N12221
Service difficulty reports · 93
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 = 'N12221' 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 = 'N12221' 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 CALA2026062517341Adapter · damagedUPPER FUSELAGE STA 385, NR 2 TCAS ANTENNA MOUNTING SURFACE HAS MULTIPLE TOOLING MARKS. REQUIRES EVALUATION. REMOVED AND REPLACED TCAS ANTENNA ADAPTER AT UPPER FUSELAGE IAW DWG: 143A3180 REV V, PL:143A3180 REV J, SRM 51-40-02-0G -0 STEP 4, 51-40-05--0G-0, AMM SDR CALA2026010912831Elec Connector · damagedSTART VALVE ILUMINATED, NR 1 ENGINE. PILOTS REPORT NR 1 ENGINE START VALVE INDICATION SHOWED OPEN AFTER TAKE OFF. ELECTRICAL CONNECTOR PINS & CONTACTS INSPECTED. NO DAMAGE FOUND. MANUALLY ACTUATED START VALVE & OPS OK. SLAVED NEW START VALVE & INDICATION SDR CALA2025111311177Control Unit · faultedSTARTER VALVE OPEN LIGHT ON AT ROTATION. LEFT PACK OFF. 3 ENGINE LIGHTS FLASHED DISCONNECTED CONNECTOR DP1202 AT START VALVE, START VALVE LIGHT STILL ON. DISCONNECTED FIREWALL CONNECTOR D30234 START VALVE STILL ON. REMOVED DEU-1 WITH DEU-2 STILL POWERED START SDR CALA2025102010267Oven · dirtyOVEN SMELLS BAD G2 GALLEY OVEN 205 DEBRIEFED CABIN CREW TO DETERMINE SOURCE OF ODOR IAW AMM 05-51-26. CREW REPORTED ODOR FROM OVEN 205 ONLY. SMELLED OF SPOILED FOOD. NO SMOKE ODOR, ONLY SPOILED FOOD. OVEN WAS NOT USED DURING FLIGHT. CABIN CREW COMPLETED QUESTISDR CALA2025101410071Power Supply · inoperativeFOUND L2 EMERGENCY EXIT LIGHT S INOP. REMOVED AND REPLACED POWER SUPPLY (M1673) REF AMM 33-51-06. OPS CHECK GOOD. OK TO CONTINUE.SDR CALA2025101410070Battery Pack · inoperativeEMERGENCY LIGHTS ROW 22 THRU 27CBA INOP REMOVED AND REPLACED BATTERY PACK (M1670) REF AMM 33-51-06 OPS CHECK GOOD. OK TO CONTINUE. PARTS USED: 99-3351-3-0015,QTY :1SDR CALA2025073007078Warning Light · false activationDESCEND THRU 16000 AFT SERVICE DOOR LIGHT CAME ON. HANDLE NOT SE ATED PER FA. INSPECTED DOOR AREA AND FOUND NO OBVIOUS DAMAGE OR FOD. OPERATED DOOR FORM INSIDE PER AMM 52-41-00-860-803 AND FOUND DOOR WARNING INDICATION TO OPERATE NORMAL. DOOR R2 HAS NO RECENSDR CALA2025062505858Cover · no discrepancyREMOVED R1 SLIDE PACK AND COVER REF AMM 25-66-01 RE-INSTALLED R1 SLIDE PACK AND COVER REF. AMM 25-66-01. INCOMPLETE AMM REFERENCE RE-INSTALLED R1 SLIDE PACK AND COVER REF. AMM 25-66-01-400-803. VERRIFIED TECH INSTALLED R1 SLIDE PACK AND COVER REF. AMM 25-66-01SDR CALA2025060405247Retainer · looseGIRT BAR BRACKET 2R LOOSE ADJUSTED DOOR 2R GIRT BAR RETAINER REFERENCE AMM 25-66-01. OPS CHECK GOOD GIRT BAR HOLDS TIGHT.SDR CALA2025050204422Slide · dislodgedR2 SLIDE PACK FALLING OUT. STOWED DOOR 2 RIGHT GIRT BAR RETAINING FLAP PER MAINTENANCE BULLETIN AND AMM 25-66-01. DOOR SLIDE ARM CHECKED OKSDR CALA2025041503840Slide · misconfiguredDOOR 1R SLIDE POSSBLY NOT PACKED CORRECT. RE-POSITIONED SMALL PORTION OF GIRT MATERIAL BACK INTO ITS PROPER LOCATION ON DOOR 1R PER AMM 25-66-01-400-801.SDR CALA2025040403532Bracket · unknownDOOR 1L SLIDE COVER BRACKET NOT HOLDING TENSION ON GIRT BAR INSPECTED GIRT BAR HOLD BRACKETS. DOOR 1L SLIDE GIRT BAR STOW BRACKETS HOLD GIRT BAR IN PLACE CORRECTLY. OPS CHECK GOOD AT THIS TIMESDR CALA2025022000395Web · cracked(SUPPORT TASK) MAIN LANDING GEAR AFT R/H CUTOUT O/B WEB IS CRACK ED. REPAIRED WEB AT MAIN LANDING GEAR AFT R/H CUTOUT O/B IAW B737-800 SRM 51-70-132R-4. HAECO GSO MECH V900535 INSP QC442. TRANSCRIBED FROM HAECO GSO NRC 9289223.SDR CALA2025022600445Skin · gouged(B757-53-4-1480) MAIN CABIN INTERNAL SURFACE OF THE FUSELAGE SKIN IS GOUGED AT THE CHEM MILL STEP UNDER THE PENETRATION DOUBLER ON THE AFT SIDE OF STA 727E BETWEEN S2R AND S3R. TRANSCRIBED FROM HAECO GSO NRC 9288543 FABRICATED AND INSTALLED REPAIR ER EC/RA 536SDR CALA2025021900382Rib · cracked(B737-5700-3-0633) L/H WING TRAILING EDGE, THE TAB ON THE DEFLECTION FITTING HAS A CRACK INDICATION APPROX WS 278.5. ACCOMPLISHED SRM REPAIR OF L/H WING T/E UPPER TAB ON DEFLECTION CONTROL RIB AT WS 278.5 PER B737-800 SRM 57-51-02-2R-3 REPAIR 3.SDR CALA2025021800375Rib · crackedRIGHT WING T/E DEFECTION CONTROL RIB AFT ATTACH FLANGE IS CRACKED JUST BELOW THE SERRATED PLATE. TRANSCRIBED FROM HAECO GSO NR 9288227 AT R/H WING I/B DEFLECTION CONTROL RIB, REPAIRED AFFECTED AREA IAW BOEING 737-800 SRM 57-51-02-2R-3 AT R/H WING I/E DEFLECTSDR CALA2025020600310Pressure Deck · dented(B737-53-3-0733) FLIGHT DECK FLOOR WEB UPPER SURFACE IS DENTED AND DEFORMED BETWEEN STA 251.6 AND 259.5 BETWEEN LBL15 AND RBL5. TRANSCRIBED FROM HAECO GSO NRC 9288882 INSTALLED REPAIR DOUBLER IAW B737-800 SRM 53-10-51-2R-2. REF HAECO GSO V900519 QC204SDR CALA2025020400283Intercostal · corrodedSUPPORT TASK- MAIN CABIN STA 957 RBL 50 HAS CORROSION ON UPPER SURFACE OF INTERCOSTAL NEAR DRAIN PLUG. TRANSCRIBED FROM HAECO GSO NRC 9288271.SDR CALA2025020200255Web · crackedSUPPORT TASK- MAIN CABIN WEB AT STA 927-947 RBL 60 CRACKED. REMOVED CRACKED WEB AT STA 927-947 RBL40 PER B737-800 SRM 51-40-02. LOCATED AND DRILLED AND INSTALLED NEW WEB PER BAC DWG 147A8501 ID:0039 REV C.SDR CALA2025010600026Floor Support · crackedMAIN CABIN FLOOR SUPPORT INTERCOSTAL UPPER FLANGE IS CRACKED AT APPROX STA 272, LBL26. REMOVED AND REPLACED INTERCOSTAL IAW B737-800 SRM 51-40-02 AND BAC DWG 141A5214.SDR CALA2025022600446Skin · corroded(B737-53-3-0717) STA 540 BL-0 IN THE MIX BAY, THE SKIN HAS EXFOL IATION AT THE SKIN AND FRAME. TRANSCRIBED FROM HAECO GSO NR 9289 015. REPAIRED FUSELAGE SKIN AT STA 540 BL-0 PER ECRA 5351-03150 AND HAECO GSO REO - G25352 REV IR. REF DIP LOG PAGES 3956169 AND 3SDR CALA2025021000320Stringer · corroded(B737-53-3-0712) STA 380-400, STR 25L HAS A BULGE IN THE SKIN. T RANSCRIBED FROM HAECO GSO NR 9289017. REPAIRED STR 25L FROM STA 258 TO 410 & REPLACED FACTORY PLICE AT STA 370 PER B737-800SRM 53-00-03-2R-1 & EC/RA 5310-08504. HAECO GSO MECH V895396 INSP QC442SDR CALA2025021000318Stringer Splice · corroded(B737-5-3-0712) STA 380-400, STR 26L HAS A BULGE IN THE SKIN. TR ANSCRIBED FROM HAECO GSO NR 9289016. REPAIRED STR 26L FROM STA 370 TO 430 & REPLACED OEM FACTORY SPLICE AT STA 370 PER B737-800 SRM 53-00-03-2R-1 & EC/RA 5330-07440. REPAIRED STR 26L FROM STA 370SDR CALA2025020200259Floorbeam · corrodedSUPPORT TASK: MAIN CABIN FLOOR BEAM STA 328 RBL15 HAS CORROSION. TRANSCRIBED FROM HAECO GSO NRC 9288264. REMOVED CORROSION FROM MAIN CABIN FLOOR BEAM STA 328 RBL15 IAW 53-10-51-2R-7. ORIGINAL MATERIAL THICKNESS .125, REMOVED .040, REMAINING .085 FOUND OUSDR CALA2025013000238Floorbeam · corrodedMAIN CABIN STA 987 FLOORBEAM UPPER SURFACE CORRODED AT RBL 16-50. REPAIRED CORRODED FLOORBEAM AT STA 987 FROM RBL 50 TO LBL 50 WITH ANGLES AND STRAPS IAW B737-800 SRM 53-70-51-2R-4.SDR CALA2025012900236Mount · corrodedSUPPORT TASK: MAIN CABIN STA 947 RBL50 AT MOUNT FITTING HAS CORROSION ON UPPER SURFACE. REMOVED CORROSION PER B737-800 SRM 51-10-02. ORIG THICKNESS REMOVED .040, REMAINING .1400 AND ALLOWED MAT LOSS .027 AND FOUND TO BE OUT OF LIMITS PER B737-800 SRM 53-70-5SDR CALA2025011500124Floorbeam · damagedMAIN CABIN STA 1006 LBL6 HAS A DRILL START ON UPPER SURFACE. CUT OUT DAMAGED AREA AT STA 1006 LBL-6 AND REPAIRED WITH 2EA ANG LES,FILLER AND A STRAP IAW SRM 53-00-51-2R-1.SFR # 1038149.SDR CALA2025010300021Crease Beam · corrodedSUPPORT TASK: MAIN CABIN L-1 DOOR CREASE BEAM STA 344 HAS CORROSION. TRANSCRIBED FROM HAECO GSO NRC 9288262. REMOVED AND REPLACED CREASE BEAM P/N 654A0004-1073 P/O 1108011.7 IAW BAC DWG 141A8110 REV.E BLENDED CORROSION IAW B737-800 SRM 5 1-10-02 ORG. 090. RSDR CALA2024030400628Hose · leakingCREW DIVERTED TO ORD DUE TO LOSE OF "A" SYSTEM HYD FLUID DEBRIEFED PILOT, STATING THAT WHEN HYDRAULIC LEVEL REACHED 20%, FLIGHT CREW PERFORMED EMERGENCY CHECKLIST AND SHUT OF PUMP. RESERVOIR IS CURRENTLY AT 17%. LEAK APPEARS TO BE A BURST LINE IN LH MLG WELL. SDR CALA2024020900374Counter · smokeSMOKE CAME FROM NUMBER DIAL ON CAPTS YOKE LASTED A FEW SECONDS D ISSAPATED QUICKLY UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. MAC METER INITIATED FOR WITH VENDOR ID V946822 MAC RELATED WORK ORDER 00000000309665SDR CALA2023062101963Lens · crackedFWD EMERG PLACARD FLT ATTNDT SAYS HAS WRONG PLACARD. R&R EMERGENCY EXIT LIGHT LENS FWD GALLEY REF CONFIG DRAWING 3351DD15945. PARTS USED: 29-3351-3-0070,QTY :1 ACP IDT INSP OF LIGHT LENS INSTALLATION AND OPS CKS OK.SDR CALA2023060201739Skin · missingPDA 1 FOUND 1/2 PANEL 193CL MISSING ON ARRIVAL. THREE PANELS FOUND MISSING. RT SIDE SHOWN FOR COMPARISON CORRECTION: LANDING GEAR PANELS ADDRESSED ON CDL WRITEUP LP 4370202. REMOVED REMAINING UPPER HALF OF PANEL(PICTURED NEXT TO INSTALLED NUTPLATES WERE INSTASDR CALA2021100101752Battery Pack · noneEMERGENCY LIGHT ON OVERHEAD BIN AT 1AB INOP. REMOVED AND REPLACED BATTERY PACK AT M1675 IAW B737NG AMM 33-51-06, OPS CHECK GOOD. SSFR REPORT, FORM 46-0024, ENTERED BY UAL INSPECTION U354653 09/29/2021. DATA WAS TRANSCRIBED FROM NSA EMX N/R 00146, WORK ACCOMPLISDR CALA2021100101749Battery Pack · noneEMERGENCY LIGHT ON OVERHEAD BIN AT 26DEF INOP. REMOVED AND REPLACED BATTERY PACK AT M1671 IAW B737NG AMM V903976. 33-51-6, OPS CHECK GOOD. SSFR REPORT, FORM 46-0024, ENTERED BY UAL INSPECTION U354653, 09/29/2021, DATA WAS TRANSCRIBED FROM NSA EMX N/R 00147, WOSDR CALA2021092201641Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STATION 540 AND LBL 32.40 IS CRACKED REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND LBL 32.40 IAW 737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORIGINAL SEE N SA EMX N/R 00102 AND HANGER N/R 5867172 FOR WORK ACCOMPLISHED SDR CALA2021092201640Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STATION 540 AND 15.04 IS CRACKED REMOVED AND REPLACED CRACKED SHEAR FITTING AT STATION 540 AND RB L 15.04 IAW B737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORIGI NAL SEE NSA EMXX N/R 00105 AND HANGER N/R 5867175 FOR WORK ACCOM SDR CALA2021092201639Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STATION 540 AND LBL 40.87 IS CRACKED REMOVED AND REPLACED CRACKED SHEAR FITTING AT STATION 540 AND LB L 40.87 IAW B737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORIGI NAL SEE NSA EMX N/R 00103 AND HAGER N/R 5867173 FOR WORK ACCOSDR CALA2021092201637Fitting · crackedB737-57-4-1262 - SHEAR FITTING AT STATION 540 AND RBL 32.40 IS CRACKED. REMOVE AND REPLACED SHEAR FITTING AT STATION 540 AND RBL 32.40 I AW B737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORIGINAL SEE N SA EMX N/R 00106 AND HANGER N/R 5867176 FOR WORK ACCOMPLISSDR CALA2021092201636Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STATION 540 AND RBL 6.14 IS CRACKED REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND RBL 6.14 I AW B737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORIGINAL SEE N SA EMX N/R 00104 AND HANGER N/R 5867174 FOR WORK ACCOMPLISHED SDR CALA2021092201633Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STATION 540 AND RBL 54.60 IS CRACKED. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND RBL 54.60 IAW B737-800 SRM AND BAC DWG 111A2000 REV ORIGINAL SEE NSA EMX N /R 00107 AND HANGER N/R 5867177 FOR WORK ACCOMPLISHED CIR C/WSDR CALA2021092201632Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STATION 540 AND LBL 15.04 IS CRACKED. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND LBL 15.04 IAW B737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORIGINAL SEE NSA EMX N/R 00101 AND HANGER N/R 5867171 FOR WORK ACCOMPLISHEDSDR CALA2021092201631Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STATION 540 AND LBL 6.14 IS CRACKED REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND LBL 6.14 I AW B737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORIGINAL SEE N SA EMX N/R 00100 AND HANGER N/R 5867170 FOR WORK ACCOMPLISHED SDR CALA2018081201789Adiru · failedLEFT IRS INOPERATIVE, NO LIGHTS, NO LAT OR LONG, NO GS, IRS BOTH ON RIGHT RESTORES IAW FIM 34-21-00-801-803, REMOVE AND REPLACED LEFT ADIRU IAW 34-21-01-400-801. OPS CHECKED NORMAL. PERFORMED A LAND VERIFY. ALL TESTS PASSED. SATISFACTORY FOR FLIGHT.SDR CALA2018020200445Lens · defectiveEMERGENCY FLOOR PROXIMITY LIGHT DOES NOT TURN ON 28C. REPLACED LENS OPS CHECKS GOOD.SDR CALA2017112104174Window Frame · crackedR1 WINDOW FRAME UPPER OTBD CORNER SHOWS EVIDENCE OF A CRACK, EXTENDING TO THE R2 WINDOW. REPAIRED THE WINDOW FRAME IAW EC/RA5311-01887.SDR CALA2017090102979Stringer · corrodedPULLED RIVET ON RIGHT SIDE OF AIRCRAFT 13 RIVETS AFT OF PRODUCTION JOINT - INGESTION WARNING DECAL- BELOW WATER LINE.WILL MARK WI TH TAPE AND MARKER. BULGING SKIN WITH RIVET POPPING IS LOCATED AT APPROX STA 373 ON STRINGER 25R. SECTION 43. HOLE EDGES CAUSING BSDR CALA2017080802580Battery Pack · dischargedEMERGENCY LIGHTS AT BAG BIN AREA ROW 21,23,25,28 INOP. REMOVED AND REPLACED BATTERY PACK AT LOCATION M1671. OPS CHECK GOOD REF AMM 335106 VERIFIED BATTERY PACK REPLACED AND EMERGENCY PATH LIGHTING OPERATIONAL CHECK REF AMM 33-51-06.SDR CALA2017062301960Lamp · inoperativeRIGHT AFT OVERWING EMERGENCY EXIT INTERIOR FORWARD EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS, OPS CHECKED OKSDR CALA2017062301959Lamp · inoperativeR1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED THE LAMPS, OPS CHECKED OK.SDR CALA2017061201810Slide · damagedL2 DOOR PIN IS STICKING OUT OF THE FLAP THAT CONNECTS TO GIRT BAR . REPLACED THE SLIDE IAW MM 25-66-01-400-801.
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