Boeing 737-522
Service difficulty reports · 1,682
Newest first. General aviation reporting is voluntary.
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 aircraft_model_key = '737522' 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 aircraft_model_key = '737522' 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 UALA2013051003271Structure · crackedRIGHT AFT SERVICE DOOR CUTOUT HAS A 1.5 INCH CRACK AT FWD LOWER CORNER, REPAIR AS REQUIRED. CATEGORY B REPAIR INSTALLED AT AFT SERVICE DOOR CUTOUT LOWER FWD CORNER.SDR UALA2013020100599Fitting · crackedRIGHT MLG OTBD SUPPORT FITTING IS CRACKED AT NR 2 HOLE. CRACK WITHIN LIMITS OF JC (I8593) FIG 2 SHEET 1. REPLACED PER MM 57- 55-99.SDR UALA2013013100584Door Frame · crackedFWD CARGO DOOR CUT OUT, AFT FRAME IS CRACKED ON AFT SIDE OF FRAME IN RADIOUS ADJACENT TO UPPER INBOARD CORNER OF LOWER BOTTOM STOP FITTING VERIFIED BY HFEC. REMOVED CRACK AND ACCOMPLISHED ANGLE REPAIR PER MM 53-30-75.SDR UALA2013013100579Attach Angle · crackedDURING SSR VISIT FOR EQ 1575 INTERCOSTAL WEB INSPECTION FOUND CRACKED ATTACH ANGLE AT BS 301.5 AND STRINGER 10L. REPLACED ATTACH ANGLE IAW REO L-01078 AND EVA 71600.SDR UALA2013013100578Frame · crackedFRAME BS 827 CRACKED AT PSU RAIL ATTACHMENT FASTENER BETWEEN S8-9L. REMOVED DAMAGE AND ACCOMPLISHED NDT FOR CRACKS. FABRICATED AND INSTALLED NESTED ANGLE REPAIR DOUBLERS AND FILLER REF AMM 53-10-84 REPAIR NR 3.SDR UALA2013013100577Frame · crackedFRAME AT BS 440 CRACKED AT PSU RAIL ATTACHMENT FASTENER BETWEEN STR 8R-9R. REMOVED DAMAGE AND NDT FOR CRACKS. FABRICATED AND INSTALLED NESTED ANGLES REPAIR DOUBLERS AND FILLER REF AMM 53-10-84 REPAIR NR 3.SDR UALA2012100905731Door Frame · crackedFORWARD CARGO DOOR CUTOUT, AFT FRAME CRACKED IN TWO PLACES AT I/B UPPER CORNER OF LOWER STOP FITTING. ONE CRACK IS ON AFT SIDE OF FRAME IN RADIUS AND THE OTHER ON FWD SIDE OF FRAME. HFEC. (N-R 12161-1400-0001) ACCOMPLISHED FILLER AND ANGLE REPAIR PER MM.SDR UALA2012100905730Skin · dentedSEVERAL FUSE DENTS AFT OF MED 2 LEFT STA 1016 STR 14L ONE EACH DENT AT STA 1088 STR 17L. NO CRACKS NO INTERNAL DAMAGE, DENTS WITHIN LIMITS. OK CONTINUED SERVICE.SDR UALA2012092105344Door Frame · crackedFORWARD CARGO DOOR CUTOUT, AFT FRAME CRACKED AT INBOARD RADIUS ABOVE LOWER STOP FITTING AND IN WEB INBOARD OF FITTING AT UPPER BOLT REF NR12637-1400-0001. REMOVED DAMAGE. FABRICATED & INSTALLED EXTERNAL NESTED ANGLE & FILLER REPAIR REF MM 53-30-75.SDR UALA2012092105343Support Fitting · crackedRIGHT MLG O/B SUPPORT FITTING IS CRACKED AT NR 1 HOLE. CRACK IS WITHIN LIMITS OF JOB CARD I8593 FIG 2 SHEET 1.SDR UALA2012091405195Door Frame · crackedFWD CARGO DOOR CUTOUT IS CRACKED IN TWO PLACES. FIRST CRACK IS ON AFT SIDE OF FRAME IS CRACKED IN TWO PLACES. FIRST CRACK IS ON AFT SIDE OF FRAME IN RADIUS ADJACENT TO I/B UPPER CORNER OF LWR STOP FITTING, SECOND CRACK IS ON FWD SIDE OF FRAME JUST BELOW UPPESDR UALA2012091405194Structure · damagedA CATEGORY B MAJOR SHEETMETAL REPAIR WAS INSTALLED BETWEEN STA 312 & 330 & BETWEEN STR 20R AND 21R PER SRM REPAIR 31.SDR UALA2012082404758Frame · crackedCABIN FRAME CRACKED BS 867 STR 8R. MAJOR REPAIR ACP'D, INSTALLED REPAIR ANGLE DOUBLERS PER MM 53-10-84 AT HMV3 ON NR11194-2000-0028. THIS REPAIR NEEDS A ONE TIME INSPECTION PER MM 53-10-84-601 BETWEEN 18000 & 24000 FROM CURRENT PTC 24573.SDR UALA2012082404750Structure · dentedFWD CARGO DOOR DENTED. LOCATE, INSPECT PER SRM 52-00-01. FOUND DENT 15.5 INCHES FROM AFT ON FWD CARGO DOOR 12.5 INCHES FROM TOP OF DOOR. DENT IS 4.5 INCHES LONG .5 INCH WIDE .064 INCH DEEP A-Y IS 7.8. OK TO DEF PER SRM 52-00-01 OK PER SFOLM. REMARKS: TO BSDR UALA2009092102960Oxygen System · emptyCREW REPORTS OXYGEN PRESSURE AT ZERO. SERVICED OXYGEN TO 1750 PSI.SDR UALA2009080302333Structure · damagedLEFT WING METAL PROTRUDING 1 INCH BY 6 INCHES AFT OF SLAT. REMOVAL OF NR 2 LEFT SLAT COMPLETED UP TO STEP 11-L. REMOVED NR 2 SLAT UP TO STEP (12) (P/N 65C26602-223, S/N 957). SLAT IS ON GROUND PLANE SIDE. STARTED INSTALLATION OF NR 2 SLAT P/N 65C26602-301,SDR UALA2009060101550Light · looseEMERGENCY LIGHTING FLOOR STRIP LOOSE NEAR ROWS 5 & 6. SECURED LIGHT STRIP.SDR UALA2009052701523Light · inoperativeLT WING OVERWING EMERGENCY LIGHT INOP. RELAMPED, OPS CHECK OKAY.SDR UALA2009042701215Radar · failedWEATHER RADAR FAILED IN FLIGHT. RTFL. REPLACED WEATHER RADAR. TESTED GOOD.SDR UALA2009041401068Battery Pack · dischargedCENTER EMERGENCY EXIT LIGHT INOP BETWEEN 2L AND 2R. REPLACED BATTERY PACK M1197, OPS OK.SDR UALA2009031800824Power Supply · faultyAFT 2 EMERGENCY EXIT LIGHTS RECESSED IN OVERHEAD BINS ON L&R SIDES OF A-C COME ON INTERMITTENTLY. REPLACED POWER SUPPLY AND BATTERY, CHECKS NORMAL.SDR UALA2009031300785Light · inoperativeCABIN ROW 8 RIGHT BULLNOSE EEL INOP. RELAMPED, LIGHT OP CHECKS OK.SDR UALA200903100074AIndicator · malfunctionedFLAP PROBLEM. RTFL. REMOVED AND REPLACED TRAILING EDGE FLAP POSITION INDICATOR. PERFORMED THE TEST OF THE TRAILING EDGE FLAP POSITION INDICATOR SYSTEM. TESTS OK. RAN FLAPS FULL UP AND DOWN SEVERAL TIMES, FLAPS ARE WORKING NORMALLY.SDR UALA2009031000746Flap · malfunctionedFLAP PROBLEM. RTFL.SDR UALA2009031000696Skin · damagedFOUND HOLE IN FUSELAGE APPROXIMATELY 36 INCHES AFT OF AFT CARGO DOOR. MAJOR REPAIR ACCOMPLISHED. HOLE MEASURES APPROX 2 1-8" X 1 1-4", WITH A SCRATCH LEADING TO HOLE APPROX 9 INCHES LONG. CUT OUT DAMAGE AND MFG DOUBLER AND STRAP. PRIMED BOTH AND AREA. NO SDR UALA2009030300721Skin · damagedFOUND HOLE IN FUSELAGE APPROXIMATELY 36 INCHES AFT OF AFT CARGO DOOR. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGE, MFG DOUBLER AND STRAP. PRIMED BOTH AND AREA. INSTALLED DOUBLER REPAIR.SDR UALA2009030300696Skin · damagedFOUND HOLE IN FUSELAGE APPROXIMATELY 36 INCHES AFT OF AFT CARGO DOOR. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGE, MFG DOUBLER AND STRAP. PRIMED BOTH AND AREA.SDR UALA2009020200353Fire Loop · failedCARGO DETECTION SUPPRESSION B-LOOP FAIL LIGHTS ON, AFT PIT IS NOT TESTING ON B-LOOP. REPLACED FORWARD AFT B-LOOP DETECTOR.SDR UALA2009011200126Controller · failedAT FL250 LT PACK COULD NOT HOLD ALT. CABIN HORN CAME ON AND WE HAD TO DO QRC W-DESCENT. REPLACED CABIN PRESSURE CONTROLLER. LT PACK FUNCTIONED NORMAL.SDR UALA2009011200123Control Panel · faultyNR 2 FIRE BOTTLE ARMED LT INOP. REPLACED CARGO SMOKE CONTROL FAULT PANEL, TESTS GOOD.SDR UALA2009031000085Slide · frayedDOOR 2R HARD TO ARM DUE TO FRAYED SLIDE PACK. REMOVED SLIDE & REPACKED SLIDE. SECURED HOOK AND LOOP ON GIRT BAR ASSY. SLIDE ARMS & DISARMS NORMALLY.SDR UALA2009010800085Slide · frayedDOOR 2R HARD TO ARM DUE TO FRAYED SLIDE PACK. REMOVED SLIDE AND REPACKED SLIDE. SECURED VELCRO ON GIRT BAR ASSY SLIDE ARMS AND DISARMS NORMALLY.SDR UALA2009010600077Skin · damagedAPPROX 5 FEET AFT OF DOOR 1R AND 6 INCHES BELOW PAX WINDOW, ACFT HAS APPROX .75 IN LONG PUNCTURE, WITHIN A 1.5 IN X 3 IN DENT, APPROX .25 IN DEEP. DAMAGED AREA CUT OUT. WILL REQUIRE DOUBLER-TRIPLER ENCOMPASSING PAX WINDOW BOX. TRIPLER-DOUBLER ENCOMPASSINGSDR UALA2008121906919Engine · odorSTRONG ENGINE OIL ODOR NOTICED IN COCKPIT DURING INITIAL CLIMB AFTER TAKEOFF. WITH PACKS OFF NR 1 ENGINE RUNNING, RIGHT AFTER NR 2 ENGINE START, GOT STRONG OIL ODOR IN COCKPIT. PACKS STILL OFF. RAN PACKS AND OIL ODOR WENT AWAY. BEFORE ENGINE RUN, RAN PACKSSDR UALA2008120906789Switch · faultyEMER EXIT LIGHTS ARE ILLUMINATED GATE WITH GROUND POWER. EMERGENCY LIGHTS WORK NORMAL IN THE ARM AND ON POSITION, LIGHTS REMAIN ON IN THE OFF POSITION, SUSPECT BAD SWITCH. REPLACED S7 EMERGENCY LIGHT SWITCH.SDR UALA2008120106698Slide · out of adjustDOOR 1 RIGHT SLIDE NEEDS ADJUSTING AS PER FLIGHT CREW. ADJUSTED DOOR SLIDE IN SLIDE HOLDER.SDR 2008UALA06498Indicator · faultyCREW OXYGEN PRESSURE INDICATOR INOP. CREW COMMENTS: FLUCTUATING 0 TO 1600. CONFIRMED PRESSURE AT BOTTLES OKAY. REPLACED COCKPIT CREW OXYGEN INDICATOR, READS NORMAL.SDR 2008UALA06471Controller · malfunctionedPRESSURIZATION PROBLEM. FLIGHT DIVERTED.
SDR UALA2008111306381Power Strip · damagedCABIN FLOOR EEL INOP FROM ROW 11 TO ROW 14. SPLICED EEL POWER STRIP AT ROW 11. OP CHECKS OKAY.SDR 2008UALA06385Connector · inoperativeCABIN FLOOR EEL INOP FROM ROW 4 TO ROW 11. CHECKED CONNECTIONS TO EEL FLOOR STRIP AND BATTERY PACK PWR SUPPLY, OPS CHECK EMERG LIGHTS, TEST OK.SDR 2008UALA06381Power Strip · damagedCABIN FLOOR EEL INOP FROM ROW 11 TO ROW 14. SPLICED EEL POWER STRIP AT ROW 11.SDR 2008UALA06380Battery · dischargedLEFT OVERWING EXTERNAL EMERGENCY SLIDE LIGHT INOP. OPS CHECK OK AFTER RECHARGING.SDR UALA2008111306359Duct · crackedWING BODY OVERHEAT LIGHT. RT FL DUE TO INCLEMENT WEATHER AT PLANNED DESTINATION. FAULT RECURRED ON NEXT FLIGHT OUT. PERFORMED TROUBLE SHOOTING, INTERROGATED M237 MODULE AND FOUND CODE 24 INDICATING LT A-C BAY OVERHEAT. INSPECTED LOOP AND COMPARTMENT. FOUND LASDR 2008UALA06359Warning System · activatedWING BODY OVERHEAT LIGHT. RTFL DUE TO INCLEMENT WEATHER AT PLANNED DESTINATION. FAULT RECURRED ON NEXT FLIGHT OUT.SDR 2008UALA06249Battery Pack · dischargedEMERGENCY LIGHTS FLOOR ROW 9-15 EXIT INOPERATIVE. REPLACED M1577 BATTERY PACK AND EMERGENCY LIGHTS CHECK NORMAL.SDR 2008UALA06238Lamp · inoperativeRT WING OVERWING EXIT EMERGENCY LIGHT INOP. REPLACED RT WING EMERGENCY LIGHT, OP CHECKS GOOD. ACFT OK FOR SERVICE.SDR 2008UALA06104Adc · malfunctionedR INERTIAL REFERENCE SYSTEM FAILURE. RTFL. REPLACED NR 2 ADC. CHECKS OKAY.SDR 2008UALA06032Flap · damagedRIGHT WING INBOARD TRAILING EDGE FLAP HAS A 4 INCH SPLIT AT THE TRAILING EDGE WITH APPROX 3.5 INCHES OF DELAMINATION IN LENGTH. RT AFT FLAP ROUTED TO SHOP FOR REPAIR. FLAP REINSTALLED. OP CHECKS NORMAL.SDR 2008UALA05901Panel · damagedRIGHT WING INBOARD LWR FIXED T/E PANEL NEXT TO BODY FAIRING DAMAGED AT WBL 71.26. REPLACED PANEL.SDR 2008UALA05799Light · inoperativeEMERGENCY LIGHTS IN FRONT OF THE AFT GALLEY IS IN OP. FOUND PINS GOING TO EEL STRIP BROKEN. REPLACED EMERGENCY LIGHT STRIP AND REPLACED TWO SIDED TAPE FOR MERGENCY LIGHT STRIP. OP CHECKED OK.
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