Airbus A320-211
Service difficulty reports · 5,271
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Query with SQL
duckdb -csv -c "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 = 'A320211' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
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 = 'A320211' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR DALA13005353214Floor Panel · damagedDURING INSPECTION, FOUND FWD CABIN FLOOR PANEL 221PF DAMAGED/DELAMINATED. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209 & DWG 3D25-37498.SDR DALA13005343214Floor Panel · damagedDURING INSPECTION, FOUND AFT CABIN FLOOR PANEL 261PF DAMAGED & DELAMINATED. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209 & DWG 3D25-37498.SDR DALA13005333214Floor Panel · damagedDURING INSPECTION, FOUND AFT CABIN FLOOR PANEL 262EF DAMAGED & DELAMINATED. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209 & DWG 3D25-37498.SDR DALA13005323214Floor Panel · damagedDURING INSPECTION, FOUND AFT CABIN FLOOR PANEL 262AB DAMAGED & DELAMINATED. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209 & DWG 3D25-37498.SDR DALA13005103214Floor Panel · damagedDURING INSPECTION, FOUND AFT CABIN FLOOR PANEL 261DF DAMAGED/DELAMINATED. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209 & DWG 3D25-37498.SDR DALA13005093214Shackle · gougedDURING INSPECTION, FOUND NR 2 ENG PYLON AFT SHACKLE 1EA SIDE HAS GOUGED MARK AROUND THE BUSHING HOLE. BLENDED DAMAGE IAW SRM 51-73-00, CHECKED LIMIT DIMENSION DEPTH=.010" MAX ALLOW .006". FOUND TO BE OUT OF LIMIT IAW ER/A 507720-14MA. RECEIVED NEW SHACKLESDR DALA13005373213Floor Panel · damagedDURING INSPECTION, FOUND AFT UTILITY FLOOR PANEL 261EF INSERTS DAMAGED. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209. INSTALLED ON WC 2500-6602.SDR DALA13005083214Floor Panel · delaminatedDURING INSPECTION, FOUND MAIN CABIN FLOOR PANEL 231BF DELAMINATED 4.0" X 6.0". FABRICATED NEW FLOOR PANEL 231BF ON STAM TRAVELER NR T13/981225 IAW SRM 53-02-00, FIG 209. DAMAGE DIMENSION LENGHT=6" WIDTH 4" & DWG NR 3D25-37498.SDR DALA13005073214Floor Panel · delaminatedDURING INSPECTION, FOUND FWD CABIN FLOOR PANEL 221EF DELAMINATED 4" X 6". FABRICATED NEW FLOOR PANEL 221EF ON STAM TRAVELER NR T13/981226 IAW SRM 53-02-00, FIG 209. DAMAGE DIMENSION LENGTH=6", WIDTH 4" & DWG NR 3D25-37498.SDR DALA13005053213Floor Support · damagedDURING INSPECTION, FOUND FORWARD CABIN UTILITY AREA FLOORBEAM BETWEEN FR 16-20 Y-254 UPPER FLANGE HOLES HAS CORROSION. REMOVED DAMAGE IAW SRM 51-74-00. DAMAGE MEASURES: AREA NR 1 L=1.8 W=1.2 D=.010, AREA NR 2 L=1.1 W=1.0 D=.015 NO LIMITS FOUND IN SRM. REPAISDR DALA13005593231Light · missingDURING NON ROUTINE CHECK SEAT 18C ESCAPE PATH LIGHT ASSY MISSING. INSTALLED REPAIRED EMERGENCY LIGHT AT SEAT 18C AND FUNCTIONAL IS NORMAL.SDR DALA13005043214Floor Support · crackedDURING INSPECTION, FOUND COCKPIT AREA AT FR11 FLOOR SUPPORT WEB CRACKED AT -Y765. CHECK LIMITS ON CRACK LENGTH .57" AND OUT OF LIMITS. REMOVED FLOOR WEB SUPPORT, DRILLED AND INSTALLED NEW FLOOR WEB SUPPORT IAW SRM 53-11-14,51-42-11 AND 51-44-11 AT FR11 +Y765.SDR DALA13004933214Floor Support · crackedDURING INSPECTION, FOUND COCKPIT AREA AT FR11+Y765, FLOOR SUPPORT WEB CRACKED. CHECK LIMITS ON CRACK AND LENGTH .815" IS OUT OF LIMITS. REMOVED FLOOR WEB SUPPORT, LOCATED, DRILLED AND INSTALLED NEW SUPPORT WEB AT FR1 1 +Y765 IAW SRM 53-11-14, 51-42-11 AND 51-SDR DALA13004443214Floorboard · delaminatedDURING INSPECTION, FOUND AFT CABIN FLOORBOARD 252GF DELAMINATED ON UNDERSIDE AROUND FASTENER HOLE. FABRICATED NEW FLOORBOARD IAW SRM 53-02-00, FIG. 209.SDR CA130128017Servo · leaking(CAN) ACFT HAD WARNING LIGHT ON GREEN HYD SYSTEM FLUCTUATING IN AND OUT OF AMBER. EMERGENCY SERVICES WERE ON STAND BY FOR FLIGHT ARRIVAL. ACFT LANDED WITH NO FURTHER ISSUE AND TAXIED ON ITS OWN POWER TO THE GATE. REPLACED G SYS LT YAW DAMPER SERVO IAW AMM 27SDR DALA13005023214Floor Support · corrodedDURING INSPECTION, FOUND AFT UTILITY FLOOR SUPPORT -Y1292 BETWEEN FR 68 AND FR 70 HAS CORROSION ON BEAM AROUND FASTENERS HOLES AND UPPER FLANGE ABOVE SPL ICE. REMOVED CORROSION IAW SRM 51-74-00. CHECK LIMIT L=4.0"W=2.5" D=0.030"FOUND OUT OF LIMIT IAW A320 53SDR DALA13005013214Floor Support · corrodedDURING INSPECTION, FOUND AFT UTILITY FLOOR SUPPORT -Y1292 BETWEEN FR 66 AND FR 68 HAS CORROSION AROUND FASTENERS AND HOLES AT FR 68 SPLICE. REMOVED CORROSION IAW SRM 51-74-00. CHECK LIMIT L=3.0"W=2.0" D=0.030" FOUND OUT OF LIMIT IAW 53-00-14, FIG 102. REPLSDR DALA13004973214Spar · corrodedDURING INSPECTION, FOUND NR 2 ENG PYLON UPPER SPAR, SPIGOT FITTING BORE PITTED. MAX DIA OF SPIGOT FITTING IS 4.335", AFTER REWORK DIA IS 4.337 " FOUND TO BE OUT OF LIMITS IAW SRM 54-51-12, FIG 101, SH. 2. REPLACED SPIGOT FITTING IAW SRM 54-51-41-400-001- A.SDR DALA13004963214Hinge · damagedDURING INSPECTION, FOUND RT AILERON, HINGE BOLT NR 3, SCORED. SCORED BEYOND LIMITS IAW AMM 27-14-41, PB 601. RECEIVED NEW BOLT TO BE INSTALLED ON JIC 5760-1010S-RT. DIMENSIONS: L=.8750"X W=.7500".SDR DALA13004953214Bolt · scoredDURING INSPECTION, FOUND RT AILERON, HINGE BOLT NR 2 SCORED. SCORED IS BEYOND LIMITS IAW AMM 27-14-41 PB 601. RECEIVED NEW BOLT TO BE INSTALLED ON JIC 5760-1010S-RT. DIMENSIONS L=.8750" X W=.7500".SDR DALA13004473215Battery Pack · inoperativeDURING NON-ROUTINE CHECK, FOUND BATTERY FAULT FOR EPSU 13WL CHECK. MX REPLACED EPSU 13WL BATTERY PACK WITH SERVICEABLE UNIT AND FUNCTIONAL CHECK WAS NORMAL.SDR DALA13005063213Skin · gougedDURING INSPECTION, FOUND LOWER FUSELAGE JUST AFT OF FR 65 BETWEEN STR 28L - 29L SKIN APPEARS TO BE GOUGED UNDER PAINT. N/R 100/4. CUTOUT DAMAGED SKIN IAW SRM 53-41-11. DIM. L=1.78" W=1.75". FABRICATED DOUBLER FROM 2024T30.071 IAW SRM 53-41-11, FIG 214. INSSDR DALA13004943214Door Frame · corrodedDURING INSPECTION, FOUND RT AFT DOOR CUT OUT FR 68 FWD FACE HAS CORROSION APPROX 1" ABOVE DOOR SILL. REMOVED CORROSION IAW SRM 51-74-00, CHECKED LIMITS, L=1.5"X W =1"X D=.021" FOUND OUT OF LIMITS IAW SRM 53-41-12. REPAIRED IAW SRM 53-41-12, FIG 201. PRINCIPLESDR DALA13004413214Bolt · scoredDURING INSPECTION, FOUND RT AILERON, HINGE BOLT NR 4, SCORED. SCORED IS BEYOND LIMITS IAW AMM 27-14-41, PB 601. RECEIVED NEW BOLT TO BE INSTALLED ON JIC 5760-1010S-RT. DIMENSIONS L=.8750" X W=.7500".SDR DALA13004403214Bolt · scoredDURING INSPECTION, FOUND RT AILERON, HINGE BOLT NR 1 SCORED. SCORED IS BEYOND LIMITS IAW AMM 27-14-41, PB 601. RECEIVED NEW BOLT TO BE INSTALLED ON JIC 5760-1010S-RT. DIMENSION L=.8750"X W=.7500".SDR DALA13004233213Sill · corrodedDURING INSPECTION, FOUND RT AFT PASSENGER ENTRANCE LOWER DOOR SILL AT FWD FR68 GIRT BAR & INBD HOLES HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. BLENDED AREA MEASURES L=1.5" W= 1.0" D=.110" AND FOUND TO BE OUT OF LIMITS IAW SRM 53-41-14, FIG 101. REMOVSDR DALA13004223214Tray · crackedDURING INSPECTION, FOUND AFT UTILITY RT SIDE TRAY AT S23R AFT OF FR68 IS CRACKED. REPLACED RT SIDE TRAY AT STR 23R AFT OF FR68 IAW SRM 51-42-11, NEW SIDE TRAY FABRICATED FROM 2024T3.063 BATCH 0002344339 IAW SRM 53-41-14.SDR DALA13004213214Tray · crackedDURING INSPECTION, FOUND AFT UTILITY RT SIDE TRAY AT S23R AFT OF FR 68 IS CRACKED. REPLACED RT SIDE TRAY AT STR 23R AFT OF FR68 IAW SRM 51-42-11, NEW SIDE TRAY FABRICATED FROM 2024T3.063 BATCH 0002344339 IAW SRM 53-41-14.SDR DALA13004203213Fitting · corrodedDURING INSPECTION, FOUND NR 1 ENGINE SPIGOT RECEPTACLE FITTING BORE AT UPPER SPAR HAS FITTING CORROSION. REMOVED CORROSION IAW SRM 51-74-00 FINAL DIAMETER FOUND TO BE OUT OF LIMITS OF 4.345 ALLOWABLE DIA 4.335 IAW SRM 54-51- 12, FIG 101. REMOVED FITTING IAW SDR DALA13004393214Sill · corrodedDURING INSPECTION, FOUND RT AFT DOOR CUTOUT FR66 AFT FACE APPROX 1" ABOVE DOOR SILL HAS CORROSION. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-41-12. REPAIR IAW SRM 53-41-12, FIG 201, REPAIR PART FAB ON TRAVELER T13/979196 IAW SRM 51-41-12. REQUIRESSDR DALA13003753213Floor Panel · corrodedDURING INSPECTION, FOUND AFT UTILITY FLOOR PANEL 261FF HAS CORROSION 4" X 6". REPLACED FLOOR PANEL IAW SRM 51-72-00.SDR DALA13003743213Floor Panel · gougedDURING INSPECTION, FOUND MAIN CABIN FWD AREA FLOOR PANEL 231CF HAS GOUGE 3" X 2". FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209.SDR DALA13003733213Floorboard · damagedDURING INSPECTION, FOUND MAIN CABIN, FWD AREA FLOORBOARD 232DF HAS A HOLE .300" X .500". FABRICATED FLOORBOARD IAW SRM 53-02-00, FIG 209.SDR DALA13003723214Floor Support · corrodedDURING INSPECTION, FOUND AFT UTILITY FLOOR SUPPORT -Y1732 HAS CORROSION AT FASTENER HOLE SEVEN INCHES FWD OF FR66. REPLACED FLOOR SUPPORT IAW SRM 51-42-11, TOP COAT PAINTED FASTENERS IAW SRM 51-75-12. REMOVED CORROSION IAW SRM 51-74-00 FOUND TO BE OUT OF LIMSDR DALA13003713214Floor Support · corrodedDURING INSPECTION, FOUND AFT UTILITY FLOOR SUPPORT Y1292 FWD OF FR68 BETWEEN FR66 AND FR68 HAS CORROSION AROUND AND UNDER FASTENERS AT SPLICES. BLENDED CORROSION IAW SRM 53-00-14 FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15. REPLACED FLOOR SUPPORT IAW SRM 51-4SDR DALA13003623213Web · corrodedDURING INSPECTION, FOUND FORWARD CABIN RT SIDE STRINGER 23 BETWEEN FR 20 TO 21 UPPER SURFACE WEB CORRODED. REMOVED CORROSION IAW SRM 51-74-00. REPLACED WEB IAW SRM 51-42-11.SDR DALA13003613214Floor Panel · corrodedDURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 152KF CORRODED. REPLACED FLOOR PANEL IAW SRM 51-72-11.SDR DALA13003583226Wire · damagedDURING NON ROUTINE CHECK, FOUND AISLE EMERGENCY LIGHT INOPERATIVE AT ROW 14. INSPECTED AND FOUND WIRES PULLED OUT OF CONNECTOR. INSTALLED NEW PINS AND CONNECTOR. OPS CHECK WERE NORMAL.SDR CA130121002Slat System · failed(CAN) SLAT FAILURE ON APPROACH, REQUESTED RADAR VECTORS FROM ATC TO PERFORM QRH PROCEDURE, THEN DECLARED EMERGENCY WITH ATC. DUTY PILOT/FLIGHT SAFETY ADVISED. TROUBLESHOOTING DONE IAW TSM 27-81-00-810-810-A, NO FAULT FOUND. SLAT ROTARY ACTUATORS TORQUE LIMITSDR DALA13003563213Floor Panel · puncturedDURING INSPECTION, FOUND MAIN CABIN CENTER WING AREA FLOOR PANEL 241LF HAS PUNCTURE. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.SDR DALA13003553213Floor Panel · dentedDURING INSPECTION, FOUND MAIN CABIN CENTER WING AREA FLOOR PANEL 241DF HAS INDENTION ON BOTTOM. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.SDR DALA13003543213Floorboard · damagedDURING INSPECTION, FOUND MAIN CABIN CENTER WING AREA FLOORBOARD 241JF IS DAMAGED AND MISSING INSERT. FABRICATED NEW FLOORBOARD IAW SRM 53-02-00, FIG 209.SDR DALA13003533213Floor Panel · damagedDURING INSPECTION, FOUND FWD CARGO FLOOR PANEL 131EF HAS EDGE DAMAGE. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.SDR DALA13003523213Floor Panel · damagedDURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 161AF HAS CORNER DAMAGE & EROSION AROUND TOP CUTOUTS. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.SDR DALA13003513213Floor Panel · damagedDURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 161DF HAS DAMAGE AT TOP CUTOUT. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.SDR DALA13003503213Panel · damagedDURING INSPECTION, FOUND FWD CARGO SLOPING WALL PANEL 131BF HAS EDGE DAMAGE. FABRICATED NEW SLOPE WALL PANEL IAW SRM 53-02-00, FIG 209.SDR DALA13003493213Panel · damagedDURING INSPECTION, FOUND FWD CARGO SLOPING WALL PANEL 131FF HAS EDGE DAMAGE. FABRICATED NEW SLOPE WALL PANEL IAW SRM 53-02-00, FIG 209.SDR DALA13003483213Panel · damagedDURING INSPECTION, FOUND FWD CARGO SLOPING WALL PANEL 131KF HAS EDGE DAMAGE. FABRICATED NEW SLOPE PANEL IAW SRM 53-02-00, FIG 209.SDR DALA13003473213Panel · puncturedDURING INSPECTION, FOUND FWD CARGO SLOPING WALL PANEL 131GF IS PUNCTURED. FABRICATED NEW SLOPE WALL PANEL IAW SRM 53-02-00, FIG 209.SDR DALA13003463213Panel · erodedDURING INSPECTION, FOUND AFT CARGO SLOPING WALL PANEL 152EF HAS EDGE EROSION AROUND TOP CUT OUT (9" X 4"). FABRICATED NEW SLOPE PANE IAW SRM 53-02-00, FIG 209.
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