 2015 · N453FE · Airbus A310222 · Fuselage, Seat/Cargo Attach Fittings
  > RAMP REPORTS AFT LOCK IN POSITION 8R LOOSE IN FLOOR, LATCH N1288. LATCH RESTRAINT DEVICE N1288 AT 8R INOPERATIVE, BROKEN OR MISSING. INSTALLED NEW SEAT TRACK SECTION IN IAW SRM 53-10-16. INSTALLED FLOORING & LOADING SYS IAW SRM 51-40-20.
- [SDR FDEA201507092173](https://openairdocs.org/sdr/FDEA201507092173.md): Seat Track · damaged · Jul 9, 2015 · N453FE · Airbus A310222 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND AT POS 8R, LOCK S1288 TO HAVE SEAT TRACK LOBE DAMAGE CAUSING LOCK TO BE LOOSE. LOBE DAMAGE AT LOCK S1288 POS 8R, LOCK INSTALLED BUT LOOSE IN FLOOR. ACFT OK FOR SERVICE. RESTRAINT HAS BEEN REMOVED IAW SR 30-53-003 & MEL HAS BEEN APPLIED. REF WRI 25-5
- [SDR FDEA201505221623](https://openairdocs.org/sdr/FDEA201505221623.md): Switch · faulty · May 22, 2015 · N453FE · Airbus A310222 · Landing Gear Position and Warning
  > LOWERED GEAR, GOT SAFE INDICATION OF GEAR DOWN. A FEW SECONDS LATER GOT UNSAFE GEAR WARNING. LIGHT & HORN IN POS 2 SELECTED SYS 1 & THE LIGHT QAND WARNING HORN WENT OUT.. 3 GREEN DOWN INDICATIONS INSYS 1. SYS 2 HAD 2 GREEN LIGHTS FOR MAIN WHEELS AND NO G
- [SDR FDEA201504101202](https://openairdocs.org/sdr/FDEA201504101202.md): Compensator · failed · Apr 10, 2015 · N455FE · Airbus A310222 · Landing Gear Brake System
  > DURING APPROACH, 2000 & 6 MILES, THE HOT BRAKE LIGHT IN THE CUBE ON THE LG TEST PANEL FLICKERED, FOLLOWED BY ECAM HOT BRAKE WARNINGS FOR ALL 4 WHEELS ON THE LT SIDE, 480, 505. LOWERED GEAR IMMEDIATELY & THE TEMPS KEPT 400, 505 & RISING. FIRE DEPARTMENT SAW
- [SDR FDEA201502120515](https://openairdocs.org/sdr/FDEA201502120515.md): Engine · vibration · Feb 12, 2015 · N453FE · Airbus A310222 · Engine (Turbine/Turboprop)
  > ON TAKEOFF, ACFT STARTED VIBRATING VERY BADLY. FELT MORE LIKE AN AIRFRAME FLUTTER RATHER THAN ENG VIBRATION. CHECKED ENG PAGE, ALL NORMAL. CLIMBING THROUGH 2500' PULLED THROTTLES BACK & FLUTTER DECREASED. AS SPEED STARTED TO INCREASE FLUTTER INCREASED. SL
- [SDR FDEA201412184149](https://openairdocs.org/sdr/FDEA201412184149.md): Panel · damaged · Dec 18, 2014 · N454FE · Airbus A310222 · Wing Main, Frame Structure
  > ON ARRIVAL LT WING TE DAMAGE FOUND. R & R THE LT WING OTBD TE PANEL IAW SRM 57-51-12.
- [SDR FDEA201409102582](https://openairdocs.org/sdr/FDEA201409102582.md): Actuator · failed · Sep 10, 2014 · N455FE · Airbus A310222 · Landing Gear Actuator
  > UPON GEAR RETRACTION, RECEIVED A LT MAIN GEAR RED UNLOCK INDICATION WITH AN AMBER LT DOOR LIGHT. COMPLIED WITH ECAM EXTENDED GEAR & LANDED. WE DID HAVE A LOUD WIND NOISE WITH THE PROBLEM, PRETTY SURE DOOR WAS OPEN. DEBRIEFED CREW & VERIFIED THEY DID ATTEMPT
- [SDR FDEA201408212293](https://openairdocs.org/sdr/FDEA201408212293.md): Sequence Valve · faulty · Aug 21, 2014 · N455FE · Airbus A310222 · Landing Gear Retraction/Extension System
  > DURING CLIMB OUT AT GEAR RETRACTION, LT MAIN GEAR DID NOT APPEAR TO RETRACT & DOOR SHOWED OPEN. ECAM INDICATED LG RETRACTION INOPERATIVE. FUEL CONSUMPTION INCREASED. SELECTED OPPOSITE SYS & CYCLED THE GEAR, NO HELP. COMPLIED WITH ECAM & QRH. DECLARED AN EM
- [SDR FDEA201407131756](https://openairdocs.org/sdr/FDEA201407131756.md): Damper · leaking · Jul 13, 2014 · N453FE · Airbus A310222 · Landing Gear Retraction/Extension System
  > ON DEPARTURE LG WOULD NOT RETRACT. TRIED BOTH SYS 1 & SYS 2 & QRH, NO HELP. RT GEAR PITCH DAMPER POPPED WITH THE REAR SEAL BLOWN ALL THE WAY OUT. R & R RT MAIN GEAR PITCH DAMPER IAW AMM 32-11-15-04-01. FOUND RT MLG BOGIE SENSOR SUPPORT BROKEN CAUSING GEAR
- [SDR FDEA201406021269](https://openairdocs.org/sdr/FDEA201406021269.md): Skin · cracked · Jun 2, 2014 · N453FE · Airbus A310222 · Wing, Plate/Skin
  > POSSIBLE CRACK ON LT WING INBD SLAT CUT OUT, BOTH CORNERS. PERFORMED HFEC OF AREA IAW NTM 51-10-08 BLOCK 601, TWO CRACK INDICATIONS. REPAIRED AREAS, INSTALLED FILLERS AND DOUBLER IAW EA 6-5730-T0308606.
- [SDR FDEA201405221136](https://openairdocs.org/sdr/FDEA201405221136.md): Valve · failed · May 22, 2014 · N455FE · Airbus A310222 · Leading Edge Slat Control System
  > NR 1 SLAT SYS FAULT LIGHT DURING FINAL. RECYCLING DID NOT CORRECT, QRH PROCEDURES ACCOMPLISHED. SLAT FAULT LIGHT REMAINED ON, BUT SPFI SHOWED SLATS & FLAPS 30 & 40 LANDING NORMAL. DECLARED LANDING EMERGENCY. LANDING NORMAL. REMOVED AND REPLACED PCU VALV
- [SDR FDEA201403050452](https://openairdocs.org/sdr/FDEA201403050452.md): Switch · failed · Mar 5, 2014 · N455FE · Airbus A310222 · Engine Thrust Reverser
  > ACCELERATING ABOVE 10,000 & 250 KTS, NR 1 ENGINE THRUST REVERSER UNLOCK ILLUMINATED STEADY. ALL OTHER INDICATIONS NORMAL. TROUBLESHOT IAW TSM 78-31-00, FOUND THE RT MASTER ACTUATOR SECONDARY LOCK SWITCH INOPERATIVE. REMOVED AND REPLACED THE NR 1 ENGINE RT
- [SDR FDEA201402030253](https://openairdocs.org/sdr/FDEA201402030253.md): Pressure Switch · faulty · Feb 3, 2014 · N450FE · Airbus A310222 · Hydraulic System, Main
  > NR 2 ENG GREEN HYD PUMP LOW PRESS WHEN SETTING TAKEOFF POWER. DISCONTINUED TAKEOFF. REMOVED OLD NR 2 ENG GREEN PUMP PRESS SWITCH 112GK & REPLACED WITH NEW SWITCH IAW AMM 29-11-62-04. LEAK & OPERATIONS CHECKED GOOD. ACFT OK TO CONTINUE.
- [SDR FDEA201312243034](https://openairdocs.org/sdr/FDEA201312243034.md): Plate · worn · Dec 24, 2013 · N454FE · Airbus A310222 · Engine Thrust Reverser
  > NR 2 ENG OTBD T/R COWL UPPER MID-SECTION INNER FACE FOUND ONE EACH PLATE WORN BY SPRING SEAL. ACCOMPLISHED THE WORK IAW EA 6-5410-T0208220.
- [SDR FDEA201312243033](https://openairdocs.org/sdr/FDEA201312243033.md): Frame · corroded · Dec 24, 2013 · N454FE · Airbus A310222 · Fuselage Main, Frame
  > FORWARD CARGO COMPARTMENT BILGE FRAME FOUND CORROSION AT FR 39, STRINGER 51R POSITION. CORROSION AREA CUT OUT & REINFORCED WITH REPAIR PART & FITTING TO INSTALLED IAW SRM 53-15-17. THE REPAIR CATEGORY B IAW 53-15-17-2-003-00.
- [SDR FDEA201310252615](https://openairdocs.org/sdr/FDEA201310252615.md): Skin · dented · Oct 25, 2013 · N450FE · Airbus A310222 · Trailing Edge Flaps
  > LT INBD FLAPS T/E LOWER SURFACE HAS NUMEROUS DENTS. FOUND WITHIN LIMITS IAW SRM 57-52-12, FIG 101, DETAIL IV. TWO DENTS, PUNCTURED, REPAIRED DENTS IAW SRM 57-52-12 AND SRM 51-77-12, PARA 4B. MAJOR REPAIR.
- [SDR FDEA201310202564](https://openairdocs.org/sdr/FDEA201310202564.md): Support · corroded · Oct 20, 2013 · N450FE · Airbus A310222 · Wing, Landing Gear Attach Fittings
  > RIGHT MLG RIB 5, FWD LUG LOWER SURFACE IS CORRODED. RT MLG RIB 5 FWD LUG CORROSION. R & R IAW REPAIR DWG R57249389, REV B IAW EA 6-5710-T0302172, PART 1. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201310172530](https://openairdocs.org/sdr/FDEA201310172530.md): Skin · damaged · Oct 17, 2013 · N450FE · Airbus A310222 · Fuselage Main, Plate/Skin
  > FOUND DAMAGE TO SKIN AT FRAME 87 BETWEEN STRINGERS 25-30R, REPAIRED IAW EA 6-5330-T0302997, PART 1. REPAIR CLASSIFIED AS MINOR.
- [SDR FDEA201310172528](https://openairdocs.org/sdr/FDEA201310172528.md): Skin · damaged · Oct 17, 2013 · N450FE · Airbus A310222 · Trailing Edge Flaps
  > RIGHT WING INBD TE FLAPS LOWER SURFACE HAS IMPACT DAMAGE. REPAIRED IAW SRM 57-52-12, PARA 4.D, FIG 204. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201310172532](https://openairdocs.org/sdr/FDEA201310172532.md): Skin · corroded · Oct 17, 2013 · N450FE · Airbus A310222 · Trailing Edge Flaps
  > LEFT OTBD FLAPS T/E LOWER SURFACE HAS CORROSION LOCATED 22 INCHES INBD OF NR 5 FLAP TRACK. PERFORMED REPAIR IAW SRM 57-53-12, FIG 209. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201310172529](https://openairdocs.org/sdr/FDEA201310172529.md): Lug · corroded · Oct 17, 2013 · N450FE · Airbus A310222 · Wing, Landing Gear Attach Fittings
  > LEFT MLG RIB 5 FWD LUG LOWER SURFACE IS CORRODED. R & R IAW REPAIR DWG R57249389, REV B IAW EA 6-5710-T0302173. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201310152508](https://openairdocs.org/sdr/FDEA201310152508.md): Skin · corroded · Oct 15, 2013 · N450FE · Airbus A310222 · Elevator, Plate/Skin
  > LEFT ELEVATOR LOWER SKIN HAS A SPOT OF CORROSION LOCATION 5 INCHES FROM T/E, 15 INCHES FROM TIP. PERFORMED REPAIR ON LT ELEVATOR SKIN IAW SRM 55-21-11, FIG 209. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201310152509](https://openairdocs.org/sdr/FDEA201310152509.md): Skin · cracked · Oct 15, 2013 · N450FE · Airbus A310222 · Wing, Plate/Skin
  > RT WING, RIB 9 LOWER SKIN FWD EDGE CRACKED. REPAIRED SKIN IAW DWG R572-57208 & EA 6-5710-T0302280. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201310132493](https://openairdocs.org/sdr/FDEA201310132493.md): Stringer · corroded · Oct 13, 2013 · N450FE · Airbus A310222 · Fuselage Main, Longeron/Stringer
  > STRINGER 44R FWD OF FRAME 17 HAS CORROSION AROUND RIVET. REPAIRED STRINGER IAW SRM 53-12-14. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201310132494](https://openairdocs.org/sdr/FDEA201310132494.md): Mount · corroded · Oct 13, 2013 · N450FE · Airbus A310222 · Engine Mount Section
  > TWO FWD ENGINE MOUNTS HAVE PITTING CORROSION IN BOTH FWD MOUNT HOLES AND THE AFT OTBD MOUNT HOLE. PERFORMED REPAIR IAW SRM 54-51-18 WITH FABRICATED BUSHINGS.
- [SDR FDEA201310132492](https://openairdocs.org/sdr/FDEA201310132492.md): Angle · bent · Oct 13, 2013 · N450FE · Airbus A310222 · Fuselage Miscellaneous Structure
  > AFT FUSELAGE THS BAY WEB AT FRAMES 89 & 84 UPPER ANGLE BENT STRINGER 32L. REPLACED WEB UPPER ANGLE IAW SRM 51-40-21. F
- [SDR FDEA201310132491](https://openairdocs.org/sdr/FDEA201310132491.md): Angle · bent · Oct 13, 2013 · N450FE · Airbus A310222 · Fuselage Miscellaneous Structure
  > THS BAY WEB UPPER ANGLE BENT LOCATION, STRINGER 32R, BETWEEN FRAMES 86 & 87. REPLACED WEB UPPER ANGLE IAW SRM 53-19-18.
- [SDR FDEA201310092461](https://openairdocs.org/sdr/FDEA201310092461.md): Mount · corroded · Oct 9, 2013 · N450FE · Airbus A310222 · Engine Mount Section
  > NR 2 PYLON AFT ENGINE MOUNT HAS CORROSION ON FWD & AFT SIDES OF MOUNT, ON INBD AND OTBD, HORIZONTALLY POSITIONED BOLTS, RECESSED AREAS. REPAIRED IAW EA 6-5451-T0302401 PART 1. REPAIR CLASSIFIED AS MINOR.
- [SDR FDEA201310092460](https://openairdocs.org/sdr/FDEA201310092460.md): Skin · dented · Oct 9, 2013 · N450FE · Airbus A310222 · Ailerons
  > RIGHT WING ALL SPEED AILERON BOTTOM SKIN HAS DENT LOCATION 27.5 IN FROM INBD, 17IN FROM FWD END. REPAIRED IAW SRM 57-61-12, PB 201, PARAGRAPH 4.A. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201310082451](https://openairdocs.org/sdr/FDEA201310082451.md): Seat Track · damaged · Oct 8, 2013 · N450FE · Airbus A310222 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK DAMAGED AT FRAME 40-42, -Y1959 REPAIRED IAW SRM 53-10-16, PARA 5, FIG 203, SH 5, FABRICATED & INSTALLED SEAT TRACK IAW SRM 51-27-11 & SRM 51-40-21. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201310062421](https://openairdocs.org/sdr/FDEA201310062421.md): Lug · damaged · Oct 6, 2013 · N453FE · Airbus A310222 · Wing, Attach Fittings
  > LEFT MLG WW RIB 5 FITTING FWD LUG DAMAGED. REPAIRED IAW EA 6-5750-T0302477 P1, REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.
- [SDR FDEA201310042404](https://openairdocs.org/sdr/FDEA201310042404.md): Lug · corroded · Oct 4, 2013 · N453FE · Airbus A310222 · Wing Miscellaneous Structure
  > CORROSION WAS FOUND ON THE LUG BORE AND AFT SPOTFACE OF RT RIB5 FWD LUG. ACCOMPLISHED CORROSION REPAIR IAW GMM 6-2-100 REPAIR CLASSIFIEID AS MINOR.
- [SDR FDEA201310042403](https://openairdocs.org/sdr/FDEA201310042403.md): Lug · corroded · Oct 4, 2013 · N453FE · Airbus A310222 · Wing Miscellaneous Structure
  > CORROSION WAS FOUND ON LUG BORE AND FWD SPOTFACE OF LT RIB 5. ACCOMPLISHED THE CORROSION REPAIR IAW GMM 6-2-100, IAW EA 6-5750-T0302477 P1. REPAIR CLASSIFED AS MINOR.
- [SDR FDEA201310032398](https://openairdocs.org/sdr/FDEA201310032398.md): Web · cracked · Oct 3, 2013 · N450FE · Airbus A310222 · Fuselage Miscellaneous Structure
  > FOUND WEB BETWEEN FRAMES 86 - 87 STRINGER 35R CRACKED. R & R WEB IAW SRM 51-40-21. REPAIR CLASSIFIED AS MINOR.
- [SDR FDEA201309302352](https://openairdocs.org/sdr/FDEA201309302352.md): Skin · damaged · Sep 30, 2013 · N450FE · Airbus A310222 · Fuselage Main, Plate/Skin
  > ACCESS DOOR 136AR EXTERNAL SKIN CUTOUT RADIUS IS OUT OF TOLERANCE. REPLACED ACCESS DOOR 136AR SKIN IAW SRM 52-41-15 & DWG 14A52475000.
- [SDR FDEA201309302338](https://openairdocs.org/sdr/FDEA201309302338.md): Beam · cracked · Sep 30, 2013 · N453FE · Airbus A310222 · Fuselage Miscellaneous Structure
  > THREE CRACKS WERE FOUND AT LT INNER LONGITUDINAL BEAM FLANGE STR 11 BETWEEN FRAMES 73A AND 74A. CUT OUT DAMAGE PORTION OF BEAM AND REWORK MILLED STEP. INSTALL THE REPAIR ANGLE AND FILLER IAW SRM 53-18-18, FIG 205A.
- [SDR FDEA201309292337](https://openairdocs.org/sdr/FDEA201309292337.md): Profile · chafed · Sep 29, 2013 · N450FE · Airbus A310222 · Fuselage Miscellaneous Structure
  > AFT CABIN PROFILE TEE, FRAME 80, STR 34L, WEB CHORD CHAFED. REPLACED DAMAGED PROFILE TEE IAW SRM 51-40-21.
- [SDR FDEA201309262322](https://openairdocs.org/sdr/FDEA201309262322.md): Tee Fitting · chafed · Sep 26, 2013 · N450FE · Airbus A310222 · Fuselage Miscellaneous Structure
  > AFT CABIN FRAME 80, S34R WEB ANGLE CHAFED REPLACED DAMAGED PROFILE TEE WITH FABRICATED PROFILE TEE AT FRAME 80, STR 34R IAW SRM 51-40-21. PROFILE FABRICATED IAW SRM 53-18-18.
- [SDR FDEA201309252309](https://openairdocs.org/sdr/FDEA201309252309.md): Floorboard · delaminated · Sep 25, 2013 · N450FE · Airbus A310222 · Fuselage Floor Panel
  > FWD MAIN DECK CARGO UTILITY AREA LAVATORY FLOORBOARD, MULTIPLE AREAS HAS DAMAGED AND DELAMINATION. FABRICATED FLOORBOARD IAW SRZ-25-005. AND INSTALLED. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201309252308](https://openairdocs.org/sdr/FDEA201309252308.md): Floorboard · damaged · Sep 25, 2013 · N450FE · Airbus A310222 · Fuselage Floor Panel
  > FWD CABIN FLOORBOARD 222DF EDGE HAS HONEYCOMB CHIPPED OFF, FABRICATED FLOORBOARD IAW SRZ-25-005 AND INSTALLED. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201309232287](https://openairdocs.org/sdr/FDEA201309232287.md): Skin · dented · Sep 23, 2013 · N450FE · Airbus A310222 · Fuselage Main, Plate/Skin
  > LOWER FUSELAGE SKIN, FRAME 19- 20, STR 34 -35R DENTED. REPAIRED IAW SRM 53-10-12 FIG 226 (SHEET 2). REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201309232292](https://openairdocs.org/sdr/FDEA201309232292.md): Floor Panel · cracked · Sep 23, 2013 · N450FE · Airbus A310222 · Fuselage Floor Panel
  > MAIN DECK CARGO FRAMES 60-62, BETWEEN Y953 AND Y1456 FLOOR PANEL 251UF CRACKED. REPLACED PANEL. PANEL FABRICATED IAW DWG SRZ-25-005.
- [SDR FDEA201309232289](https://openairdocs.org/sdr/FDEA201309232289.md): Floorboard · cracked · Sep 23, 2013 · N450FE · Airbus A310222 · Fuselage Floor Panel
  > FLOORBOARD 231BG HAS A CRACK. REPLACED FLOORBOARD. FLOORBOARD FABRICATED ON TRAVELER T13/1025840 IAW DWG SRZ-25-005 & INSTALLED ON WC 230-SWC-FIT.
- [SDR FDEA201309232288](https://openairdocs.org/sdr/FDEA201309232288.md): Floorboard · damaged · Sep 23, 2013 · N450FE · Airbus A310222 · Fuselage Floor Panel
  > FLOORBOARD 231ZF HAS DAMAGE IN SEVERAL AREAS. FABRICATED & REPLACED FLOORBOARD.
- [SDR FDEA201309232286](https://openairdocs.org/sdr/FDEA201309232286.md): Skin · damaged · Sep 23, 2013 · N450FE · Airbus A310222 · Fuselage Main, Plate/Skin
  > DURING ACCOMPLISHMENT OF STRINGER REPAIR AT FR 72 2 EA HOLES HAVE EXCESSIVE PITCH AT STRINGER 41R. ACCOMPLISHED CATEGORY B SKIN REPAIR AT FR 72 STR 41R IAW SRM 53-10-12, FIG 225SH. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201309232283](https://openairdocs.org/sdr/FDEA201309232283.md): Floor Panel · damaged · Sep 23, 2013 · N453FE · Airbus A310222 · Fuselage Floor Panel
  > FLOOR PANEL 132RF IN LOWER FWD CARGO BAY WAS FOUND SOFT. FABRICATED A NEW PANEL WITH INSERTS AND ADHESIVE IAW SRM 53-10-20 & IRM 9701. REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
- [SDR FDEA201309232282](https://openairdocs.org/sdr/FDEA201309232282.md): Floor Panel · dented · Sep 23, 2013 · N453FE · Airbus A310222 · Fuselage Floor Panel
  > FLOOR PANEL 162HF IN BULK CARGO, FOUND SERIOUS DENT IN SKIN. FABRICATED A NEW PANEL WITH INSERTS AND ADHESIVE IAW SRM 53-10-20 & IRM 9701. REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Next page: https://openairdocs.org/model/airbus-industrie-a310-222/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 = 'A310222'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/airbus-industrie-a310-222/reports

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