Airbus A320-211

Service difficulty reports · 5,271

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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.

SDR DALA13006653213Floor Panel · corrodedDURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 152KF IS CORRODED. REMOVED CORROSION IAW SRM 51-74-00, L=1.0" W=0.70" D=0.050 NO ESTABLISHED SRM LIMITS.Feb 7, 2013 · N313US · Airbus A320211 · Fuselage Floor PanelSDR DALA13006643213Web · corrodedDURING INSPECTION, FOUND AFT CARGO BAY FRAME 55-56, STR 39-40R WEB PLATE HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW ER/A 484892-14MA DIMENSION L=1.80" W=2.00" D=0.047". FABRICATED COVER SHEET IAW STAM TRAVELER T13/97964Feb 7, 2013 · N313US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13006633213Structure · crackedDURING INSPECTION, FOUND LT FWD EMERGENCY EXIT DOOR, AFT LOAD TRANSMITTING PROFILE FASTENER HOLES (5EA) HAS CRACK. HFEC IAW NTM 51-10-08 CRACK INDICATION NOTED .025" LENGTH OF CRACK, NO ALLOWABLE DAMAGE IN SRM. REPLACED LOAD TRANSMITTING PROFILE IAW SRM 51-4Feb 7, 2013 · N313US · Airbus A320211 · Emergency ExitsSDR DALA13006623213Structure · crackedDURING INSPECTION, FOUND LT AFT EMERGENCY EXIT DOOR, AFT LOAD TRANSMITTING PROFILE FOUR FASTENER HOLES HAS CRACK. HFEC IAW NTM 51-10-08 CRACK INDICATION NOTED .025" LENGTH OF CRACK, NO ALLOWABLE DAMAGE IN SRM. REPLACED LOAD TRANSMITTING PROFILE IAW SRM 51-4Feb 7, 2013 · N313US · Airbus A320211 · Emergency ExitsSDR DALA13006353213Structure · corrodedDURING INSPECTION, FOUND LT AFT EMERGENCY EXIT DOOR FWD LOWER T SECTION HAS CORROSION. REMOVED OLD "T" SECTION IAW SRM 51-42-11. TREATED AND PRIMED HOLES IAW SRM 51-42-11 LOCATED AND DRILLED NEW "T" SECTION IAW SRM 5 1-44-11.INSTALLED NEW "T" SECTION IAW SRM Feb 6, 2013 · N313US · Airbus A320211 · Emergency ExitsSDR DALA13006483213Profile · crackedDURING INSPECTION, FOUND LT AFT EMERGENCY EXIT DOOR, AFT LOAD TRANSMITTING PROFILE (4EA) FASTENER HOLES HAS CRACK. CRACK INDICATION NOTED .025" LENGTH OF DAMAGE, NO ALLOWABLE DAMAGE IN SRM. REPLACED LOAD TRANSMITTING PROFILE IAW SRM 51-42-11 AND DWG D5227904Feb 6, 2013 · N313US · Airbus A320211 · Emergency ExitsSDR DALA13006433213Structure · crackedDURING INSP, FOUND RT FWD EMERGENCY EXIT DOOR, FWD LOAD TRANSMITTING PROFILE (9EA) FASTENER HOLE HAS CRACKED. HFEC IAW NTM 51-10-08 CRACK INDICATION NOTED .025" NO ALLOWABLE DAMAGE IN SRM. REPLACED LOAD TRANSMITTING PROFILE IAW SRM 51-42-11.Feb 6, 2013 · N313US · Airbus A320211 · Emergency ExitsSDR DALA13006423213Structure · crackedDURING INSPECTION, RT AFT EMERGENCY EXIT DOOR, AFT LOAD TRANSMITTING PROFILE FASTENER HOLE HAS CRACK. HFEC IAW NTM 51-10-08 CRACK INDICATION NOTED .027" LENGTH OF DAMAGE, NO DAMAGE ALLOWED IAW SRM. REPLACED LOAD TRANSMITTING PROFILE IAW SRM 51-42-11 AND DWG Feb 6, 2013 · N313US · Airbus A320211 · Emergency ExitsSDR DALA13006413213Structure · corrodedDURING INSPECTION, FOUND RT FWD EMERGENCY EXIT DOOR LOWER AFT TEE SECTION HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00 L=.90" W=.80" D=.010" NO ALLOWABLE DAMAGE IN SRM. REPLACED T-SECTION PN D5227905420400 IAW SRM 51-42-11 AND DWG D52279040.Feb 6, 2013 · N313US · Airbus A320211 · Emergency ExitsSDR DALA13006403213Structure · corrodedDURING INSPECTION, FOUND RT FWD EMERGENCY EXIT DOOR, FWD LOWER TEE SECTION HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00 L=1.0" W=.70" D=.012" NO ALLOWABLE DAMAGE IN SRM. REPLACED T-SECTION PN D5227905420400 IAW SRM 51-42-11 AND DWG D52279040.Feb 6, 2013 · N313US · Airbus A320211 · Emergency ExitsSDR DALA13006393213Structure · corrodedDURING INSPECTION, FOUND RT AFT EMERGENCY EXIT DOOR, FWD LOWER TEE SECTION HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00 L=2.0" W=1.5" D=.040" NO ALLOWABLE DAMAGE IN SRM. REPLACED T-SECTION PN D5227905420400 IAW SRM 51-42-11 AND DWG D52279040.Feb 6, 2013 · N313US · Airbus A320211 · Emergency ExitsSDR DALA13006383213Floor Support · corrodedDURING INSPECTION, FOUND AFT CARGO BAY FRAME 59 STR 44 FLOOR SUPPORT HAS CORROSION. REMOVED CORROSION NO LIMITS IN SRM 53-41-14 L=.5" W=.5" D=.020". REMOVED CORRODED PROFILE. LOCATED AND DRILLED NEW PROFILE. TREATED AND PRIMED HOLES IAW SRM 51-21-, INSTALLEFeb 6, 2013 · N313US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13006673213Floor Support · corrodedDURING INSPECTION, FOUND AFT CARGO FRAME 58-59, STR 44, FLOOR SUPPORT CORRODED. REMOVED AFT CARGO FLOOR SUPPORT IAW A320 SRM 51-42-11 FR 58-59 STR 44. REMOVED CORROSION IAW SRM 51-74-00 OUT OF LIMITS IAW SRM 53-00-14. NO ESTABLISHED LIMITS L=1.5"W=1.0"D=0.03Feb 5, 2013 · N313US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13006333214Skin · corrodedDURING INSPECTION, FOUND RT AFT FUSELAGE LAV VENT HAS CORROSION ON SKIN SURFACE. PERFORMED REPAIR IAW SRM 53-41-11 FIG 205. BLENDED AREA IAW SRM 51-74-00. CHECKED LIMITS DEPTH: 0.011" MAX ALLOW 0.06" FOUND TO BE OUT OF LIMITS IAW SRM 53-41-11, DIAGRAM 102 SHFeb 5, 2013 · N314US · Airbus A320211 · Fuselage Main, Plate/SkinSDR CA130204010Duct · fod(CAN) AFTER DEPARTURE, THERE WAS A STRONG ODOR IN THE CABIN. THE ODOR HAD BEEN PRESENT, BUT MINOR, WHILE ON THE GROUND. THE FLIGHT CREW ELECTED TO DIVERT BACK AND DECLARED AN EMERGENCY DUE TO AN OVERWEIGHT LANDING SITUATION. THE FLIGHT LANDING WAS OTHERWISE Feb 4, 2013 · Airbus A320211 · Air Distribution SystemSDR DALA13006363213Door · corrodedDURING INSPECTION, FOUND LT AFT EMERGENCY EXIT DOOR FWD LOWER T SECTION HAS CORROSION. REMOVED OLD "T" SECTION IAW SRM 51-42-11. TREATED AND PRIMED HOLE S IAW SRM 51-42-11 LOCATED AND DRILLED NEW "T" SECTION IAW SRM 51-44-11. INSTALLED NEW "T" SECTION IAW SRMFeb 4, 2013 · N313US · Airbus A320211 · Emergency ExitsSDR DALA13006323213Structure · gougedDURING INSPECTION, FOUND LT PYLON PYRAMID MATING FACE AFT GUIDE PIN HOLE HAS GOUGE. REMOVED GOUGE IAW A320 TRM 54-51-18. CHECKED LIMITS: AREA 1L=0.284" W=0.062" D=0.063"; AREA 2 L=0.299" W=0.049" D=0.053". FOUND TO BE OUT OF LIMITS IAW TRM 54-51-18 FIG 2. ACFeb 4, 2013 · N313US · Airbus A320211 · Nacelle/Pylon, Main FrameSDR DALA13006313213Structure · gougedDURING INSPECTION, FOUND LT PYLON PYRAMID MATING FACE MID GUIDE PIN HOLE HAS GOUGE. REMOVED GOUGE IAW TRM 54-51-18. CHECKED LIMITS: AREA 1L=0.446" W=0.022" D=0.046"; AREA 2 L=0.338" W=0.047" D=0.080"; AREA 3 L=0.360" W=0.071" D=0.156". FOUND TO BE OUT OF LIMFeb 4, 2013 · N313US · Airbus A320211 · Nacelle/Pylon, Main FrameSDR DALA13006303213Frame · gougedDURING INSPECTION, FOUND FWD CARGO COMPT FR28 FRAME SPLICE AFT FACE IS GOUGED STR 35L. BLENDED FISH PLATE IAW SRM 51-73-00, MEASUREMENTS ARE L=1.5" W=.5" D=. 014, NO LIMITS FOUND IN SRM R & R IAW SRM 51-42-11.Feb 4, 2013 · N313US · Airbus A320211 · Fuselage Main, FrameSDR DALA13006293213Frame Splice · gougedDURING INSPECTION, FOUND FWD CARGO COMPT FR26 FRAME SPLICE AFT FACE IS GOUGED STR 35L. REPLACED FISH PLATE IAW SRM 51-42-11 DWG NR C2.D53230405. BLENDED FISH PLATE IAW SRM 51-73-00, L=2.0" W=1.5" D=1.5" NO ESTABLISHED LIMITS IN SRM.Feb 4, 2013 · N313US · Airbus A320211 · Fuselage Main, FrameSDR DALA13006663213Frame · corrodedDURING INSPECTION, FOUND AFT CARGO FRAME 55-58, STR 43L HAS CORROSION. REMOVED CORROSION IAW 51-74-00 FROM STRINGER 43L BET FRAME 55-58 AND FOUND NO ESTABLISHED DAMAGE LIMITS. DAMAGE DIMENSIONS L=2.5 "W=1.0" D=0.015". REPAIRED STRINGER IAW SRM 53-00-13, FIG Feb 3, 2013 · N313US · Airbus A320211 · Fuselage Main, FrameSDR DALA13006283213Stop Fitting · chafedDURING INSPECTION, FOUND LT AFT PASSENGER ENTRANCE FRAME 68 ROLLER STOP FITTING ON MID OUTER SURFACE HAS CHAFED. REPLACED ROLLER STOP FITTING AT LT AFT PAX ENTRANCE ON FRAME 68 IAW SRM 51-49-00 (TR14925 TORQUE WRENCH USED) DUE TO NO ESTABLISHED LIMIT FOUND IAFeb 3, 2013 · N313US · Airbus A320211 · Fuselage Main, StructureSDR DALA13005903213Skin · gougedDURING INSPECTION, FOUND RT NR 4 SLAT LWR T/E SKIN HAS GOUGE 10" INBD OF SLAT TRACK NR 10. ACCOMPLISHED REPAIR IAW ER/A 509275-14 REV ORIGINAL AS PERMANENT REPAIR SECTION I. DAMAGE DIMENSIONS L=0.70", W=0.30", D=0.125". FOUND TO BE OUT OF LIMITS IAW SRM 57-4Feb 2, 2013 · N313US · Airbus A320211 · Leading Edge DevicesSDR DALA13005893213Stringer · corrodedDURING INSPECTION, FOUND AFT CARGO FRAME 56-57, STR 41L HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. CHECKED DAMAGE DIMENSION S L=5.0" W=1.0"D=0.012". NO ESTABLISHED LIMITS IN SRM. REPLACED STRINGER IAW SRM 51-42-11 AND DWG D53470345.Feb 2, 2013 · N313US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA13005883214Floor Panel · damagedDURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 151PF DAMAGED 12" X 24". FABRICATED FLOOR PANEL IAW DWG 3D25-37705.Feb 1, 2013 · N314US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13005873214Panel · crackedDURING INSPECTION, FOUND FORWARD CARGO SLOPE PANEL 131JF CRACKED 6.0" LONG. FABRICATED SLOPE PANEL IAW DWG 3D25-37705.Feb 1, 2013 · N314US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13005863214Floor Panel · damagedDURING INSPECTION, FOUND AFT PIT FLOOR PANEL 151GF DAMAGED 1" X 2" AND HAS DAMAGED INSERT. FABRICATED FLOOR PANEL IAW DWG 3D25-37705.Feb 1, 2013 · N314US · Airbus A320211 · Fuselage Floor PanelSDR DALA13005853214Panel · delaminatedDURING INSPECTION, FOUND AFT CARGO SLOPE PANEL 151MF DELAMINATED 6" X 4". FABRICATED SLOPE PANEL IAW DWG 3D25-37705.Feb 1, 2013 · N314US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13006373213Floorboard · crackedDURING INSPECTION, FOUND MID CABIN FLOORBOARD 232MF CORNER EDGE IS CRACKED. FLOORBOARD FABRICATED IAW SRM 53-02-00, FIG 209.Jan 31, 2013 · N313US · Airbus A320211 · Fuselage Floor PanelSDR DALA13005583213Floorboard · delaminatedDURING INSPECTION, FOUND MID CABIN BETWEEN FR35 TO 36 MOST CENTER FLOORBOARD 241AF HAS DELAMINATION. REPLACED FLOORBOARDIAW AMM 53-12-12-400-001-A. FABRICATED FLOORBOARD IAW SRM 53-02-00, FIG 209 & DWG 3D25-37498.Jan 30, 2013 · N313US · Airbus A320211 · Fuselage Floor PanelSDR DALA13005573214Panel · damagedDURING INSPECTION, FOUND AFT CARGO SLOPE PANEL 151RF DAMAGED 4" X 4". FABRICATED SLOPE PANEL IAW DWG 3D25-37705.Jan 30, 2013 · N314US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13005563214Panel · damagedDURING INSPECTION, FOUND AFT CARGO SLOPE PANEL 152QF DAMAGED 6" X 4". FABRICATED SLOPE PANEL IAW DWG 3D25-37705.Jan 30, 2013 · N314US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13005553214Panel · damagedDURING INSPECTION, FOUND AFT CARGO SLOPE PANEL 151FF DAMAGED 12" X 6". FABRICATED SLOPE PANEL IAW DWG 3D25-37705.Jan 30, 2013 · N314US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13005543214Panel · damagedDURING INSPECTION, FOUND AFT CARGO SLOPE PANEL 151EF DAMAGED 12" X 12". FABRICATED SLOPE PANEL 151EF ON STAM TRAVELER T13/979335. MATERIAL A402AB-60X144, BATCH 2335662, DWG 3D25-37705.Jan 30, 2013 · N314US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13005533214Panel · delaminatedDURING INSPECTION, FOUND AFT CARGO SLOPE PANEL 151 HF DELAMINATED 8" X 4". FABRICATED SLOPE PANEL 151 HF ON STAM TRAVELER T13/979331. MATERIAL A402AB-60X144, BATCH 2335662, DWG 3D25-37705.Jan 30, 2013 · N314US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13005503214Panel · damagedDURING INSPECTION, FOUND AFT CARGO SLOPE PANEL 151CF DAMAGED 12" X 12". FABRICATED SLOPE PANEL IAW DWG 3D25-37705.Jan 30, 2013 · N314US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13005493214Panel · delaminatedDURING INSPECTION, FOUND AFT CARGO SLOPE PANEL 151 NF DELAMINATED 4" X 4". FABRICATED SLOPE PANEL IAW DWG 3D25-37705.Jan 30, 2013 · N314US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13005483214Panel · damagedDURING INSPECTION, FOUND AFT CARGO SLOPE PANEL 152CF, DAMAGED 12" X 12". FABRICATED SLOPE PANEL IAW DWG 3D25-37705.Jan 30, 2013 · N314US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13005473214Panel · damagedDURING INSPECTION, FOUND AFT CARGO SLOPE PANEL 152EF DAMAGED 12"X36". FABRICATED SLOPE PANEL IAW DWG 3D25-37705.Jan 30, 2013 · N314US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13005463214Panel · crackedDURING INSPECTION, FOUND FWD CARGO SLOPE PANEL 132GF CRACKED 1.0". FABRICATED SLOPE PANEL IAW DWG 3D25-37705.Jan 30, 2013 · N314US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13005453214Floor Panel · damagedDURING INSPECTION, FOUND FWD CARGO FLOOR PANEL 132 FF, DAMAGED 2.0"X2.0". FABRICATED FLOOR PANEL IAW DWG 3D25-37705.Jan 30, 2013 · N314US · Airbus A320211 · Fuselage Floor PanelSDR DALA13005443214Panel · damagedDURING INSPECTION, FOUND FWD CARGO SLOPE PANEL 131FF DAMAGE AT TDP. FABRICATED SLOPE PANEL IAW DWG 3D25-37705.Jan 30, 2013 · N314US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13005433214Panel · puncturedDURING INSPECTION, FOUND FWD CARGO SLOPE PANEL 131KF PUNCTURED 2.0" X 1.0". FABRICATED SLOPE PANEL IAW DWG 3D25-37705.Jan 30, 2013 · N314US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13005423214Panel · damagedDURING INSPECTION, FOUND FWD CARGO SLOPE PANEL 132JF HAS DAMAGE AT TDP. FABRICATED SLOPE PANEL IAW DWG 3D25-37705.Jan 30, 2013 · N314US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13005413214Panel · damagedDURING INSPECTION, FOUND FWD CARGO SLOPE PANEL 131CF DAMAGED AT TDP. FABRICATED FLOOR PANEL IAW DWG 3D25-37705.Jan 30, 2013 · N314US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13005403214Floor Panel · delaminatedDURING INSPECTION, FOUND FWD CARGO FLOOR PANEL 131 EF DELAMINATED 40"X3.5". FABRICATED FLOOR PANEL IAW DWG 3D25-37705.Jan 30, 2013 · N314US · Airbus A320211 · Fuselage Floor PanelSDR DALA13005393214Floor Panel · damagedDURING INSPECTION, FOUND FWD CARGO FLOOR PANEL 131AF DAMAGED TDP. FABRICATED FLOOR PANEL IAW DWG 3D25-37705.Jan 30, 2013 · N314US · Airbus A320211 · Fuselage Floor PanelSDR DALA13005313214Panel · damagedDURING INSPECTION, FOUND FWD CARGO SLOPE PANEL 132KF DAMAGED. FABRICATED FLOOR PANEL IAW DWG 3D25-37705.Jan 30, 2013 · N314US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13005383213Floor Panel · damagedDURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 161 BF IS DAMAGED. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209. INSTALLED ON WC 2500-5019 AND DWG 3D25-37705. MISSING INSERTS & EDGE DELAMINATED.Jan 29, 2013 · N313US · Airbus A320211 · Fuselage Floor PanelSDR DALA13005363214Floor Panel · damagedDURING INSPECTION, FOUND AFT CABIN FLOOR PANEL 261EF DAMAGED/DELAMINATED. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209 & DWG 3D25-37498.Jan 29, 2013 · N314US · Airbus A320211 · Fuselage Floor Panel
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