N112US
Service difficulty reports · 251
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
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 n_number = 'N112US' AND registry_match = 'registration' 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 n_number = 'N112US' AND registry_match = 'registration' 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 USAA2014081900005Flap · crackedFTIS VISIT TWO CRACKS OF 0.75 INCHES & 2.5 INCHES ON RT WING TE FLAP LE AT APPROX 2 INCHES FROM OTBD END & BETWEEN RIB 9 & 10. REPAIRED RT WING TE FLAP LE IAW SRM 57-53-00-201 & 51-23-11.SDR USAA2014072100010Stator · inoperativeAIRCRAFT DIVERTED FOR A ECAM ENG NR 1 FADEC ALTERNATOR MSG. PERFORMED TEST FOR LOSS OF POWER IAW TSM 77-10-00-810-839-A. REPLACED ALTERNATOR STARTER IAW AMM 73-21-300-000-001 & 400-001.SDR USAA2014061200026Slide Raft · defectivePERFORMING EO 2514Y110 FOUND CONTACT BETWEEN THE SLIDE RAFT COVER AT DOOR L1 & THE FUSELAGE. NO DAMAGE FOUND. PLACED ON MONITOR, INSPECT EVERY 100 HRS. REPLACED SLIDE AT NEXT HEAVY CHECK. REPLACED EMER EXIT SLIDE AT DOOR L1 IAW JOB CARD 26L00025011.SDR USAA2014030600002Lens · missingEMERGENCY LIGHT LENS MISSING AT ROW 11 LT. REPLACED EMERGENCY LIGHT LENS AT ROW 11 LT.SDR USAA2013120900011Light · inoperativeEMERGENCY ESCAPE DOORS LIGHTING INOPERATIVE ON BOTH FWD LT & RT HANDLE ILLUMINATING. REPLACED LIGHT BULBS ON EMERGENCY ESCAPE DOORS. LIGHTING ON BOTH FWD LT & RT HANDLE ILLUMINATING AS REQUIRED.SDR USAA2013112500007Damper · damagedL1 DOOR EMERGENCY OPERATION CYLINDER HAS DAMAGED SPRING IN TRIGGER ASSEMBLY. REPLACED L1 DOOR DAMPER CYLINDER IAW A320 AMM 52-11-14.SDR USAA2013111800014Lens · missingCREW REPORTED THE FLOOR LEVEL EMERGENCY EXIT SIGN NEAR DOOR 1L LENS MISSING. MAINTENANCE REPLACED LENS. LIGHT CHECKS OK.SDR USAA2013100400004Battery · inoperativeF/A SEAT DOOR 2L FLASHLIGHT BATTERY DEAD. REPLACED BATTERY.SDR USAA2013021400009Strap · unsecure2R DOOR SQUEAL REPORTED. FOUND SLIDE RETAINER STRAP BETWEEN SEAL AND FRAME. SECURED STRAP.SDR USAA2013011800013Lens · missingEMERGENCY LIGHT LENS COVERS MISSING AT LEFT ROWS 9 & 11. INSTALLED COVERS AT ROWS 9 & 11.SDR USAA2012100500040Connector · disconnectedEMERGENCY LIGHT AT SEAT 24 ABC INOPERATIVE. RECONNECTED PLUG, OPERATIONAL CHECK GOOD.SDR USAA2012071800001Bellcrank · out of adjustL1 DOOR PERCUSSION BELLCRANK FINGER REQUIRES ADJUSTMENT FOLLOWING SCHEDULED SLIDE DEPLOYMENT. SLIDE FULLY DEPLOYED IN 8 SECONDS BUT DOOR FAILED TO OPEN DUE TO MISALIGNMENT WITH STRIKER. ADJUSTED PERCUSSION BELLCRANK FINGER IAW AIRBUS MAINTENANCE MANUAL 52-11SDR USAA2012042300042Circuit Breaker · trippedCREW REPORTED ON DESCENT THAT BRAKE ACCUMULATOR PRESSURE WAS ZERO WITH GEAR DOWN AND BRAKE PEDALS HAD NO RESISTANCE (FELT SPONGY). CREW WAS ADVISED THAT AIRCRAFT WOULD STILL HAVE NORMAL BRAKING AND ANTI-SKID AVAILABLE, BUT DECLARED AN EMERGENCY AND LANDED WITSDR USAA2012042300040Megaphone · inoperativeAFT MEGAPHONE INOPERATIVE. REPLACED AFT CABIN MEGAPHONE.SDR USAA2012021600011Control Panel · defectiveENGINE NR 1 AGENT 1 DISCHARGE CAME ON IN FLIGHT. MAINTENANCE REMOVED AND REPLACED THE ENG/APU FIRE PANEL 1WD IAW AIRBUS MAINTENANCE MANUAL 26-12-12.SDR USAA2012020900012Slide Raft · faultyPILOT REPORTED L1 DOOR SLIDE WOULD NOT ARM. REMOVED AND REPLACED L1 DOOR ESCAPE SLIDE/ RAFT AND GIRT BAR ASSEMBLY IAW AIRBUS MAINTENANCE MANUAL 52-11-22.SDR USAA2012010900042Lens · brokenEXIT LIGHT COVER BROKEN AT 15C. REPLACED LENS 15C.SDR USAA2011111100008Slide Raft · faultyLEFT AFT EXTERNAL LOAD MESSAGE ON EMERGENCY LIGHTS SYSTEM BITE TEST. MAINTENANCE REMOVED AND REPLACED LEFT AFT SLIDE RAFT.SDR USAA2011111100007Power Supply · faultyLEFT EMERGENCY POWER SUPPLY UNIT FAULT. MAINTENANCE REMOVED & REPLACED LEFT EPSU & BATTERY IAW AIRBUS MAINTENANCE MANUAL 33-51-38.SDR USAA2011092900001Cylinder · failed2S CHECK - DURING OPERATIONAL TEST OF DAMPING FUNCTION A HARD IMPACT WAS FOUND BETWEEN THE DOOR SLIDERS AND PASSENGER CREW R2 DOOR 841. REPLACED R2 DOOR DAMPER CYLINDER IAW A320 AMM 52-11-14-400-0001, 52-11-14-000-001.SDR USAA2011092600012Container · delaminated2S CHECK - DELAMINATION ON RIGHT OFF WING ESCAPE SLIDE ENCLOSURE AT 194AT FAIRING. REPLACED RIGHT OFF WING ESCAPE SLIDE ENCLOSURE ASSEMBLY AT 194AT FAIRING PER JC 26C19053012.SDR USAA2011092600013Slide Raft · misinstalled2S CHECK - SLIDE/RAFT AT DOOR 841 HITS FUSELAGE WHEN DOOR IS FULLY OPEN. REPACKED SLIDE RAFT AT DOOR 841 IAW CMM 25-61-20 REV 16 PAGE 309 SECC, DISASSEMBLY AND FOLDING PROCEDURE P-11921 REV AC.SDR USAA2011092700004Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 232FF BETWEEN FR20 TO FR24, BETWEEN -Y1732 TO -Y1292. REPLACED FLOOR PANEL 232FF BETWEEN FR20 TO FR24, BETWEEN -Y1732 TO -Y1292 IAW A320 SRM 53-12-00, IRM 9701 REV G.SDR USAA2011101000015Frame · cracked2S CHECK - CRACK INNER FRAME SEGMENT OF RIGHT EMERGENCY EXIT HATCH DOOR BETWEEN FR40 TO FR41 & BETWEEN BEAM 1 TO BEAM 3. REPLACED INNER FRAME SEGMENT IAW EO 5210Y228.SDR USAA2011101000014Frame · cracked2S CHECK - CRACK INNER FRAME SEGMENT OF LEFT EMERGENCY EXIT HATCH DOOR BETWEEN FR40 TO FR41 & BETWEEN BEAM 1 TO BEAM 3. REPLACED INNER FRAME SEGMENT IAW EO 5210Y228.SDR USAA2011101000013Frame · cracked2S CHECK - CRACK INNER FRAME SEGMENT OF RIGHT EMERGENCY EXIT HATCH DOOR BETWEEN FR38 TO FR39 & BETWEEN BEAM 1 TO BEAM 3. REPLACED INNER FRAME SEGMENT IAW EO 5210Y228.SDR USAA2011101000012Frame · cracked2S CHECK - CRACK INNER FRAME SEGMENT OF LEFT EMERGENCY EXIT HATCH DOOR BETWEEN FR38 TO FR39 & BETWEEN BEAM 1 TO BEAM 3. REPLACED INNER FRAME SEGMENT IAW EO 5210Y228.SDR USAA2011092300011Web · cracked2S CHECK - CRACK ON WEB BETWEEN FR8 TO FR11, Y765. REPLACED WEB BETWEEN FR8 TO FR11, Y765 IAW A320 SRM 51-72-11.SDR USAA2011100300038Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR24 TO FR35, -Y1292. REPLACED SEAT TRACK BETWEEN FR24 TO FR35, -Y1292 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53370000.SDR USAA2011093000013Fitting · corroded2S CHECK - CORROSION ON CORNER FITTING AT FR68, S23R. REPLACED CORNER FITTING AT FR68, S23R IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53480505.SDR USAA2011092800017Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR43 TO FR46, -Y1292. REPLACED SEAT TRACK BETWEEN FR43 TO FR46, -Y1292 IAW A320 SRM 51-72-11.SDR USAA2011092800016Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK AT FR38 + 8 INCHES, Y1292. REPLACED SEAT TRACK AT FR38 + 8 INCHES, Y1292 IAW A320 SRM 51-72-11 & AIRBUS DRAWING 57130147.SDR USAA2011100500004Sill · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON LOWER SILL BETWEEN FR67+15 INCHES TO FR68+2 INCHES, S23R. REPLACED LOWER SILL A320 SRM 51-72-11, AIRBUS DRAWING D53480505 & EA 133802.SDR USAA2011100300037Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON RAIL SEAT BETWEEN FR47 TO FR63, Y1292. REPLACED RAIL SEAT BETWEEN FR47 TO FR63, Y1292 IAW A320 SRM 53-41-15 FIG 202.SDR USAA2011093000014Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR59 TO FR59, -Y1292. REPAIRED SEAT TRACK BETWEEN FR59 TO FR59, -Y1292 IAW A320 SRM 53-41-15.SDR USAA2011093000010Seat Track · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT RAIL BETWEEN FR55 TO FR56, Y765. REPLACED SEAT RAIL BETWEEN FR55 TO FR56, Y765 IAW A320 SRM 53-00-15 FIGURE 201 PAGE 207 AND 208.SDR USAA2011101000005Sill · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON L2 DOOR SILL BETWEEN FR67 TO FR68 PLUS 2 INCHES, S23L. REPAIRED L2 DOOR SILL BETWEEN FR67 TO FR68 PLUS 2 INCHES, S23L IAW EA 133779 PART 2.SDR USAA2011100600029Skin · saturated2S CHECK - TRAPPED WATER INDICATION ON LEFT ELEVATOR UPPER SURFACE BETWEEN THS STA 527 TO STA 589 & BETWEEN THS RIB 12 TO RIB 13. REPAIRED LEFT ELEVATOR UPPER SURFACE IAW A320 SRM 55-21-11 PAR 5N.SDR USAA2011100600028Skin · saturated2S CHECK - TRAPPED WATER INDICATION ON LEFT ELEVATOR UPPER SURFACE BETWEEN THS STA 466 TO STA 527 & BETWEEN THS RIB 11 TO RIB 12. REPAIRED LEFT ELEVATOR UPPER SURFACE IAW A320 SRM 55-21-11 PAR 5N.SDR USAA2011100300036Floor Support · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT BETWEEN FR16 TO FR21, -Y254. REPLACED FLOOR SUPPORT BETWEEN FR16 TO FR21, -Y254 IAW A320 SRM 53-11-14.SDR USAA2011100300035Floor Support · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT BETWEEN FR18 TO FR24, Y254. REPLACED FLOOR SUPPORT BETWEEN FR18 TO FR24, Y254 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53110900.SDR USAA2011093000017Skin · saturated2S CHECK - AREA OF WATER INGRESS ON RIGHT ELEVATOR UPPER SURFACE BETWEEN THS STA 527 TO STA 584 & BETWEEN THS RIB 12 TO 13 APPROX 4.5 INCHES FROM TRAILING EDGE. REPAIRED RIGHT ELEVATOR UPPER SURFACE IAW SRM A320 55-21-11.SDR USAA2011093000012Skin · saturated2S CHECK - WATER INGRESS ON RIGHT ELEVATOR UPPER SKIN AT BETWEEN STAB STATION 466 TO STAB STATION 527, BETWEEN RIB 11 TO RIB 12, 6 INCHES FROM TRAILING EDGE. REPAIRED RIGHT ELEVATOR UPPER SKIN IAW A320 SRM 55-21-11 PARA 5D.SDR USAA2011093000009Floorbeam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR64 TO FR66, Y1292. REPLACED FLOORBEAM BETWEEN FR64 TO FR66, Y1292 IAW A320 SRM 51-72-11.SDR USAA2011092900008Skin · saturated2S CHECK - WATER INGRESS ON LEFT ELEVATOR UPPER SKIN BETWEEN STAB STATION 277 TO STAB STATION 271, BETWEEN RIB 6 TO RIB 7, 8 INCHES FROM TRAILING EDGE. REPAIRED LEFT ELEVATOR UPPER SKIN IAW A320 SRM 55-21-11 PARA 5D.SDR USAA2011092900007Skin · saturated2S CHECK - WATER INGRESS ON LEFT ELEVATOR UPPER SKIN AT STAB STATION 271, RIB 7, 7 INCHES FROM TRAILING EDGE. REPAIRED LEFT ELEVATOR UPPER SKIN IAW A320 SRM 55-21-11 PARA 5D.SDR USAA2011092900006Skin · saturated2S CHECK - WATER INGRESS ON LEFT ELEVATOR UPPER SKIN BETWEEN STAB STATION 466 TO STAB STATION 527, BETWEEN RIB 11 TO RIB 12, 6 INCHES FROM TRAILING EDGE. REPAIRED LEFT ELEVATOR UPPER SKIN IAW A320 SRM 55-21-11 PARA 5D.SDR USAA2011092900005Skin · saturated2S CHECK - WATER INGRESS ON LEFT ELEVATOR UPPER SKIN BETWEEN STAB STATION 181 TO STAB STATION 227, BETWEEN RIB 5 TO RIB 6, 8 INCHES FROM TRAILING EDGE. REPAIRED LEFT ELEVATOR UPPER SKIN IAW A320 SRM 55-21-11 PARA 5D.SDR USAA2011092900004Skin · saturated2S CHECK - WATER INGRESS ON RIGHT ELEVATOR UPPER SKIN BETWEEN STAB STATION 466 TO STAB STATION 527, BETWEEN RIB 11 TO RIB 12, 5.5 INCHES FROM TRAILING EDGE. REPAIRED RIGHT ELEVATOR UPPER SKIN IAW A320 SRM 55-21-11 PARA 5D.SDR USAA2011092800023Coupling · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON COUPLING AT FR67+16 INCHES, -Y1150. REPLACED COUPLING AT FR67+16 INCHES, -Y1150 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472780.
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