Airbus A320-211
Service difficulty reports · 5,271
Newest first. General aviation reporting is voluntary.
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 DALA12016233210Attach Fitting · chafedDURING INSPECTION, FOUND CHAFED MARK ON LT AFT PAX DOOR ASSIST CYLINDER ATTACHMENT FITTING. BLENDED OUT DAMAGE IAW SRM 51-73-00. DIM OF REWORK L=.4", W=.2", D=.008", NO ALLOWABLE LIMITS PROVIDED. HFEC ACCOMPLISHED IAW NTM 51-10-08, NO CRACKS OR OTHER DISCRESDR DALA12016223210Plate · damagedDURING INSPECTION, FOUND LT WING SLAT TRACK NR 6, CLOSING PLATE CHAFING WITH SLAT LOWER T/E. BLENDED OUT CHAFE DAMAGE IAW SRM 51-73-00. DIM OF REWORK L=3.2", W=.25", D=.012". FOUND OUT OF LIMITS IAW SRM 57-40-00, FIG 106. ACCOMPLISHED DVI IAW NTM 51-90-00SDR DALA12016283210Rib · corrodedDURING INSPECTION, FOUND LT OTBD FLAP, INBD RIB L/E HAS 2 AREAS OF PITTING AFTER RUB STRIP REMOVAL. BLENDED CORROSION IAW SRM 51-74-00, AREA L 1 =1.5" W=1.0 "D =0.028"AREA 55"W=0.070" D=0.030". ACCOMPLISHED ER/A 508976-14 REV ORIGINAL SECTION I PERMANENT REPSDR DALA12016273227Wire Harness · brokenDURING INSPECTION, FOUND FLOOR/AISLE EMERGENCY ESCAPE PATH LIGHT AT 14C INOPERATIVE. INSPECT WIRE HARNESS FOR DAMAGE FLAT SPOTS CRIMPS OR SHARP BENDS, CHECK BULB AND REPLACE, MAY NEED 32-3300-3-0586. FOUND BROKEN WIRE ALONG WIRE HARNESS. TERMINATED NEW QUICSDR DALA12016263227Epsu · inoperativeEMERGENCY EXIT SIGNS DID NOT ILLUMINATE WHEN GEAR DOWN ON LANDING. MX REPLACED EPSU AND BATTERY AT 2L DOOR AND FUNCTIONAL CHECKED NORMAL.SDR DALA12016013210Panel · crackedDURING INSPECTION, FOUND AFT CARGO SLOPE PANEL 151CF CRACKED 6.0 INCHES LONG. SLOPE PANEL FABRICATED IAW SRM 53-02-00, FIG 209 L=6.0, W=.100 OUT OF LIMITS IAW 53-02-00.SDR DALA12016003210Panel · puncturedDURING INSPECTION, FOUND AFT CARGO SLOPE PANEL 162EF MULTIPLE PUNCTURES. SLOPE PANEL FABRICATED IAW FIG 209, DIAMETER OF PUNCTURE .350 AREA (1) .400 AREA (2) FOUND OUT OF LIMITS IAW SRM 53-02-00.SDR DALA12015993210Panel · damagedDURING INSPECTION, FOUND AFT CARGO SLOPE PANEL 151HF HAS EDGE DAMAGE BEYOND ALLOWABLE LIMITS. SLOPE PANEL FABRICATED IAW 53-02-00. DAMAGE LOCATED AT EDGE OF CUTOUT 2.00" LONG W=2.0 OUT OF LIMITS IAW SRM 53-02-00.SDR DALA12015983210Floor Panel · damagedDURING INSPECTION, FOUND FLOOR PANEL 241AF IS SOFT AND SPONGY. REMOVED CABIN FLOOR PANEL IAW MM 53-12-12-000-001-A. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209 & INSTALLED IAW AMM 53-12-12000-001-A.SDR DALA12015913210Floor Support · corrodedDURING INSPECTION, FOUND AFT CARGO BAY AT FRAME 58, STR 44 BEAM HAS CORROSION. REMOVED CORROSION IAW 51-74-00. AREA MEASURES L=1.0"X W=.80"X D=.012" ORG MAT .079, NO LIMITS FOUND IN SRM. R & R BEAM AT STR 44 BETWEEN FR 58 AND 59 IAW SRM 51-42-11.SDR DALA12015973210Attach Bracket · corrodedDURING INSPECTION, FOUND AFT CARGO COMPT FRAME 58, STR 36-38L, SEAL PLATE ATTACHMENT BRACKET HAS CORROSION. FOUND AFTER SEAL PLATE REMOVAL. REMOVED CORROSION IAW SRM 51-74-00 L=.600, W=.250, D=.100. ORIG MAT .120 NO LIMITS FOUND IAW SRM. REMOVED FITTING IASDR DALA12016293210Carriage · gougedDURING INSPECTION, FOUND RT WING NR 1 FLAP TRACK, FLAP CARRIAGE FWD LOWER TRACK HAS GOUGE (2 EA). ACCOMPLISHED RT WING NR 1 FLAP TRACK, FLAP CARRIAGE FWD LWR TRACK REPAIR BY BLENDING AREA IAW SRM 51-73-00, OTBD L=1.400"W=.250"D =.003", INBD L=1.400"W=.250"D=SDR DALA12015923278Wire · brokenDURING NON ROUTINE CHECK, FOUND ROW 24 EMERGENCY ESCAPE PATH LIGHT INOPERATIVE. FOUND BROKEN WIRE AT CONNECTOR, MX INSTALLED NEW SPLICE AND FUNCTIONAL CHECK WAS NORMAL.SDR DALA12015713210Floor Panel · corrodedDURING INSPECTION, FOUND FWD UTILITY FLOOR PANEL 221FF CORRODED ON LWR SURFACE 3.5" X 2.0". REPLACED FLOOR PANEL IAW SRM 51-72-00.SDR DALA12015503210Web · corrodedDURING INSPECTION, FOUND FORWARD CABIN RT SIDE AT FR 16 STRINGER 23 UPPER SURFACE WEB HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. CHECKED LIMITS L=1", W=1.3", D=.062. NO ESTABLISH LIMITS IN SRM. R & R WEB IAW SRM 51-42-11. PAINTED FASTENERS IAW SRMSDR DALA12015493210Skin · damagedDURING INSPECTION, FOUND RT SIDE LOWER AFT FUSELAGE FR 69,S28-29R EXTERNAL SKIN SURFACE HAS PRE-EXISTING TOOL MARK (APPEARS TO BE FROM FASTENER REPLACEMENT). REMOVED TOOL MARKS IAW SRM 51-73-00. CHECKED DAMAGE L=.8", W=.7", D=.012". FOUND TO BE OUT OF LIMITS ISDR DALA12015433210Floor Panel · crackedDURING INSPECTION, FOUND FWD UTILITY FLOOR PANEL 221EF CRACKED 4.0" X 1.0". AND FWD UTILITY PANEL 221EF. REPLACED IAW SRM 51-72-00.SDR DALA12015703210Skin · damagedDURING INSPECTION, FOUND LOWER FUSELAGE HAS LIGHTNING STRIKE ON THIRD FASTENER ON STRINGER 42R FWD OF FR 31. REMOVED FASTENER & REAMED HOLE IAW SRM 53-21-11, FIG 213. COLD WORK FASTENER HOLE IAW SRM 51-48-00. INSTALLED FASTENER IAW SRM 51-42-11. PERFORMED SSDR DALA12015483210Hinge Pin · corrodedDURING INSPECTION, FOUND LT WING SPOILER NR 4 CENTER HINGE INBD PIN CORRODED. RECEIVED NEW CTR PIN TO BE INSTALLED ON JIC 5770-1010S-LT.SDR DALA12015033210Hinge Pin · corrodedDURING INSPECTION, FOUND RT WING NR 5 SPOILER BOTH INBD AND OTBD CTR HINGE PIN HAS CORROSION AND THREAD DAMAGED. RECEIVED NEW CTR PINS INSTALLED ON JIC 5770-1010S-RT.SDR DALA12015023210Hinge Pin · corrodedDURING INSPECTION, FOUND LT WING SPOILER NR 5 CENTER HINGE INBD PIN CORROD PIN INSTALLED ON JIC 5770-1010S-LT.SDR DALA12015013210Floor Panel · corrodedDURING INSPECTION, FOUND AFT UTILITY FLOOR PANEL 262FF CORRODED 3.0" X 3.0". REPLACED FLOOR PANEL IAW SRM 51-72-00.SDR DALA12015003210Threshold · corrodedDURING INSPECTION, FOUND AFT CARGO THRESHOLD PANEL 152KF CORRODED.3.5 X 3.5. REPLACED AFT CARGO THRESHOLD PANEL IAW SRM 51-72-00.SDR DALA12014993210Floor Panel · corrodedDURING INSPECTION, FOUND AFT UTILITY FLOOR PANEL 262EF WITH MULTIPLE CORRODED INSERTS. FABRICATED FLOOR PANEL IAW DWG 3D25-37498.SDR DALA12014983210Floor Panel · puncturedDURING INSPECTION, FOUND AFT UTILITY FLOOR PANEL PUNCTURED 261DF 4.0" X 4.0". FABRICATED FLOOR PANEL IAW DWG.SDR DALA12014973210Floor Panel · puncturedDURING INSPECTION, FOUND FWD UTILITY FLOOR PANEL 222CF PUNCTURED "2.5 X 3.0". FABRICATED FLOOR PANEL IAW DWG 3D25-37498.SDR DALA12014963210Floor Panel · crackedDURING INSPECTION, FOUND MAIN CABIN FLOOR PANEL 231YF CRACKED 7.0" LONG. FABRICATED FLOOR PANEL IAW DWG 3D25-37498.SDR DALA12014943210Floor Panel · corrodedDURING INSPECTION, FOUND AFT UTILITY FLOOR PANEL 261EF WITH CORRODED INSERTS. FABRICATED FLOOR PANEL IAW DWG 3D25-37498.SDR DALA12014773210Floor Support · crackedDURING NON ROUTINE CHECK, FOUND COCKPIT FLOOR SUPPORT BETWEEN FR 8-11 Y-765 WEB CRACKED. REMOVED WEB FROM FR8 TO FR11 Y-765 IAW SRM 51-42-11. RECEIVED NEW WEB PN D5311332220102 BATCH 2364974 AND INSTALLED NEW WEB FROM FR8 TO FR11 IAW SRM 51-42-11.SDR DALA12014763210Floor Panel · puncturedDURING NON ROUTINE CHECK, FOUND AFT UTILITY FLOOR PANEL 262AB PUNCTURED 2.0" X 2.0". FABRICATED FLOOR PANEL IAW DWG.SDR DALA12014783225Battery Pack · failedDURING SERVICE CHECK, EMERGENCY LIGHT TEST FAILED BATTERY LT AFT. MX REPLACED BATTERY PACK AND FUNCTIONAL CHECK WAS NORMAL.SDR DALA12014453209Power Supply · inoperativeDURING NON ROUTINE CHECK, FOUND EMERGENCY PATH LIGHT AT ROWS 13, 14, 15, 18, 19, 20, 23, 24, 25 INOPERATIVE. REPLACED AFT LT EPSU AND FUNCTIONAL CHECK WAS NORMAL.SDR DALA12014443220Connector · missingDURING NON ROUTINE CHECK, FOUND EMERGENCY LIGHT AT 23 ABC INOPERATIVE. MX REPLACED WIRE END CONNECTOR THAT WAS PULLED OFF AND FUNCTIONAL CHECK WAS NORMAL.SDR DALA12014433210Panel · damagedDURING NON ROUTINE CHECK, FOUND AFT CARGO SLOPE PANEL 151BF DAMAGED 4.0" X 4.0". FABRICATED SLOPE PANEL 151BF ON STAM TRAVELER T12/971271 IAW DWG 3D25-37705.SDR DALA12014423210Panel · damagedDURING NON ROUTINE CHECK, FOUND AFT CARGO SLOPE PANEL 152BF DAMAGED 6.5" X 6.5". FABRICATED SLOPE PANEL 152BF ON STAM TRAVELER T12/971269 IAW DWG 3D25-37705.SDR DALA12014413210Panel · damagedDURING NON ROUTINE CHECK, FOUND AFT CARGO SLOPE PANEL 152CF DAMAGED 4.0" X 5.0". FABRICATED SLOPE PANEL 152CF ON STAM TRAVELER T12/971268 IAW DWG 3D25-37705.SDR DALA12014403210Panel · damagedDURING NON ROUTINE CHECK, FOUND AFT CARGO SLOPE PANEL 152EF DAMAGED 3.0" X 3.0". FABRICATED SLOPE PANEL 152EF ON STAM TRAVELER T12/971263 IAW DWG 3D25-37705.SDR DALA12014393210Panel · damagedDURING NON ROUTINE CHECK, FOUND AFT CARGO SLOPE PANEL 152FF DAMAGED 5.0" X 5.0". FABRICATED SLOPE PANEL 152FF ON STAM TRAVELER T12/971261 IAW DWG 3D25-37705.SDR DALA12014383210Panel · delaminatedDURING NON ROUTINE CHECK, FOUND AFT CARGO SLOPE PANEL 161BF DELAMINATED AT EDGE 4.0" X 4.0". FABRICATED SLOPE PANEL 161BF ON STAM TRAVELER T12/971278 IAW DWG 3D25-37705.SDR DALA12014373210Panel · damagedDURING NON ROUNTINE CHECK, FOUND AFT CARGO SLOPE PANEL 161CF DAMAGED 4.5" X 5.0". FABRICATED SLOPE PANEL 161CF ON STAM TRAVELER T12/971277 IAW DWG 3D25-37705.SDR DALA12014363210Panel · damagedDURING NON ROUTINE CHECK, FOUND AFT CARGO SLOPE PANEL 151QF DAMAGED 5.0" X 5.0". FABRICATED SLOPE PANEL 151QF ON STAM TRAVELER NR T12/971276 IAW DWG 3D25-37705.SDR DALA12014353210Panel · delaminatedDURING NON ROUTINE CHECK, FOUND AFT CARGO SLOPE PANEL 151RF DELAMINATED 3.5" X 4.0". FABRICATED SLOPE PANEL 151RF ON STAM TRAVELER NR T12/971275 IAW DWG 3D25-37705 (A320).SDR DALA12014343210Panel · damagedDURING NON ROUTINE CHECK, FOUND AFT CARGO SLOPE PANEL 151EF DAMAGED AREA 4.0" X 4.0". FABRICATED SLOPE PANEL 151EF ON STAM TRAVELER NR T12/971273 IAW DWG NR 3D25-37705.SDR DALA12014333210Panel · damagedDURING NON ROUTINE CHECK, FOUND AFT CARGO SLOPE PANEL 151FF DAMAGED 6.0" X 6.0". FABRICATED SLOPE PANEL 151FF ON STAM TRAVELER NR T12/971272 IAW DWG NR 3D25-37705.SDR DALA12014323210Panel · damagedDURING NON ROUTINE CHECK, FOUND FWD CARGO SLOPE PANEL 131CF DAMAGED 4.5" X 4.5". FABRICATED SLOPE PANEL 131CF ON STAM TRAVELER T12/971010 IAW DWG 3D25-37705 A320).SDR CA121203002Computer · failed(CAN) REJECTED TAKEOFF APPROXIMATELY 100 KTS ACCOUNT, NO V-SPEEDS. FLIGHT OPS/FLIGHT SAFETY ADVISED. FMGC 1 REPLACED AND TESTED, OK IAW AMM 22-83-34 PB401. LAND TEST PERFORMED SUCCESSFULLY. OK FOR CAT 3 APPROACHES. OBSERVED FMA DATA DISPLAYED NORMALLY DURSDR DALA12015683210Skin · dentedDURING INSPECTION, FOUND LOWER FUSELAGE AT STR 31L BET FR 20 AND 21 DENTED .018" DEEP .437" WIDE OUT OF EDGE LIMITS IAW SRM 53-00-11, PG 101-LP 2472695. DENT FOUND OUT LIMITS IAW SRM 53-11-11. CUTOUT DAMAGE L=1.90 0"W=1.0"& FABRICATED DOUBLER AND REPAIR PARTSDR DALA12014313210Floor Support · corrodedDURING NON ROUTINE CHECK, FOUND FORWARD CABIN FLOORBEAM BETWEEN FR 18 TO FR 20 Y-254 UPPER FLANGE HAS CORROSION. BLENDED AREA ON FLOOR SUPPORT Y-254 IAW SRM 51-74-00, ORIG MATERIAL 155"L=.36"W=1"D=.030". NO ALLOWABLE DAMAGE WAS FOUND IN SRM. REPLACED FLOORBSDR DALA12015473210Floor Panel · damagedDURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 151AF EDGE DAMAGE 4.0" X 4.0" NR. 150/52. FABRICATED FLOOR PANEL IAW DWG 3D25-37705.SDR DALA12015353210Floor Panel · damagedDURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 151DF DAMAGED 7.0" X 7.0". FABRICATED FLOOR PANEL IAW DWG 3D25-37705.
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