N14228
Service difficulty reports · 103
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 = 'N14228' 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 = 'N14228' 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 CALA2026092819876Failsafe · crackedBS 663.75 FRAME FITTING AND FAIL SAFE STRAP AT S-18A HAD A VISIBLE CRACK. PERFORMED AN INSPECTION OF RT BS 663.75 REAR SPAR FRAMEASSEMBLY ON AIRCRAFT N14228 IAW PART 2 OF THE LATEST REVISION OF ECRA5340-02286. PART 1 STEP 1 OF ECRA ACCOMPLISHED LP AND WORK CASDR CALA2026090819303Failsafe · corrodedDURING LH FAILSAFE FITTING REPLACEMENT FOUND LH KICK FITTING WITH CORROSION. LH PICKELFORK KICK FITTING WAS REPLACED ON ECRA# 5340-02285 AND EO 260452 STEP 132SDR CALA2026051416264Battery · faultyROW 15-21 RH SIDE EMERGENCY PROXIMITY LIGHTS INOP. REPLACED POWER SUPPLY FUSES. NO HELP. REMOVED AND REPLACED EMERG EXIT BATTERY POWER SUPPLY ELEC REF NUMBER M1694 IAW AMM 33-51-06-960-806 AND SSM 33-51-21-101.1. OPS CK NORMAL. ALL EMERGENCY LIGHTS OPS CK NORMSDR CALA2025121512137Light · no testEMERGENCY LIGHTS - OPERATIONAL CHECK EMERGENCY LIGHTS OPERATIONAL CHECK - ROW 11 FLOOR PROXIMITY LIGHT FOUND INOP REMOVED AND REPLACED FLOOR PROXIMITY LIGHT IAW AMM CH 33-51SDR CALA2025110911024Slide · no discrepancyDUE TO ISAP REPORT OF EXCESS GIRT MATERIAL AND TRIGGER CABLE HANGING OUT FROM BELOW SLIDE PACK. INSPECTED 4 DOOR SLIDES. NO EXCESS GIRT MATERIAL FOUND AND TRIGGER CABLE NO VISIBLE. OK FOR SERVICE.SDR CALA2025110310841Battery Pack · no testOVERWING EMERGENCY SEAT LIGHTS INOP. EMERGENCY LIGHTING SYSTEM OPERATIONAL CHECK. REMOVED AND REPLACED EMERGENCY BATTERY PACK AT ROW 20A OPS CHECK GOOD REF 33-51-06.SDR CALA2025092909394Plunger · corrodedAFT ENTRY LIGHT ILLUMINATED ON CLIMB. FLIGHT CREW REPORTS NO PRESSURIZATION LOSS . INDICATION ONLY. GRD OPERATION 2 DOOR AFT NO DEFECTS NOTED, SPOKE TO CREW HAD NO PRESSURIZATION ISSUE NOTED INSPECTED DOOR AREA NO DEFECTS NOTED, COMPLIED MEL 5203B. INSPECTISDR CALA2025072106751Battery Pack · no testBATTERY PACK M1675 OPERATION TEST FAILED (REF. AAR NR 1000042537 ). REMOVED AND REPLACED EMERGENCY BATTERY PACK M1675 AT LH FWD ENTRY LOWERED CEILING PANEL IAW B737 AMM 33-51-06-960-805 OPS TEST GOOD.SDR CALA2025072206839Skin · damagedPER ECRA 5360-01825 REV C STEP 4, INITIATE DIP FOR PERMANENT REPAIR. ( REF L/P 8387154) "ACCOMPLISH A PERMANENT REPAIR TO THE SECTION 46 SKIN BETWEEN BS 827 & BS 867/ S-25R & S-26R REPAIRED AREA AS PER PART 3 OF THE LATEST REVISION OF ECRA 5360-01825.SDR CALA2025072106748Skin · dentedPERFORM PERMANENT REPAIR AT THE FUSELAGE SKIN. DENT IS LOCATED 11" BELOW THE AFT CARGO DOOR BETWEEN STR24R AND STR25R AT APPROXIMATELY STA830 REF TO LP 8387154 (REF: AAR NR 1000038586) PERMANENT REPAIR ACCOMPLISHED AT FUSELAGE SKIN DENT IS LOCATED 11" BELOW AFSDR CALA2025071406501Battery Pack · no testBATTERY PACK M1695 FAILS OP'S CHECK (REF AAR NR 1000038519). REMOVED AND INSTALLED NEW BATTERY PACK AND OPS TEST IAW B737 AMM 33-51-06-960-805 & AMM 33-51-00710-801 TEST GOOD. BATTERY PACK FAILED FUNCTIONAL CHECK DURING D CHECK IN RFD.SDR CALA2025071406500Skin · dentedREMOVE AND REPLACE THE FWD CARGO DOOR EXTERNAL SKIN DUE TO EXC ESSIVE DENTS DAMAGE .(REF AAR NR 1000038526) FWD CARGO DOOR EXTERNAL SKIN REPLACED IN RFD DURING D CHECK. REMOVED & REPLACED THE FWD CARGO DOOR EXTERNAL SKIN DUE TO EXCES SIVE DENTS DAMAGE. OK TSDR CALA2025071806697Skin · damagedFOUND DAMAGE CREASE AT THE FUSELAGE SKIN BS 807 BTW S27R & 26L. REPAIRED DAMAGE CREASE AT THE FUSELAGE EXTERNAL SKIN STA 807 BTW STRG 27R & STRG 26L IAW EO#250153 REV P1, P2, IR , ECRA 5360-01970.SDR CALA2025071406499Web · corrodedAFTER FURTHER EVALUATION AT THE AFT CARGO DOOR SURROUND STRUCTUR E MAIN SILL WEB FOUND TO BE OUT OF LIMIT REQUIRE REPLACEMENT (RE F. AAR NR 1000042306) ALL DOCUMENTATION AND SUPPORTING DOCUMENTS ON RFD AAR N/R 1000042306. REMOVED & REPLACED THE AFT CARGO LOWSDR CALA2025071406497Skin · dentedREMOVE AND REPLACE THE AFT CARGO DOOR EXTERNAL SKIN DUE TO EXC ESSIVE DENTS DAMAGE. AFT CARGO DOOR RE-SKINNED IN RFD DURING D CHECK DUE TO EXCESSIVE DENTS. REMOVED & REPLACED THE AFT CARGO DOOR EXTERNAL SKI N IAW B737-800 SRM 52-30-01-2R-3. OK TO CLOSE REMSDR CALA2025070806331Angle · corrodedAPU COMPARTMENT LEFT SIDE LOWER TORQUEBOX BEAM ANGLE CORROED ON OUTBOARD SIDE NEAR 2ND FROM AFT NUT PLATE (9"FWD OF AFT BULKHEAD ). REMOVED AND REPLACED APU COMPARTMENT LEF SIDE LOWER TORQUE BOX B EAM ANGLE IAW SRM 51-10-02-0G-0,51-40-02-0G-0, 51-40-05 -0G-0SDR CALA2025070806329Web · corrodedAFTER FURTHER EVALUATION AT THE FWD CARGO DOOR SURROUND STRUCTURE MAIN SILL WEB FOUND TO BE OUT OF LIMIT REQURIE REPLACEMENT (RE F. AAR NR 1000042333) ESFR TRANSACTION COMPLETE REMOVED AND REPLACED THE FWD CARGO DOOR LOWER MAIN SILL BTW STA. 440 TO 500 R/H IAWSDR CALA2025072206838Pressure Web · crackedCENTER WING BOX REAR SPAR VERTICAL PRESSURE WEB HAS CRCK INDICATION BETWEEN RBL 31.83 AND RBL 40 (LENGTH 2") RBL 40- RBL 45. 64 (LENGTH 2" ) (REF AAR NR 1000038 596)REPAIRED DAMAGE CRACK AT THE CENTER WING REAR SPAR VERTICAL PRESSURE WEB BETWEEN RBL 31.83 ANSDR CALA2025072206837Pressure Web · crackedCENTER WING REAR SPAR VERTICAL PRESSURE WEB BETWEEN WL192.0 AND WL 200.6, 01 CRACK BETWEEN LBL 31.83/LBL 40.00 AND 01 CRACK BETWEEN LBL 40.00/LBL 45.64. (REF: AAR NR 1000038583)ESFR CREATED AND SUBMITTED. REPAIRED DAMAGE CRACK AT THE CENTER WING REAR SPAR VERTSDR CALA2025061005426Floorbeam · corrodedPASSENGER CABIN FWD WET AREA FLOOR BEAM STA 344 AND LBL 12 PREVI OUS REPAIR REQUIRE REPLACEMENT (REF. AAR NR 1000038991) REPAIRED CORROSION ON FLOOR BEAM AT STA 344 FROM LBL 43" TO RBL 18.5, IAW SRM 53-10-51-2R-10. THIS IS A CATEGORY A REPAIR, PERMANENT REPAIRSDR CALA2025062605894Stub Frame · crackedCRACK FOUND ON FWD GALLEY DOOR STUB FRAME UPPER LEFT CORNER. REF TO EA5310-07694 REV C OPS 009, STEP, STEP 5 (A) (REF: AAR NR 1000042353) REMOVED AND REPLACED THE R1 DOOR FWD GALLEY DOOR UPPER STUB FRAME IAW B737-800 , SRM 51-40-02-0G-0, IPC 53-11-00-80.SDR CALA2025062605893Floor Support · corrodedPASSENGER CABIN FWD WET AREA INNER CHORD RH SIDE BTW STA 294.5 A ND STA. 328 FOUND TO BE OUT OF LIMTS REQUIRE REPLACE (REF AAR NR 1000038901) PASSENGER CABIN FWD WET AREA INNER CHORD RH SIDE BETWEEN STA 294 .5 AND STA 328 HAS OUT OF LIMITS CORROSION. REMOVED ASDR CALA2025062605892Floor Support · crackedFWD WET AREA LEFT INNER CHORD CRACK BETWEEN STA. 294.5 AND 312. (REF AAR NR 1000038758) ESFR HAS BEEN COMPLIED WITH. REMOVED AND REPLACED FWD WET AREA LH INNER CHORD BTW STA 260 TO STA 360, ALL WORK DONE IAW B737-800, DWG 654A0004-1073, DWG 141A8110, SRM 51-4SDR CALA2025060505297Floorbeam · corrodedAFT WET AREA, PREVIOUS REPAIR WITH CORROSION OUT OF LIMITS ON STA 986.5 LBL 44 AND RBL 43 REQUIRE REPLACEMENT. REPAIRED THE AFT WET AREA FLOORBEAM STA 986.5 IAW B737 -800, SRM 53-70-51-2R-4 REPAIR 4, THIS REPAIR IS A CATEGORY A REPAIR PERMANENT REPAIR.SDR CALA2025060505296Floorbeam · corrodedAFTER REMOVING THE AFT WET AREA FLOOR SUPPORT FOUND CORROSION UNDER THE GALLEY FITTINGS AT STA STA. 947.5 REQUIRE REPAIR BOTH ENDS OF THE FLOOR BEAM. (REF: AAR NR 1000038860) REPAIRED AFT WET AREA FLOOR BEAM STA 947 IAW B737-800, SRM 53-70-51-2R-5. THIS REPAISDR CALA2025060505294Floorbeam · corrodedAFTER REMOVING THE AFT WET AREA FLOOR SUPPORT STABILAZER TO FOM . FOUND CORROSION UNDER THE GALLEY FITTING AT STA 947 LBL52 (REF: AAR NR 1000039742) REPAIRED THE AFT WET AREA FLOOR BEAM STA 947 LBL 52 IAW SRM 53-70-51-2R-5 REPAIR 5, THIS REPAIR IS A CATEGORY ASDR CALA2025062605891Floor Support · corrodedAFT WET AREA, DURING REPAIR PROCESS OF FLOOR SUPPORT 986.5, FOUND C ORROSION ON INNER CHORD STA 887 TO 1016 LBL 45 REQUIRE REPLACE ( REF AAR NR 1000038955) ESFR & SDR DETAILS UPDATED. REMOVED AND REPLACED NEW INNER CHORD ON AFT WET AREA BTW STA 100 6 TO 887 LBSDR CALA2025020702242Door · warning lightFWD ENTRY DOOR LIGHT ILLUMINATED ON TAKEOFF ROLL. REJECTED TAKEO FF. LIGHT EXTINGUISHED ACOMPLISHED FIM 52-10 TASK 815, NO SOFT UNLATCHING , PER FIM STEP D 1 A SUBSEQUENT FLIGHT NO FAULTSSDR CALA2025011301880Lamp · inoperativeL/H OVER WING EMERG DOOR BOTH SIDEWALL LIGHT INOP RELAMPED BOTH WINDOW LIGHT ON L/H OVERWING EMERG DOOR. ALL OPS C HECK NORMAL.SDR CALA2024112601313Slide · looseR1 DOOR SLIDE REPORTED LOOSE PERFORMED VISUAL INSPECTION OF FWD GALLEY SVC DOOR FLOOR MOUNTED ESCAPE SLIDE PAWL, MOUNTED PLATE, GIRT BAR AND RETAINER CLIPS (J-HOOKS)- NO DEFORMATION NOTED AS PER STEP C REF AMM TASK 25-66-01. A/C OK FOR SVC.SDR CALA2024041801128Skin · damagedLIGHTNING STRIKE DAMAGE AT BS 500G 6.5 INCHES ABOVE STR 4R. REPAIRED.SDR CALA2022112503231A/C Pack · odorFUMES IN FLIGHT DECK ON DEPARTURE 2000AGL. NOTHING IN OVENS. REF LOG PAGE 3157817 - PERFORM AMM TASK 05-51-26-800-801-C1 AND REPLACE HEPA RE-CIRCULATION FILTERS. PERFORMED CONDITIONAL INSPECTION, ENGINE RUNS, NO ODOR/SMELLS NOTED. REF AMM 05-51-26. NEED TO RESDR CALA2022100302652Warning Light · false indicationFORWARD ENTRY DOOR LT ON TAKEOFF ROLL...REJECT 80 KNOTS VERIFIED DOOR IS SECURE.PERFORMED OPS CHECK OF FWD ENTRY DOOR. AND DOOR WARNING SYSTEM ADJUSTMENT TEST. FWD ENTRY DOOR OPS CHECKS GOOD NO FAULTS FOUND. COULD NOT DUPLICATE.SDR CALA2021080901286Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STA 540 AND RBL 6.14 IS CRACKED. N/R 6227487 REMOVED AND REPLACED SHEAR FITTING AT STA 540 RBL 6.14 IAW BAC D WG 111A2000 REV ORIGINAL AND B737-800 SRM 51-40-02 DATA TRANSCRI BED FROM NSA EMX NR 00092 AND HANGAR NR 6227487 ACCOMSDR CALA2021080901285Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STA 540 AND LBL 6.14 IS CRACKED. N/R 6227488 REMOVED AND REPLACED SHEAR FITTING AT STA 540 LBL 6.14 IAW BAC D WG 111A2000 REV ORIGINAL AND B737-800 51-40-02 DATA TRANSCRIBED FROM NSA EMX NR 00091 AND HANGAR NR 6227488 ACCOMPLISHSDR CALA2021080901284Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STA 540 AND RBL 32.40 IS CRACKED . N/R 6227485 REMOVED AND REPLACED SHEAR FITTING AT STA 540 RBL 32.40 IAW BAC DWG 111A2000 REV ORIGINAL AND B737-800 SRM 51-40-02 DATA TRANSCR IBED FROM NSA EMX NR 00094 AND HANGAR NR 6227485 ACCSDR CALA2021080901283Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STA 540 AND LBL 40.87 IS CRACKED N/R 6205862 REMOVED AND REPLACED SHEAR FITTING AT STA 540 LBL 40.87 IAW BAC DWG 111A2000 REV ORIGINAL AND B737-800 SRM 51-40-02 DATA TRANSCR IBED FROM NSA EMX NR 00087 AND HANGAR NR 6205862 WORK SDR CALA2021080901282Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STA 540 AND LBL 32.40 IS CRACKED . N/R 6205863 REMOVED AND REPLACED SHEAR FITTING AT STA 540 LBL 32.40 IAW BAC DWG 111A2000 REV ORIGINAL AND B737-800 SRM 51-40-02 DATA TRANSCR IBED FROM NSA EMX NR 00089 AND HANGAR NR 6205863 ACCSDR CALA2021080901291Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STA 540 AND RBL 54.60 IS CRACKED . N/R 6227484 REMOVED AND REPLACED SHEAR FITTING AT STA 540 RBL 54.60 IAW DWG 111A2000 REV ORIGINAL AND B737-800 SRM 51-40-02 DATA TRANSCRIBED FROM NSA EMX NR 00095 AND HANGAR NR 6227484 ACCOMPLISDR CALA2021080901289Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STA 540 AND LBL 15.04 IS CRACKED . N/R 6227489 REMOVED AND REPLACED SHEAR FITTING AT STA 540 LBL 15.04 IAW BAC DWG 111A2000 REV ORIGINAL AND B737-800 SRM 51-40-02 DATA TRANSCR IBED FROM NSA EMX NR 00090 AND HANGAR NR 6227489 ACCSDR CALA2021080901287Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STA 540 AND RBL 15.04 IS CRACKED . N/R 6227486 REMOVED AND REPLACED SHEAR FITTING AT STA 540 RBL 15.04 IAW BAC 111A2000 REV ORIGINAL AND B737-800 SRM 51-40-02 DATA TRANSCRIBED FROM NSA EMX NR 00093 AND HANGAR NR 6227486 ACCOMPLISDR CALA2021030500260Hose · damagedENG DRIVEN HYD PUMP1 LOW PRESSURE LGT QUANTITY 0 FOUND LEAKING HYDRAULIC HOSE ON RIGHT MAIN LANDING GEAR DOWNLOCK ASSEMBLY REF IPC 32-32-51-02 ITEM #5. REMOVED AND REPLACED HOSE IAW AMM 20-10-52. PERFORMED GEAR SWING IAW AMM 32-32-00-701-801. ALSO PERFORMED SDR CALA2020100901173Control Valve · inoperativeAFTER T/O RT DUCT PRESS 15PSI LT DUCT 45PSI FLIGHT CREW REPORTS DUCT PRESSURES NOW EVENLY MATCHED AT 45 PSI AT CRZ ALT. FOUND RT ENGINE PRECOOLER VALVE TO FAIL PNEUMATIC HEALTH TEST. REPLACED PRECOOLER CONTROL VALVE, REF AMM 36-12-02-400-801. ADD EMP:094388SDR CALA2020021600434Warning Message · false activationPACK LIGHT LIGHT ON DURING CLIMB, LIGHT COMES ON AGAIN AFTER RES ET LEFT ACFT RETURNED TO GATE WITH NO FAULT LIGHTS ILLUMINATED ON THE 6 PACK OR OVERHEAD AIRCOND PANEL. ALSO PERFORMED A BITE TEST ON BOTH PACK/ZONE CONT''S. NO FAULTS. IN ADDITION, RAN L&R PACKSSDR CALA2019121902237Motor · failedSTABILIZER FAILS TO TRIM NOSE UP AND NOSE DOWN ELEC STAB TRIM FAIL BOTH CAPT/FO BOTH DIRECTIONS. CB CHECKS NORM AL CREW REPORTS APU OVERSPED DURING DEICING. AUTO PILOT DID NOT WORK, MANUAL TRIM OK. FOUND POWER GOOD TO THE MOTOR. REPLACED STAB TRIM MOTOR IAW MMSDR CALA2019112862086Compensator · inoperativeAC BURNED RUBSTANIALLY MORE FUEL ENROUTE TO BE ABLE TO COTINUE T O DESTINATION REMOVED AND REPLACED BOTH LEFT AND RIGHT MAIN TANK COMPENSATORS. REFERENCE LOG PAGES 3888465 & 3888457. REF. LOG PAGE 3889649, REPLACED RT TANK PROBES 2,3,7,8,9, AND 10. OPS CHECKSDR CALA2019072901265Angle · corrodedCORROSION AT NUTPLATE HOLE ANGLE (MARKED) ON LT SIDE OF APU COMPARTMENT APPROX. STA. 1136. TRANSFERRED FROM FLEET CYCLE N/R 9681448 FOR DIP REPORTING. REF. ECRA 5311-02209. BEFORE THE AIRCRAFT REACHING 75,000 TOTAL FLIGHT CYCLES. PLANNING TO CONTACT ENGINERRINSDR CALA2019072401232Rib · crackedRT HORIZONTAL STAB LOWER SKIN AT ST 92.70 REQUIRES ACCESS HOLES FOR IN-SPAR RIB CRACKS.(NR# 9677013,9677014,9677015,967701 6 FOR RIB CRACKS). REPAIR AS PER SRM 55-10-01 REPAIR 11.INITIATE DIP TO INSPECT EXTERNAL DOUBLER AT 56K TOTAL COMPONENT FLIGHT CYCLES WITSDR CALA2018012100274Battery Pack · inoperativeFWD ENTRY AND 1ST CLASS EMERGENCY LIGHTS INOPERATIVE. R & R THE BATTERY PACKS IAW AMM 33-51-06.SDR CALA2017110303921Light · inoperativeEMERGENCY EXIT SIGN DOES NOT TURN ON. 20F RELAMPED. CHK'S GOOD. OK TO CONT.
Back to N14228