N14235
Service difficulty reports · 121
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 = 'N14235' 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 = 'N14235' 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 CALA2026062517322Oven · odorOVEN 204 EMITTS ACRID ELETRICAL SMELL WHEN HEATED. NO SMOKE OR FIRE. FOUND BURNED FOOD RESIDUE ON INSIDE OF OVEN DOOR. CLEANED AFFECTED AREA ON OVEN DOOR. OPS CHECKED OVEN AT 350 DEGREES FOR 20 MIN. NO BURN SMELL OR ODOR. ACFT OK FOR SERVICE.SDR CALA2026060416826Skin · crackedLEFT WING LOWER SKIN AT S9, DURING HFEC INSPECTION CRACK WAS FOUND AT OTBD MOST FASTENER. PERFORMED PERMANENT REPAIR ON LH WING LOWER SKIN AT S-9 IAW EA 5725-01143 REV A.SDR CALA2026010512657Skin · dentedDAMAGE FROM BAGGAGE CART AT FWD CARGO DOOR. BS 440+7 - 440+13.7, S20R-2 - S20R+2.4. DENT IS WITHIN LIMITS IAW SRM 52-30-01-1A-1 SEC 4, PARA B, SUBSECTION (4) FIG 103, ALLOWABLE DAMAGE 1, DETAIL F. DENT IS 7.00 INCHES LONG, 4.250 WIDE, .320 DEEP. NO CRACKS SDR CALA2026010512656Skin · damagedDAMAGE FROM BAGGAGE CART AT RT SIDE OF FUSELAGE. BS 344-2 - 360+3, S20R-1 - S20R+10.5. MEASUREMENTS: HEIGHT: 7.3" WIDTH: 20.75" DEPTH: 0.24". INSPECTED AREA, THE DAMAGE BS 344 -360, S20R - S21R. STR 20R APPEARS TO BE BENT, CAUSING THE ATTACHING CLIPS ON BOTHSDR CALA2026010512655Stringer · bentWHILE INSPECTING EXTERNAL FUSELAGE SKIN DAMAGE FROM STA 344 TO STA 360, FOUND STRINGER 20R BENT FROM STA 344 TO STA 360. REPAIRED STRINGER 20R FROM STA 344 TO STA 360 AS PER SRM 53-00-03-2R-1 TYPE 1 STRINGER, WITH THE DEVIATIONS PROVED IN EC/RA 5310-08761 ANDSDR CALA2025111911348Unknown · odorDUR FLT FAINT SMOKE SMELL BTW ROWS 12-21 AIRCRAFT LEFT. SMELL DISSIPATED AFTR 5 MINS FLIGHT AND CABIN CREW COMPLETED FORM 46-6020. DEBRIEFED FLIGHT AND CABIN CREW ON ASSOCATED SMOKE/ODOR IN CABIN. INSPECTED AREAS SUSECTED TO CAUSE CONCERN REF AMM TASK 05-51-SDR CALA2025111111130Girt Bar · no discrepancyFA REPORTS LEFT GIRT BAR CLIP ON DOOR 1R LOOSE. INSPECTED BOTH J HOOKS FOR GIRT BAR ON 1R, J HOOKS ARE SECURED, NO DEFECTS NOTED. REF AMM TASK 25-66-01- 200-802.SDR CALA2025090908674Contact · shortedGATE RETURN, WHEN SETTING TAKE OFF PWR ADIRU LIGHTS ILLUMINATED , MCP FLICKERED FOLLOWED WITH NUMEROUS WARNING LIGHTS ILLUMINATED ON THE OVERHEAD PANEL. TOMC ADVISED GATE RETURN MCP ALL LIGHTS ON. ALSO NUMBERS FLASHING 8 ON DISPLAY WINDOWS. FIRE PANEL SHOWING SDR CALA2025090108318Pcb · not reportedSEVERAL ANNUNCIATIONS ON OVHD PANEL CENTER INSTRUMENT PANEL AND MCP. WOULD REF WDM 31-52-75 AND IF NO FAULTS. REPLACE R33/R34 AS A PRECAUTION. GND TESTED OK AFTER ARRIVAL, REPLACED R33, MASTER TEST RELAY, AND R34, MASTER DIM RELAY. PERFORMED OP TESTED OK ISDR CALA2025081107559Skin · crackedRIGHT WING NR 8 SLAT LOWER SURFACE AT ACTUATOR ATTACH POINT CRACKED. ACCOMPLISHED PERMANENT REPAIR AT SLAT NR 8 NOSE SKIN LOWER SURFACE IAW SRM 57-42-01-2R-8 FIGURE 202 ALTERNATIVE 1. NO FURTHER ACTION REQUIRED.SDR CALA2025081407755Window Frame · crackedEA 5310-08195 REV B CRACK FOUND AT LH SIDE NUMBER 3 WINDOW FRAME POST 4TH HOLE FROM THE BOTTOM. ACCOMPLISHED ON THE LT NR 3 WINDOW POST FRAME E-F IAW ECRA 5310-08666 PART 1. AFTER 49900 TOTAL AIRCRAFT FLIGHT CYCLES (FC), BUT BEFORE 50000FC PERFORM AN INSPSDR CALA2025081407746Spar · corrodedLEFT WING L/E TO FRONT SPAR APPROXIMATELY RIB 26 HAS CORROSION. ACCOMPLISHED INTERIM REPAIR CATEGORY B AT LEFT WING FRONT SPAR LOWER CHORD BETWEEN OFSS 700 AND OFSS 710 AS PER EC/RA 5720-03555 PART 1 PARAGRAPH 1.SDR CALA2025080607383Floorbeam · corrodedFOWARD WET AREA STA.294.5 RBL 10" FLOORBEAM STRUCTURE HAS CORROSION. ACCOMPLISHED ESFR FORM AS PER UAL GMM 04-20-05.REMOVED AND REPLACED UPPER T-CHORD AT FLOORBEAM STA 294.5 BETWEEN LBL 35 TO RBL 57 REF SRM 53-10-51-2R-16 AND SRM 51-40-02-0G-0 PARAGRAPH 4 ANSDR CALA2025080507321Floorbeam · corrodedFORWARD WET AREA BS 328, RBL 46, FLOORBEAM HAS CORROSION. REMOVED AND REPLACED FLOORBEAM SECTION BS 328 BETWEEN RBL 0 AND RBL 56 IAW SRM 53-10 51-2R-7 AND SRM SRM 51-40-02-0G-0 PARAGRAPH 7.D.SDR CALA2025080807489Structure · corrodedAFT WET AREA. EXFOLIATION CORROSION ON SEVERAL SPOTS OF RT INNER CHORD BETWEEN BS 947.5 -1006. REMOVED AND REPLACED INNER CHORD AT RT AFT WET AREA BETWEEN STA 890 TO STA 1006 PER SRM 51-40-02-0G-0, 51-40-03-0G-0 AND DWGS 147A8501, 147A0004.SDR CALA2025080407232Stringer · corrodedCORROSION FOUND AT AREA AFT OF AFT CARGO COMPT S-21R BETWEEN STA 967-986.5. ACCOMPLISHED CATEGORY A REPAIR AT STRINGER S-21R BETWEEN STA 967 AND 986.5 AS PER SRM 53-70-03-2R-1 AND SRM 53-00-03-2R-1 FIGURE 201 FOR DAMAGE ON STRINGER FREE FLANGE. NO FURTHER ACTSDR CALA2025080107208Floorbeam · corrodedAFT WET AREA. EXFOLIATION CORROSION AT SEVERAL SPOTS ON FLOOR BEAM UPPER SURFACE BS 986.5 RBL7 TROUGHT RBL47. REMOVED AND REPLACED EXISTING REPAIR T - CHORD AT STA 986.5 RBL 8 TO RBL 50 REF SRM 53-70-51-2R-4 AND SRM 51-40-02-0G-0.SDR CALA2025073007076Battery Pack · no testSEVERAL EMERGENCY LIGHTS INOP. (REF AAR N/R 9986389) REMOVED & REPLACED BATTERY PACKS AT POSITIONS M1672 & M1673 AS PER AMM 33-51-06-02. PERFORMED INSTALLATION TEST AS PER B737 AMM 33-51-06-02 (SUBTASK 33-51-06-710-004). TEST FOUND NORMAL, NO DEFECTS NOTED. RESDR CALA2025072806978Angle · corrodedCORROSION APU BAY. AFT BULKHEAD. LOWER ANGLE FOR SEAL RETAINER, DOT 260 001 FOR REF N/R 9985897 REMOVED AND REPLACED CORROSION APU BAY. AFT BULKHEAD. LOWER ANGLE FOR SEAL RETAINER, DOT 260 001. AFT BULKHEAD. LOWER ANGLE FOUND EXFOLIATION OUT OF LIMITIS. REMOVSDR CALA2025072806977Waste Tank · corrodedAFT CARGO WASTE TANK COMP CORROSION AT DUMP CHUTE BASE BETWEEN S STA 847-867 REMOVED AND REPLACED WASTE TANK DRAIN NEW PAN ASSY AT AFT CARGO WASTE TANK AT DUMP CHUTE BASE BETWEEN STA 847-867 IN REF SRM 51-40-02-0G-0 AND DWG 146A7401 ESFR TRANSACTION COMPLETEDSDR CALA2025063006074Skin · crackedCRACK FOUND AT LOWER SKIN OF RIGHT HORIZONTAL STABILIZER AT STAB STA 92.70, 12" FROM REAR SPAR, I/B ROW. CRACK LENGTH : 0.468". REPAIRED CRACK FOUND AT LOWER SKIN OF RIGHT HORIZONTAL STABILIZER AT STAB STA 92.70, 12" FROM REAR SPAR, I/B ROW. IN REF SRM 55-10-SDR CALA2025032603194Handle · no discrepancyCOCKPIT EMERGENCY ESCAPE HANDLE OUTSIDE NOT FLUSH. CREW STOWED HANDLE. FOUND HANDLE FLUSH CREW STOWED HANDLE. FOUND HANDLE FLUSH.SDR CALA2025013002134Hook And Loop · worn20F EXIT ROW VELCROW COMING NEEDS REPLACING FOUND DEBRIS IN OVERWING EXIT LIFT STRAP COVER VELCRO, CLEANED DEBRIS AND RESECURED COVER IN REF AMM 52-22-00SDR CALA2024062400062Skin · damagedRAMP REPORT DURING CARGO REMOVAL DOOR WAS SCRATCHED FWD CARGO DOOR. SCRATCH MEASURED 5.5" VERTICALLY, BLENDED TO A SMOOTH CONTOUR REF SRM 52-30-01-1A-1. REQUEST HFEC INSP OF REWORKED AREA FOR CRACKS AND CHECK REMAINING THICKNESS. PERFORMED HFEC. NO CRACKS IASDR CALA2024053101659Toilet · leakingAFT LAV AREA CARPET SOAKED POSSIBLE LAV LEAK REQUEST MEL FOR LAVATORY " E " AS UNUSABLE COMPLIED WITH DDP PLACED LAVATORY "E" ON MEL AS INOP DO NOT USE , COMPLIED WITH DDP . R&R LAV E REF AMM 38-32-01 OPS CHECK GOOD NO LEAKS.SDR CALA2024052201557Vent · crackedWASTE TANK FUSELAGE VENT EXHIBITS CRACKS AND CORROSION EXTERNALLY ON EXTERIOR SKIN AFT OF STATION # 907 SECTION # 47 REMOVED WASTE TANK ENCLOUSER PANELS. REF AMM 25-52-20. REMOVED POTABLE WATER TANK. REF AMM 38-11-01-00-801. REPAIR DAMAGED AREA PER SRM 53-70-0SDR CALA2024040300958Landing Gear · unknownNOSE GEAR CAME DOWN WITH GEAR LEVER IN OFF POSITION DURING AFTER TAKEOFF PROCEDURE RIGGING, COULD NOT DUPLICATE THE ISSUE LIKE MIDNIGHTS DID. RECONNECTED LG DOORS AND CYCLED GEAR SEVERAL MORE TIMES WITH NO ISSUES. VERIFIED CABLE RIG TENSION ONLY.RII 09-25-05 SDR CALA2024040300957Landing Gear · unknownNOSE GEAR CAME DOWN WITH GEAR LEVER IN OFF POSITION DURING AFTER TAKEOFF PROCEDURE RIGGING, COULD NOT DUPLICATE THE ISSUE LIKE MIDNIGHTS DID. RECONNECTED LG DOORS AND CYCLED GEAR SEVERAL MORE TIMES WITH NO ISSUES. VERIFIED CABLE RIG TENSION ONLY.RII 09-25-05 SDR CALA2023092702878Uplock Sensor · wornRIGHT GEAR RED LIGHT GEAR HANDLE UP RAN CHECKLIST EVENTUALLY G OT 3 DOWN AND LOCK PER CREW ON GEAR RETRACTION GOT RED RIGHT GEAR LIGHT ONLY. WITH THEGEAR LEVER IN THE OFF POSITION THEY GOT BOTH THE RED AND GREEN RIGHT GEAR LIGHT. PERFORMED MANUAL EXTENSION SAMSDR CALA2023012500201Light · damagedSEAT MOUNTED EMERGENCY EXIT LIGHT AT ROW 34ABC DAMAGED. REMOVED AND REPLACED WHITE LIGHT ASSY REF MM 33-51-11. OPS CK OK. PARTS USED: BR9644-11,QTY :1 VERIFIED IDT REQUIREMENTS AND PROPER OPERATION OF LIGHTSDR CALA2022120803334Structure · crackedAFTER EVALUATING DMG ROUTINE CARD AT AFT CARGO DOOR FWD LOWER CO RNER FOUND POSSIBLE CRACK (REF: AAR NR 99952238) PLACED ON DIP PER TABLE 202 INSPECTION AT 22,500 FC AND REPEAT INSPECTIONS AT INTERVALS OF 1,400 FC ON CATEGORY B REPAIR. WORK ACCOMPLISHED ON AARSDR CALA2022081602083Circuit Breaker · not seatedPSEU ILLUMINATED UPON RECALL PERFORMED BITE TEST OF PSEU AND FOUND FAULTS: 31-52105, 31-52111, 32-64004, ALSO FOUND MAINTENANCE MESSAGE ON FSEU 27-53279. FOUND CIRCUIT BREAKER A12 ON P6-2 OPEN. RESET C/B A12. OPERATED FLAPS AND SLATS THRU SEVERAL CYCLES NO FASDR CALA2022061301496Axle · departedPDA 1 ON TAXI OUT, LEFT NLG WHEEL AND AXLE DEPARTED AIRCRAFT. COMPLETED REMOVAL OF THE NOSE LANDING GEAR FOR REPLACEMENT. REF INSTALLED BOTH NOSE LANDING GEAR WHEELS ON THE NLG REF AMM AMM 32-21-00-000-801. 32-45-21, WHEELS NOT SAFETIED, AWAITING NEW WHEEL WASSDR CALA2022032100714Frame · crackedF/O''S UPPER OUTBOURD CORNER WINDOW FRAME IS CRACKED. LOCK FOR MX FERRY PHOTO ADDED RAMS REQUITED LOGPAGE UNLOCKED FOR UPDATE COMPLETED STEPS B1&2 OF AVO9568 REF NDT PART 6 51-00-01. CORRECTION: COMPLETED STEPS B3 & B4 OF AVO9568 REF NDT PART 6 INSPECTION EVALSDR CALA2021061400867Proximity Sensor · inoperative*DECLARED EMERGENCY* LE FLAP TRANSIT LITE T/S REF FIM 27-51-801 FOUND LEADING EDGE FLAP EXTEND PROX SENSOR BAD F2 R&R PROX SENSOR REF MM 27-88-11-400-802 OPS NORMALSDR CALA2020032700737Wire · brokenWING-BODY OVERHEAT LIGHT LIGHT ON THIS IS A REPEAT WRITEUP BITE ON WING BODY OVERHEAT CTL. SHOWED CODE 44, AFT CARGO OVERHEAT ALARM. PERFORMED CONTINUITY CHECK OF CARGO BIN LOOPS WAS BAD PER TABLE 301 FIM TASK 26-18-00 P 301. NEED TO ISOLATE WHICH LOOP IS BAD SDR CALA2019102981839Bulkhead Web · canningREF EA 5310-04639 REV E OP002 AFT BULKHEAD WEB EVVIDENCE OF OIL CAN CONDITION AT BS1016 S-13R WL232.5 IN I/B SIDE FROM OUTER PERIMETER L-2.0 W-1.218 AND D-0.020 ACCOMPLISHED REPAIR AT APB WEB BS1016, S13R WL232.5 14IN FROM OUTER PERMITER I.A.W RES-WI NO.201518SDR CALA2019102981838Bulkhead · corrodedCORROSION FOUND AT LT W/W AFT BULKHEAD AREA AT STA 727 ADJECENT TO ELECTRICAL FEED THRU SUPPORT NEAR ENGINE FIRE BOTTLES REF AAR N/R 99848687 ACCOMPLISHED LT WHEEL WELL STA 727 WEB REAPIR PER AAR RES 2015189-46 REV IR AND UNITED ECRA 5311-02284 ADD EMP:V891438SDR CALA2019102501814Rib · crackedL/H HORIZONTAL STAB NO.1 RIB HAS CRACKS ON THE LOWER SIDE OF EACH STIFFENER (4 EACH) (REF N/R 99848214) REPAIRED L/H HORIZONTAL STAB NO.1 RIB AT VERTICAL STIFFENER NO.1 AS PER REF B737-800 SRM 55-10-09 FIG 02 REPAIR 4.SDR CALA2019102981834Bulkhead Web · crackedUPPER VAPOR BARRIER APPEARS TO BE CRACKED APPROX 3IN LONG NEAR B SYS HYD RESERVOIR IN RIGHT WHEEL WELL. NEED TO VERIFY UPPER VAPOR BARRIER IS CRACKED PER NDTINSP CW NDT PART 6, REF 51-00-00-23, NOTED A 2.5 INCH CRACK IN RIGHT WW AREA VAPOR BARRIER. E/WIZ HAS BSDR CALA2019102501809Floor Support · corrodedLEFT SIDE FLOOR SUPPORT ANGLE IS CORRODED BETWEEN 927-993 JUST INBOARD OF L2 DOOR. (REF NR 99847955) REMOVED AND REPLACED FLOOR SUPPORT ANGLE "CREASE BEAM CHORD" AT MAIN CABIN L2 DOOR JUST INBOARD REF B737-800 SRM 51-40-02.SDR CALA2019102501805Web · corrodedFWD CARGO COMPT DOOR CUTOUT LOWER SILL WEB CORRORED (REF NR 99847849) REMOVED AND REPLACED LOWER SILL WEB AT FWD CARGO COMPT DOOR IAW B737-800 SRM 51-40-02 AND DWG 143A8330.SDR CALA2019102501804Rib · crackedIN REF TO EA 5510-01843 REV G OP 002 L/H HORIZ. STAB IN-SPAR RIB STA 92.70 VERTICAL STIFFENER NO.4 CRACKS AT LWR TRANSITION RADIUS MKD. (REF N/R 99848208) REPAIRED L/H HORIZONTAL STAB IN-SPAR RIB STA 92.70 VERTICAL STIFFENER NO.4 AS PER REF B737 SRM 55-10-09 FSDR CALA2019102501803Rib · crackedREF TO EA 5510-01843 REV G OP 02 L/H HORIZ. STAB INSPAR RIB STA 92.70 VERTICAL STIFFENER NO.3 CRACKS AT LWR TRANSITION RADIUS MKD (REF N/R 99848207) REPAIRED L/H HORIZONTAL STAB INSPAR RIB STA 92.70 VERTICAL STIFFENER NO.3 AS PER REF B737-8 SRM 55-10-09 FIG 20SDR CALA2019102501802Rib · crackedREF TO EA 5510-01843 REV G OP 02. L/H HORIZ. STAB. INSPAR RIB STA 92.70 VERTICAL STIFFENER NO.2 CRACKS AT LWR TRANSITION RADIUS MKD (REF N/R 99848206) REPAIRED L/H HORIZONTAL STAB INSPAR RIB STA 92.70 VERTICAL STIFFENER NO.2 AS PER REF B737-800 SRM 55-10-09 FISDR CALA2019102501801Stringer · corrodedFOUND CORROSION AT AFT WET AREA, STRINGER 22R BETWEEN STA 1006 AND STA 1016 CLOSER TO STA 1016 JUST AT THE END OF THE FITTING BELOW FLOOR WEB AREA. (REF NR 99848703) INSTALLED REPAIR PARTS AT AFT WET AREA STRINGER 22R BETWEEN STA 986.5 TO STA 1016 IAW B737-800SDR CALA2019102311789Skin · corrodedAFT CARGO COMPT DOOR INTERNAL T/E WEB SKIN HAS 1EA SPOT EXFOLIATION CORROSION AND 3EA SPOTS SURFACE CORROSION REF AAR N/R99847994 REMOVED AND REPLACED INNER SKIN AT AFT CARGO COMPT DOOR REF B737 SRM 51-40-02 AND DWG 146A6110.SDR CALA2019102311785Fitting · crackedCENTER WING FUEL TANK UPPER R/H SURFACE AT STATION 540 HAS I/B BRACKET AFT END CRACKED REF AAR N/R 99848702 REMOVED AND REPLACED NEW BRACKET AT CENTER WING FUEL TANK UPPER R/H SURFACE STATION 540I/B REF B737 SRM 51-40-02 DWG 111A2000 AND AMM 51-31-00SDR CALA2019102311784Angle · crackedMAIN FLOOR SUPPORT ANGLE APPEARS CRACKED AT FASTNER HEAD AT RBL55 STA 616 REF AAR N/R 99848350 INSTALLED REPAIR AT R/H MAIN FLOOR INNER CHORD STA 616 HOLE FASTNER FROM STA 601-639 RBL 55 AS PER RES WI2015189-51 AND ECRA 5315-01134.SDR CALA2019102311783Floorbeam · corrodedFLOOR SUPPORT CROSSBEAM AT 987 HAS CORROSION AT NUT PLATE 47IN RIGHT OF CENTER LINE REF AAR N/R 99847940 FLOOR SUPPORT CROSSBEAM AT 987 STA RBL 7.98 TO RBL 50 REPAIRED IN REF B737 SRM 53-70-51 REPAIR 4 REPAIR ALYERNATIVE 2 FIG 205 FROM PAGE 214 TO PAGE 229 ADD
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