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 DALA2015112107211Floor Support · corrodedFWD GALLEY AREA CORROSION ON FLOORBEAM 765 BETWEEN FRAME 12 TO FRAME 24 MEASURES APPROXIMATELY L:0.980", W:0.700", D:0.002". REPLACED FLOORBEAM 765 BETWEEN FRAME 12 TO FRAME 24 IAW SRM 51-72-11 AND DWG D53110920. MEASURES OF CORROSION ARE: L=1.470", W=1.071"SDR DALA2015112107210Seat Track · corrodedUPPER FLANGE IN PASSENGER CABIN CORROSION OUT LIMIT SEAT TRACK +Y1292, FRAME 35 TO 36, MEASURES ARE: FR 35 +8", L: 3.905", W: 0.381", D: 0.042'. REPLACED SEAT TRACK 1292 AND FASTENER LOCATED FRAME 35 TO FRAME 36 IAW SRM 51-72-11 AND DWG D53370124.SDR DALA2015112007113Web · corrodedCORROSION ON WEB BETWEEN FRAME 20 AND FRAME 24 MEASURES APPROXIMATELY L:0.210", W:0.190", D:0.003", RT SIDE AT FWD GALLEY AREA. REPLACED WEB BETWEEN FRAME 20 AND FRAME 24 RT SIDE AT FWD GALLEY AREA IAW SRM 51-72-11 AND DWG D53112783, D53114392. MEASURES OF CSDR DALA2015112007112Attach Fitting · damagedWEAR FIXED BUSHING INBD LUG ON AILERON OTBD ATTACHMENT FITTING ACTUATOR ON RT WING, REPLACED BUSHING, 1EA ON INBD LUG ON AILERON OTBD FITTING ACTUATOR RT WING IAW CMM 57-61-21.SDR DALA2015112007111Floor Support · corrodedCORROSION ON FLOORBEAM -Y1162 BETWEEN FRAME 67+15" TO FRAME 69 MEASURES APPROXIMATELY L:0.300", W:0.175", D:0.003" AT AFT GALLEY AREA, REPLACED FLOORBEAM -Y1162 BETWEEN FRAME 67+15" TO FRAME 69 AT AFT GALLEY AREA IAW SRM 51-72-11 AND DWG D53472000. MEASURE ARSDR DALA2015112007110Floor Support · corrodedCORROSION ON FLOORBEAM -Y1225 BETWEEN FRAME 66+5" TO FRAME 67+15" MEASURES APPROXIMATELY L:0.400", W0.260", D:0.003", AT AFT GALLEY AREA, REPLACED FLOORBEAM -Y1225 BETWEEN FRAME 66+5" TO FRAME 67+15" AT AFT GALLEY AREA IAW SRM 51-72-11 AND DWG D53472000. MEASDR DALA2015112007102Seat Track · crackedCRACK ON SEAT TRACK -Y765, FRAME 36 TO 41 IN PASSENGER CABIN, REPLACED SEAT TRACK -Y765 LOCATION BETWEEN FRAME 36 TO FRAME 41 IAW SRM 51-72-11 AND DWG D53370500 AND D57130147 MEASURE ARE: CRACK, L=0.980".SDR DALA2015111907116Seat Track · crackedCRACK ON SEAT TRACK -Y1292, FRAME 36 TO 41 IN PASSENGER CABIN, REPLACED SEAT TRACK -Y1292 FR36 TO 41 IN PASSENGER CABIN IAW SRM 51-72-11 AND DWG D53370500 MEASURE OF CRACK IS 0.517".SDR CA151117004Actuator · failed(CAN) ON APPROACH AIRCRAFT HAD SLAT/FLAP FAILURE, GO-AROUND WAS CONDUCTED AND FLAPS WERE RECYCLED THREE TIMES AND EVERYTHING SEEMED TO WORK OK. TOWER ADVISED ARFF WERE PRESENT FOR PRE-CAUTIONARY REASONS ONLY. ACFT WAS TAKEN OFF-LINE FOR MAINTENANCE INVESTIGASDR DALA2015112007115Wire · brokenROW 21 ACFT LT EMERGENCY LIGHT IN SEAT INOPERATIVE, REPAIRED BROKEN WIRE.SDR DALA2015112007114Wire · brokenROW 18 ACFT LEFT EMERGENCY LIGHT IN SEAT INOPERATIVE, REPAIRED BROKEN WIRE.SDR DALA2015111807109Skin · not reportedPERFORMED NEW REPAIR ON EXTERNAL SKIN TAIL CONE LT SIDE BETWEEN FRAME 84 TO FRAME 85 ON UPPER FUSELAGE IAW SRM 53-51-11, PARAGRAPH 5.B, FIG 203.SDR DALA2015111807108Seat Track · corrodedCORROSION ON FLOORBEAM -Y765 BETWEEN FRAME 12 TO FRAME 24 MEASURES APPROXIMATELY L:0.900", W:0.400", D:0.003" AT FWD GALLEY AREA, REPLACED SEAT TRACK -Y765 LOCATED BETWEEN FRAME 12 TO FRAME 24 IAW SRM 51-72-11 AND DWG D53110920 MEASURES OF CORROSION P1: FR20SDR DALA2015111807107Floor Support · corrodedCORROSION ON FLOORBEAM -Y189 BETWEEN FRAME 20 TO FRAME 23 MEASURES APPROXIMATELY L:1.5", W:1", D:0.002" AT FWD GALLEY AREA, REPLACED FLOORBEAM -Y189 BETWEEN FRAME 20 TO FRAME 23 SRM 51-72-11 AND DWG D53112834 MEASURES OF CORRODED AREA ARE L=2.362", W=1.189", SDR DALA2015111807106Skin · not reportedPERFORMED NEW REPAIR ON EXTERNAL SKIN ON FRAME 23 AND BETWEEN STR 22L TO STR 23L IAW SRM 53-00-11, PARA 4.W, REPAIR 7, FIG 238. RECHECK REQUIRED AT 60,000FC IAW SRI 53-00-11 PARA 32 IIR 53-00-11-2-017-00, TABLE 225, PAGE 289.SDR DALA2015111807105Skin · not reportedPERFORMED NEW REPAIR ON EXTERNAL SKIN BETWEEN FRAME 51 TO FRAME 52 AND BETWEEN STR 38R TO STR 39R IAW SRM 53-41-11, PAR 5F, REPAIR 4, FIG 207.SDR DALA2015111707104Floor Support · corrodedCORROSION ON FLOORBEAM +Y512 BETWEEN FR 64 TO FR 70 MEASURES APPROXIMATELY L=0.270", W=0.115", D=0.003" AT AFT GALLEY AREA. REPLACED FLOORBEAM Y512 BETWEEN FRAME 64 TO FRAME 70 IAW SRM 51-72-11 AND DWG D53472000 MEASURES OF CORROSION ARE L=1.484", W=0.371", DSDR DALA2015111606996Floorbeam · damagedELONGATED HOLE CROSSBEAM SECTION ON FLOOR STRUCTURE AT AFT GALLEY AREA ON FRAME 68 STR 24L. REPLACED CROSSBEAM SECTION ON FLOOR STRUCTURE AT AFT GALLEY AREA ON FRAME 68 BETWEEN. STR 23L AND STR 24L IAW SRM 51-72-11 AND DWG D53470150. MEASURE OF ELONGATED HOSDR DALA2015111606995Seat Track · corrodedCORROSION ON SEAT TRACK +Y1292 FRAME 47 TO 64 EVALUATED AND FOUND OUT OF LIMITS ON JC 2500-2032 IN PASSENGER CABIN. MEASURE OF REWORKED ARE: L=3.955, W=0.356, D=0.051. REPLACED SEAT TRACK +Y1292 LOCATED BETWEEN. FRAME 47 TO FRAME 64 IN PASSENGER CABIN. AS IAWSDR DALA2015111606994Seat Track · corrodedCORROSION ON SEAT TRACK -Y1292 BETWEEN FRAME 12 TO FRAME 24 MEASURES APPROXIMATELY L=1", W=0.200", D=0.002" AT FWD GALLEY AREA. REPLACED SEAT TRACK -Y1292 LOCATED BETWEEN FRAME 12 TO FRAME 24 AT FWD GALLEY AREA IAW SRM 51-72-11 AND DWGS NR D53112812, D531109SDR DALA2015111606993Seat Track · corrodedCORROSION OUT LIMIT SEAT TRACK +Y765, FRAME 41 TO 47 EVALUATED WITH JC 2500-2031 MEASURE ARE: FR 44+7", L=3.869", W=0.385", D=0.043", UPPER FLANGE IN PASSENGER CABIN. REPLACED SEAT TRACK +Y765 LOCATED BETWEEN FRAME 41 TO FRAME 47 IAW SRM 51-72-11 AND DWGS D53SDR DALA2015111606992Floor Support · corrodedCORROSION ON FLOORBEAM +Y254 BETWEEN, FRAME 12 TO FRAME 24 MEASURES APPROXIMATELY L=0.105", W=0.100", D=0.003" AT FWD GALLEY AREA, REPLACED FLOORBEAM +Y254 BETWEEN FRAME 12 TO FRAME 24 IAW SRM 51-72-11, MEASURE OF CORROSION ARE L=0.452", W=0.377", D=0.080SDR DALA2019072804508Stop Fitting · crackedCRACK INDICATION DOOR STOP FITTING ON FRAME 68 LOC BTW STR 21L TO STR 22L CRACK DIRECTION: 6 O'CLOCK APPROX AT AFT GALLEY AREA, REPAIR ON DOOR STOP FITTING AND FRAME 68 LOC BTW STR.21L TO STR.22L AT AFT GALLEY AREA AS PER SRM 53-41-12 PARAGRAPH 5.C AND 5.E FIGSDR DALA2019072804507Stop Fitting · crackedCRACK INDICATION DOOR STOP FITTING ON FRAME 68 LOC BTW STR 21R TO STR 22R CRACK DIRECTION: 6 O'CLOCK APPROX AT AFT GALLEY AREA, PERFORMED PERMANENT REPAIR ON DOOR STOP FITTING ON FR.68 LOC BTW STR.21R TO STR.22R AT AFT GALLEY AREA AS PER SRM 53-41-12 PARAGRAPHSDR DALA2015111306956Battery Pack · inoperativeAFT LT EMERGENCY LIGHT FAULT, REPLACED BATTERY.SDR DALA2015111206952Skin · corrodedCORROSION ON INSIDE SURFACE OF SKIN OTBD OF STR 42L BETWEEN FRAMES 56-57. PRI 541258-14AD, REV O,1,2. C/W PRI 541258-14AD, REV 2, STEP 9.SDR DALA2015111206951Skin · corrodedCORROSION ON SKIN UNDER STR 43L BETWEEN FRAME 56 & 57, PRI 541258-14AD, REV 0, 1, 2 AND ER/A 541258-14AD. BLENDED OUT CORROSION UNDER SKIN IAW 51-74-00, MININUM REMAINING THICKNESS .148.SDR DALA2015111206950Stringer · corrodedCORROSION ON STR 42L BETWEEN 56-57. EXISTING REPAIR BETWEEN FRAMES 57-58 AND A SPLICE UNDER FRAME 53. FABRICATED STR 42L BETWEEN FRAMES 55 & 58 AND COUPLER IAW SRM 53-00-13, FIG 201. TREATED AND PRIMED AND PAINTED IAW SRM 51-75-12, INSTALLED STR 42L IAW SRMSDR DALA2015111206949Stringer · corrodedCORROSION ON STR 43L BETWEEN FRAMES 56-57. EXISTING SPLICE BETWEEN FRAMES 56-57 AND A SPLICE UNDER FRAME 54. FABRCATED STR 43L BETWEEN FRAMES 55 & 58 AND COUPLERS IAW SRM 53-00-13, FIG 201. TREATED PRIMED AND PAINTED STR IAW 51-75-12 INSTALLED STRINGER 43LSDR DALA2015111106948Battery Pack · failedLINE CHECK OF THE CABIN EMERGENCY LIGHTS FAILED, FWD LT EPSU BATTERY FAULT. REPLACED BATTERY.SDR DALA2015110906868Angle · not reportedREPLACED ANGLE ON INTERNAL STRUCTURE BOTTOM SKIN OF KEELBEAM IN MAIN WHEEL WELL ON STR 43L BETWEEEN FRAME 45 TO FRAME 46 IAW SRM 51-72-11 AND DWG D53371804.SDR DALA2015110906867Angle · not reportedREPLACED ANGLE ON INTERNAL STRUCTURE EXTERNAL BOTTOM SKIN OF KEELBEAM IN MAIN WHEEL ON STR 43R BETWEEN FRAME 45 TO FRAME 46 IAW SRM 51-72-11 AND DWG D53371804.SDR DALA2016042003047Skin · gougedGOUGE FOUND ON AFT CARGO COMPARTMENT DOOR OUTER SKIN BETWEEN FRAME 54 AND FRAME 54A AND AT BEAM 4. PERFORMED PERMANENT RAPAIR ON EXTERNAL SKIN ON DOOR 826 LOCATED 33" AFT EDGE IN AFT CARGO COMPARTMENT IAW ER/A NR 54-0586-14, REV 0, MEASURE OF DAMAGE IS L:0.3SDR DALA2015110706866Skin · dentedDENT ON EXTERNAL SKIN PASSENGER CREW DOOR 831, LOCATED AFT LOWER EDGE AT FWD GALLEY AREA. PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN PASSENGER CREW DOOR 831 LOCATED AFT LOWER EDGE IAW SRM 52-10-00, PARA 5 C, FIGURE 203.SDR DALA2015110606776Strap · corrodedCORROSION ON INTERNAL STRUCTURE STRAP, LOCATED STR 43R TO STR 44 AND FRAME 64 MEASURES ARE: L=2.810", W=1.300" APPROXIMATELY. REPLACED STRAP LOCATED INTERNAL STRUCTURE STR 43R TO STR 44 AND FRAME 64 IN AFT CARGO COMPARTMENT IAW SRM 51-72-11 AND DWG D534-7034SDR DALA2016112509235Boss · corrodedCORROSION FOUND ON FWD WEB BOSS OF MLG RIB GEAR SUPPORT AT RIB 5 AREA OF THE RH WING. PERFORMED TIME LIMITED REPAIR IAW ERA.SDR DALA2015110606777Stringer · corrodedCORROSION STR 27LT INTERNAL STRUCTURE AT LEVEL FRAME 67 AT LOWER FUSELAGE, REPLACED SECTION CONNECTION ON STRINGER 27LT AT LEVEL FRAME 67 IAW PRI 540587-14, REV 0 AND ER/A 540587-14, REV ORIGINAL.SDR DALA2016111708957Support · corrodedCORROSION FOUND ON FWD WEB BOSS OF MLG RIB GEAR SUPPORT AT RIB 5 AREA OF THE LT WING. PERFORMED TIME LIMITED REPAIR ON FALSE SPAR BOX OUTBOARD FACE OF THE OUTER GEAR-SUPPORT RIB#5 AS PER PRELIMINARY REPAIR INSTRUCTION ERA 570607-14.SDR DALA2015110206724Floor Panel · delaminatedDELAMINATED FLOOR PANEL 261FF AT AFT GALLEY AREA, REPLACED FLOOR PANEL 261FF AT AFT GALLEY AREA.SDR DALA2015102606525Stringer · corrodedCORROSION ON STRINGER 30L, FRAME 67. REPLACED THE STRINGER IAW SRM 51-72-11 AND DWG D53480019.SDR DALA2015102606524Fitting · corrodedCORROSION FITTINGS ON EMERGENCY EXIT DOOR. REPLACED THE FITTING IAW SRM 51-72-11 AND DWG D522-79040.SDR DALA2015102606523Support · corrodedCORROSION ON LOWER SUPPORT BETWEEN FRAMES 66 TO 68 AND STRINGER 23R AT A FT GALLEY AREA. REPLACED LOWER SUPPORT IAW SRM 51-72-11 AND DWG D53480019, E53474250.SDR DALA2015102606522Fitting · corrodedCORROSION ON CORNER FITTING FRAME 66, RT MEASURE OF CORROSION ARE AT AFT GALLEY AREA. REPLACED CORNER FITTING FRAME 66 RT AT AFT GALLEY AREA IAW SRM 51-72-11 AND DWG D53480019.SDR DALA2015102606521Floor Support · corrodedCORROSION ON FLOOR SUPPORT -Y254, FRAMES 12 TO 24. REPAIRED THE FLOOR SUPPORT IAW SRM 53-00-14, PARA 4.F, FIG 206.SDR DALA2015102606430Fitting · corrodedCORROSION FITTING ON EMERGENCY EXIT DOOR 834 IN PASSENGER CABIN. REPLACED FITTING ON EMERGENCY EXIT DOOR 834 IAW SRM 51-72-11 AND DWG D522-79040, JOB COMPLETE.SDR DALA2015102606429Floor Support · corrodedCORROSION ON FLOOR SUPPORT -Y765, FRAMES 12 TO 24. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, DWS D53112812, D53110984, AND D53110920.SDR DALA2015102606428Fitting · corrodedCORROSION FITTING ON EMERGENCY EXIT DOOR 844 IN PASSENGER CABIN. REPLACED FITTING ON EMERGENCY EXIT DOOR 844 IAW SRM 51-72-11 AND DWG D522-79040.SDR DALA2015102606431Web · corrodedCORROSION ON WEB AT STR 38L, FRAMES 33 - 34 . REPLACED THE WEB IAW SRM 51-72-11 AND DWG D53230340.SDR DALA2015102506415Shear Tie · corrodedCORROSION ON CLEAT FRAME 28 LT IN FWD CARGO COMPARTMENT BETWEEN STR 40L TO STR 41L SSI 532180. REPLACED CLEAT AND FASTENERS LOCATED ON FRAME 28 LT SIDE IN FWD CARGO COMPARTMENT BETWEEN STR 40L TO STR 41L IAW SRM A320 51-72-11 AND DWG D53231712.SDR DALA2015102506414Shear Tie · corrodedCORROSION ON CLEAT FRAME 26 LT IN FWD CARGO COMPARTMENT BETWEEN STR 42L TO STRINGER 43L. REPLACED CLEAT LOCATED AT FRAME 26 IN FWD CARGO COMPARTMENT BETWEEN STR 42L TO STRINGER 43L IAW SRM 51-72-11 AND DWG D53231712.
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