N17233
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 = 'N17233' 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 = 'N17233' 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 CALA2026080918418Coffeemaker · faultedAT CRUISE AFT FA OBSERVED SMOKE COMING FROM COFFEE POT 419. FA PULLED CBS AND SMOKE SUBSIDED. NE EMERGENCY ACTIONS TAKEN. ATTENDING FA COMPLETED SMOKE AND ODOR REPORT. CONFIRMED SMOKE EMANATING FROM COFFEMAKER 419 WITH CORRESPONDING ELECTRICAL ODOR. REF LP 9SDR CALA2026072918094Coupling · detachedREMOVED FORWARD CARGO COMPARTMENT AFT BULKHEAD LINER PANELS. FOUND WASTE LINE CLAMP COUPLING OFF OF THE LINE BEHIND FORWARD CARGO COMPARTMENT AFT BULKHEAD LINER PANEL BHD 500I. LINE IS LOCATED ABOVE LH RECIRCULATION FILTER. IMAGES SHOW EXACT LOCATION WHERE CLASDR CALA2026060816901Bulb · burned outEMERGENCY LIGHTS - OPERATIONAL CHECK EMERGENCY LIGHTS OPERATIONAL CHECK - EMERGENCY EXIT SIGN AT DOOR 2L HAS BULBS BURNT OUT RELAMPED REF AMM 33-51-01-960-801. BOTTOM BULB STILL INOP AFTER MULTIPLE RELAMPS. SUSPECT BAD ASSY. REPLACED EXIT ASSY REF AMM 33-51-01SDR CALA2026052916652Lamp · inoperativeEXTERIOR EMERGENCY LIGHT AFT OF L2 DOOR IS INOPERATIVE. REPLACED THE LAMPS IAW AMM 33-51-04-960-801.SDR CALA2025120711818Unknown · odorFAS REPORTED SMOKE ODOR NEAR 1ST CLASS WALL. COMPLETED CONDITIONAL INSPECTION FOR SMOKE ODOR IN 1ST CLASS AREA IAW AMM 05-51-26-800-801-C1, NO FAULT NOTED.SDR CALA2025112111402Processor · faultedREPEAT ISSUE, RT TANK QTY STUCK AT 6.93 FOR 30 MINS IN CRUISE & THEN RAPIDLY DECREASED. PERFORMED BITE TEST OF THE FQIS, TESTED GOOD, AS A PRECAUTION, REMOVED AND REPLACED WITH A NEW FUEL QUANTITY PROCESSOR UNIT IAW TASK 28-41-81-000-801, AND TASK 28-41-81-4SDR CALA2025111211149Light · inoperativeSEAT ROW 11 LT EMERGENCY ESCAPE LIGHT INOPERATIVE. REMOVED AND REPLACED THE LIGHT ASSEMBLY AT SEAT ROW 11, OPS CHECKS GOOD IAW AMM 33-51-11-960-802.SDR CALA2025110610977Skin · crackedCRACK INDICATION AT THE MOST OTBD FASTENER HOLE AT STR 9 ON THE RT WING LOWER SKIN APPROX .75" IN LENGTH AT THE 6 O'CLOCK POSITION LOOKING AFT. REPAIRED RT WING LOWER SKIN IAW REO G25610, REV IR, AND EC/RA 5720-03575. MAJOR REPAIR.SDR CALA2025110610962Power Supply · no testBATTERY PACK FAILED FUNCTIONAL CHECK, REMOVED AND REPLACED THE M1675 BATTERY PACK AND POWER SUPPLY IAW AMM 33-51-06.SDR CALA2025102710572Frame · corrodedFWD WET AREA RT, BS 328 RBL 27-53, FRAME HAS CORROSION AT FASTENER HOLES. REMOVED DAMAGE, FABRICATED, LOCATED, DRILLED REPAIR PARTS, HFEC AREA, NO CRACKS NOTED. INSTALLED REPAIR AND RESTORED COATING IAW SRM 53-10-51-2R-7, FIG 205, REPAIR 7, AND ECRA 5315-01SDR CALA2025101710222Crease Beam · corrodedFWD WET AREA RT, R1 DOOR CREASE BEAM BS 270-340 HAS CORROSION ON TOP AND SIDE OF ANGLE. REMOVED AND REPLACED CREASE BEAM AT R1 DOOR IAW SRM 51-40-02 AND DWG 141A8310 REV -.SDR CALA2025102610536Floorbeam · corrodedB737-53-3-0737 MAIN CABIN AFT WET AREA R/H STA 987 RBL43 FRAME HAS CORROSION MARKED. REMOVED DAMAGE ONLY .150 MATERIAL LOSS .040 REMAINING .110 FOUND TO BE OUT OF LIMITS REF SRM 53-70-51-1A-1 FLOORBEAM REPAIRED.SDR CALA2025102610534Floorbeam · corrodedMAIN CABIN AFT WET AREA R/H STA 947 O/B LAV MOUNT, FRAME HAS CORROSION MARKED. REMOVED DAMAGE,HFEC NO DEFECTS NOTE,FABRICATED,LOCATED DRILLED, INSTALLED,AND RESTORED ,COUTINGS REF B737-800 SRM 53-70-51-2R-5 THIS IS A CAT A REPAIR NO FURTHER ACTION REQUIRED.SDR CALA2025102610532Crease Beam · corrodedB737-53-3-0737 MAIN CABIN AFT WET AREA R/H AT R2 DOOR, CREASE BEAM HAS MULTI SPOTS OF CORROSION. REMOVED AND REPLACED MAIN CABIN AFT WET AREA R/H CREASE BEAM AT R2 DOOR IAW B737-800 SRM 51-40-02 & BAC DWG 147A8501 REV:B.SDR CALA2025101710218Frame · corrodedMAIN CABIN AFT WET AREA LT BS 987 LBL43, FRAME HAS CORROSION. REMOVED DAMAGE, HFEC NO DEFECTS NOTED, FABRICATED, LOCATED, DRILLED, INSTALLED REPAIR, AND RESTORED COATINGS REF SRM 53-70-51-2R-4, THIS IS A CAT A REPAIR. NO FURTHER ACTION REQUIRED.SDR CALA2025100909846Beam · crackedFWD CARGO DOOR UPPER BEAM -A- CRACKED UNDER EXISTING SKIN DOUBLER. REMOVED AND REPLACED -7 BEAM IAW 14A6117 REV A, CMM 2-31-15, SRM 51-40-02, AND DWG 143A6117.SDR CALA2025100909843Skin · crackedFORWARD CARGO DOOR SKIN REPLACED. REMOVED AND REPLACED OUTER SKIN IAW B737-800 SRM 52-30-01-2R-3 REP.3, CMM 52-31-15 AND BAC DWG 143A6110 REV D.SDR CALA2025101309944Seat Track · corrodedMAIN CABIN AFT WET AREA RT BS 890 RBL44, SEAT TRACK HAS CORROSION AT FASTENER HOLE. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-40-02 AND NAT DWG 10N00633 REV-.SDR CALA2025102610516Skin · damagedDURING AAI INSPECTION NO RECORDS OR INSPECTION REQUIREMENTS WERE FOUND FOR THE EXTERNAL DOUBLER REPAIR ON THE FUSELAGE BETWEEN STA 727G - 727H AT STR 21L. REMOVED EXISTING DOUBLER ON FUSELAGE SKIN BETWEEN STA727G TO 727H AT STR 21L. FABRICATED AND INSTALLED NSDR CALA2025092909372Skin · damagedAFT CARGO DOOR SKIN REPLACED. AFT PIT DOOR SKIN REMOVED AND REPLACED PER B737-800 SRM 52-30-01-2R-3 AND BAC DWG 146A6110. NO FURTHER ACTION REQUIRED.SDR CALA2025102610510Receptacle · gougedSUPPORT TASK R1 DOOR HANDLE BOX CUTOUT, UPPER TORQUE TUBE BUSHING STUB BEAM IS GOUGED, REMOVED DAMAGED STUB BEAM AND INSTALLED NEW STUB BEAM REF B737- 800 SRM 51-40-02 AND BAC DWG 141A6525 AND 141A6516.SDR CALA2025091809021Stub Beam · gougedSUPPORT TASK L1 DOOR, HANDLE BOX CUTOUT, UPPER TORQUE TUBE BEARING AREA, STUB BEAM IS GOUGED, REMOVED DAMAGED STUB BEAM AND INSTALLED NEW STUB BEAM REF SRM 51-40-02, NAC DWG 141A6260 AND 141A6143.SDR CALA2025060605341Transmitter · faultedON APPROACH FLAPS SKEW AND STOIPPED AT 15 AND 25. FELT AC ROLL. REMOVED AND REPLACED LEFT FLAP POSITION TRANSMITTER REF AMM 27-58-01-000-801. STILL STOPS AND SPLITS AT BETWEEN 15-25 REMOVED AND REPLACED LEFT FLAP POSITION TRANSMITTER FOR FURTHER TROUBLESHOOTSDR CALA2025022402461Light · detachedSEAT C12 EMERGENCY EXIT LIGHT ON THDE GROUND REMOVED AND REPLACED SEAT 12C SEAT MOUNTED EMERGENCY FLOOR PROXIMITY LIGHT BRACKET REFERENCE AMM 33-51-11. OPS CHECK GOOD.SDR CALA2024070500143Wheel · damagedHIGH SPEED REJECTED T/O FOR DIRECTIONAL CONTOL.REQEST MX INSPECTTOMC UPDATE: PER FLT CREW VERBAL, HIGH SPEED RTO WAS APPROX AT 100 KTS. LOCKED LP TP ENSURE HIGH ENERGY STOP AMM 05-51-07 IS COMPLIED WITH BEFORE DEPARTURE. MM CHANGED ALL 6 LANDING GEAR TIRES. SDR CALA2023050801404Shutoff Valve · unknownLEFT WING BODY OVHT MSG AFTER TAKEOFF MSG CLEARED AFTER SOME TIME WITH BLEEDS OFF FOLLOWED FIM26-18 TASK 801, WING BODY OVERHEAT DETECTION CONTROL CREW REPORT WING TO BODY OVERHEAT LIGHT TURN OFF ENGINE BLEED MODULE-BITE, IT SHOWS MSG 14, LEFT WING LE-ALARM. SDR CALA2022100602706Light · damagedSEAT MOUNTED EMERGENCY LIGHT AT ROW 34ABC INOP. REMOVED AND REPLACED LIGHT ASSY REF MM 33-51-11. OPS CK OK. VERIFIED INSEAT EMERGENCY LIGHT ATTACHED AND WORKS PROPERLY.SDR CALA2022100602705Light · damagedSEAT MOUNTED EMERGENCY EXIT LIGHT ON 37ABC DAMAGED. REMOVED AND REPLACED LIGHT ASSY REF MM 33-51-11. OPS CK OK. VERIFIED INSEAT EMERGENCY LIGHT ATTACHED AND WORKS PROPERLY.SDR CALA2022012600245Access Panel · departedPDA 2 AFT LAV SVC ACCESS PANEL DEPARTED THE AIRCRAFT AND WAS FOUND ON THE O''HARE TAXIWAY . UPDATING PHOTOS OF MISSING LAV ACCESS SVC PANEL, SEE CDL-52D REF L/P 7873970SDR CALA2020121001357Landing Gear · obstructedLANDING GEAR, MAIN AND NOSE DOES NOT RETRACT WHEN LANDING GEAR LEVER MOVED TO UP POSITION NOSE GEAR RED LT IN UP POSITION. SOUNDED LIKE GEAR MOVED BUT DOORS DID NOT CLOSE. VISUAL INSPECTION OF NOSE GEAR AND NOSE WHEEL WELL PERFORMED AND FOUND PLASTIC MAINTENSDR CALA2019111101952Floor Support · corrodedAFT CARGO COMPT FLOOR SUPPORT ANGLE CORR STA 787 TO STA 847 RBL 13.84 (REF NR 99851984) REMOVED CORROSION ON FLOOR SUPPORT ANGLE BETWEEN STA 787 TO STA 847 RBL 13.84 AS PER B737-800 SRM 51-10-02. FOUND TO BE OUT OF LIMITS PER REF B737-800 SRM 53-00-53. REMOVEDSDR CALA2019110301893Rib · crackedLT HRZ STAB IN-SPAR STIFFNER #1 CRACKED AT TRANSITION RADIUS STA 92.70. REF. AAR N/R: 99851822 REPAIRED LT HORIZ. STAB. IN-SPAR RIB AT STIFFNER #1 STA 92.70 PER B737-800 SRM 55-10-096 REPAIR 4,FIG.202,DETAIL "A".THIS IS A CATEGORY "A" REPAIR. DATA WAS TRANSCRSDR CALA2019110301890Skin · dentedFWD CARGO DOOR SKIN HAS DEEP DENT AT ABOUT 9.5" FROM TOP EDGE A ND 28.5 FROM FWD EDGE. REF. TO DMG L/P 6070962. INSPECTED DENT AND FOUND DENT LARGER THAN LIMITS SHOWN. W=3.7 Y .149 NO OTHER DMG NOTED. REF.SRM 52-20-01 ALLOWABLE DMG 1. INSP ECT FOR CORROSION ANSDR CALA2019110301889Skin · crackedCRACK FOUND AT R1 DOOR LOWER INTERNAL SKIN FORWARD UPPER SECTION UNDER 841AZ (REF NR NO. 99851848) REPAIRED THE R1 DOOR WHERE CRACK WAS FOUND AT LOWER INTERNAL SKIN UPPER SECTION UNDER PANEL 841AZ AS PER B737-800 RES NO. 2015275-14 REV P1. DOUBLER MATERIAL USESDR CALA2019110301888Skin · dentedR1 DOOR HAS NEG DENTS ON OUTER SKIN 3 INCHES ABOVE SNUBBER AND 5 INCHES FROM FWD EDGE. (REF NR 99852054) REPAIRED R1 DOOR OUTER SKIN ABOVE SNUBBER AS PER RES NO.201527523 REV P1 AND SRM 51-40-02. REPAIR DOUBLER, MATERIAL USED 2024-T3 CLAD PO NO. 1631052.SDR CALA2019103101857Skin · dentedR1 DOOR HAS NEG DENTS ON OUTER SKIN 3 INCHES ABOVE SNUBBER AND 5 INCHES FROM FWD EDGE. (REF NR 99852054) REPAIRED R1 DOOR OUTER SKIN ABOVE SNUBBER AS PER RES NO.201527523 REV P1 AND SRM 51-40-02. REPAIR DOUBLER, MATERIAL USED 2024-T3 CLAD PO NO. 1631052.SDR CALA2019110501908Seat Track · crackedAS PER NDT STEP 5.4 OF GENERATING CARD, CRACK INDICATIONS FOUND AT RBL 45.50 AFT I/B & O/B HOLE AT STA 727B REF. AAR N/R: 99852076 ORIGINATED BY EMPLOYEE ACCOMPLISHED PERMANENT REPAIR AT FLOOR BEAM UPPER CHORD & SEAT TRACK STA 727B , RBL 45.50 I/B & O/B ARSDR CALA2019110101879Rib · crackedRT. HORIZ STAB STA 129.50 IN-SPAR RIB STIFFENER # 2 IS CRACKED. REF. AAR N/R: 99851821 REPAIRED RT HORIZ. STAB. IN-SPAR RIB AT STIFFNER #2 TRANSITION RADIUS AREA PER B737-800 SRM 55-10-096 REPAIR 4,FIG.202,DETAIL "A". THIS IS A CATEGORY "A" REPAIR. ( STA 129.SDR CALA2019110101878Rib · crackedRT HORIZONTAL STAB IN-SPAR RIB AT STA 92.70 STIFFENER # 4 IS CRACKED. [MKD 78-28] REF. AAR N/R: 99851819 REPAIRED RT HORIZ. STAB. IN-SPAR RIB AT STA 92.70 STIFFNER #4 TRANSITION RADIUS AREA,PER B737-800 SRM 55-10-096 REPAIR 4,FIG. 202, DETAIL "A". THIS IS A CSDR CALA2019110501905Seat Track · crackedAS PER NDT STEPS 5.2 OF T/C CRACK INDICATION FOUND AT RBL 24.75 AFT O/B HOLE AT STA 727B REF. AAR N/R: 99852077 ORIGINATED BY EMPLOYEE ACCOMPLISHED PERMANENT REPAIR AT FLOOR BEAM UPPER CHORD & SEAT TRACK STA 727B , RBL 24.75 O/B AREA PER B737-800 SRM 53-40-5SDR CALA2019110501903Seat Track · crackedAS PER NDT STEP 5.2 OF GENERATING DOCUMENT,CRACK INDICATION FOUN D AT AFT O/B HOLE OF LBL 24.75 REF. AAR N/R: 99852075 ORIGINATED BY EMPLOYEE ACCOMPLISHED A PERMANENT REPAIR AT FLOOR BEAM UPPER CHORD & SEAT TRACK STA 727B,LBL 24.75 O/B AREA PER B737-800 SRM 5SDR CALA2019102981845Rib · crackedLT HRZ STAB IN-SPAR STIFFNER NO.4 CRACKED AT TRANSITION RADIUS. REF AAR NR 99851828 REPAIRED LT HORZ.STAB.IN-SPAR RIB AT STIFFNER NO.4 TRANSITION RA DIUS PER B737-800 SRM 55-10-09 REPAIR 4 FIG 202 (A) THIS IS A CA TEGORY "A" REPAIR.SDR CALA2019102981844Rib · crackedLT HRZ STAB IN-SPAR STIFFNER NO.2 CRACKED AT TRANSITION RADIUS. REF AAR NR 99851823 REPAIRED LT HORZ.STAB.IN-SPAR RIB AT STIFFNER NO.2 TRANSITION RA DIUS PER B737-800 SRM 55-10-09 REPAIR 4 RIG 202 (B). THIS IS A C ATEGORY "A" REPAIR.SDR CALA2019102981842Rib · crackedLT HRZ STAB IN-SPAR STIFFNER #3 CRACKED AT TRANSITION RADIUS. REF. AAR N/R: 99851825 ORIGINATED BY EMPLOYEE V891482 REPAIRED LT HORIZ. STAB. INSPAR RIB AT STIFFNER #3 TRANSITION RADIUS PER B737-800 SRM 55-10-09 REAPIR "A" FIG. 202 (B) THIS REPAIR IS A CATEGORSDR CALA2019102981841Rib · crackedRT HORIZONTAL STABILIZER STA 129.50 IN SPAR RIB WITH A CRACK INDICATION AT LOWER I/B NO.18 HOLE COUNTING FROM AFT REF AAR N/R 99852170 REPAIRED RT HORIXONTAL STAB INSPAR RIB AT STA 129.50 LOWER I/B FLANGE NO.18 HOLE COUNTING FROM AFT PER REF B737 SRM 55-10-09 SDR CALA2019102501813Fitting · crackedPAX CABIN CENTER WING BOX,AFT OF STA 540 2ND STIFFNER TO THE RIGHT OF BL 0 CRACKED. REMOVED AND REPLACED CRACKED STIFFNER ( SHEAR FITTING ) AT PAX CABIN WING BOX AFT OF STA 540 2ND TO THE RIGHT OF BL0 PER B737-8 00 SRM 51-40-02 AND DRWG#111A2000 .SDR CALA2019101801771Floor Support · corrodedCORROSION FOUND ON FLOOR SUPPORT AT STA 947.5 + 5 RBL53 . REMOVED CORROSION ON FLOOR SUPPORT ( INNER CHORD ) AT STA 947.5+ PER REF. B737-800 SRM 53-70-15. REMOVED AND REPLACED INNER CHORD ( P.O#1637761) AS PER B737-800 SRM 51-40-02 AND DRWG#147A8501 DATA WAS SDR CALA2019101801770Floor Support · corrodedCORROSION FOUND ON FLOOR SUPPORT AT STA 947.5 THROUGH 986 LBL 55 THROUGH 48. L2 DOOR ENTRY AREA LOWER. (200-036) REMOVED AND REPLACED L2 DOOR LOWER INNER CHORD AS PER B737-800 SRM 51-40-02 DUE TO CORROSION BEING OUT OF LIMITS,AS PER B737-8 SRM 53-70-15, DRWGSDR CALA2019101801769Intercostal · crackedFORWARD WET AREA BETWEEN STA 344 AND STA 360, BL 0, INTERCOSTAL IS CRACKED AT UPPER AFT FASTNER HOLE. [MKD 78-12 REF. AAR N/R: 99851708 ORIGINATED BY EMPLOYEE V891249 REMOVED AND REPLACED INTERCOASTAL AT FWD WET AREA BETWEEN STA344 TO STA 360 BL0,AS PER RSDR CALA2019032900480Duct · crackedAPU BLEED DUCT LEAK FWD WALL OF AFT PIT. CAUSED HEAT DAMAGE TO ISOLATION AND A BURN ODOR REPORTED BY CREW.
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