Boeing 737-2L9
Service difficulty reports · 593
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 = '7372L9' 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 = '7372L9' 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 KNNA200816Seat Track · corrodedREMOVED GALLEY AND FOUND THAT THE SEAT TRACK HAD EXFOLIATION CORROSION ON THE UPPER SURFACE AT STA 938 TO 947.5. RBL 24.5. REMOVED AND REPLACED SEAT TRACK FROM STA 927 TO STA 947, RBL 24.5.SDR KNNA200815Skin · corrodedOPENED UP MIDFLAP AND FOUND SKIN AND UPPER CHORD CORRODED AT REAR SPAR ON O/B MID FLAP RT WING. REPLACED OUTBOARD MIDFLAP.SDR KNNA20080014Seat Track · corrodedREMOVED GALLEY AND THEN FOUND CORROSION ON UPPER SURFACE OF SEAT TRACK AT STA 270 TO STA 294 AND RBL 16. REMOVED SECTION OF SEAT AND REPLACED WITH NEW SECTION.SDR KNNA20080013Skin · dentedFOUND SEVERAL DENTS ON FUSELAGE SKIN AROUND ALTERNATE STATIC PORT, RIGHT SIDE FROM STA 400 TO 440 AND STR 20R TO 24R. CUTOUT DAMAGE AND INSTALLED A REPAIR IAW SRM 53-30-3 FIG 46.SDR KNNA20080011Seat Track · corrodedREMOVED GALLEY AND THEN FOUND THAT A SEAT TRACK WAS CORRODED. REMOVED AND THEN REPLACED SEAT TRACK.SDR KNNA20080006Keelbeam · corrodedAFTER OPEN UP, FOUND CORROSION AT RT KEEL BEAM AT STA 727, AREA WENT OUT OF LIMITS AFTER CORROSION REMOVAL. REPAIRED AREA IAW BOEING MESSAGE 1-522105282 AND IAW SKY KING ACO-0753105.SDR KNNA20080005Keelbeam · corrodedAFTER OPEN UP, FOUND CORROSION AT RT KEEL BEAM AT STA 727, AREA WENT OUT OF LIMITS AFTER CORROSION REMOVAL. REPAIRED AREA IAW BOEING MESSAGE 1-522105282 AND IAW SKY KING ACO-0753105.SDR KNNA20080008Structure · crackedAFTER OPEN UP FOUND STA 727 RT CHORD CRACKED AT LWR END. CUTOUT OUT CHORD AND SPLICED IN NEW SECTION OF CHORD IAW SB 737-53-1088 AND ACO-085313.SDR KNNA20080007Keelbeam · corrodedAFTER OPEN UP FOUND CORROSION AT RT KEEL BEAM AT STA 727, AREA WENT OUT OF LIMITS AFTER CORROSION REMOVAL. REPAIRED AREA IAW BOEING MESSAGE 1-522105282 AND IAW SKY KING ACO-0753105.SDR KNNA20080010Skin · crackedFOUND CRACK ON FUSELAGE SKIN DURING C-CHECK. WHILE REMOVING FASTENERS FOUND CORROSION ON UPPER SKIN FWD OF CRACK, OPENED UP ENTIRE LAP JOINT AND REMOVED CORROSION ON UPPER SKIN. PERFORMED NDT IAW THE SRM AND FOUND 27 CRACKED COUNTERSINKS. CUTOUT ALL DAMAGE SDR KNNA20080009Skin · delaminatedDELAMINATION OF LEFT WING INBOARD AFT FLAP TRAILING EDGE WAS ORIGINALLY FOUND TO BE WITHIN LIMITS SO SPEED TAPE WAS APPLIED AS A TEMPORARY REPAIR AND THEN PLACED ON CARRY OVER. THE FLAP WAS MONITORED UNTIL THE CONDITION DETERIORATED BEYOND LIMITS SO IT WAS RESDR KNNA20080004Handle · unsecureACCORDING TO CAPTAIN'S REPORT, THEY DEPARTED ON RUNWAY 10 WITH FLAPS 5 DEGREES FOR IMPROVED PERFORMANCE AND UNPRESSURIZED DUE TO DEFERRED APU. AT 2,000 FT AND 210 KM/H, ENGINE BLEEDS UTILIZED FOR PRESSURIZATION. PERFORMED CLIMBING RIGHT TURN TO CROSS VALENCISDR KNNA20080002Fire Warning · false activationAPU FIRE WARNING ON APPROACH. APU WAS NOT OPERATING AND WAS CURRENTLY ON MEL 49-01 DMI 737-08-20. CAPTAIN'S AFTER LANDING INSPECTION FOUND NO EVIDENCE OF FIRE OR/OVERHEAT. PILOTS FOLLOWED AFM PROCEDURES AND FIRED APU FIRE EXTINGUISHER BOTTLE.SDR KNNA20080001Apu · malfunctionedTHERE WAS AN APU FIRE INDICATION IN FLIGHT AFTER PILOTS FOLLOWED ABNORMAL CHECK LIST FOR CSD LOW OIL PRESSURE LIGHT ILLUMINATION. ACCORDING TO PILOT'S REPORT, THEY WERE AT FLIGHT LEVEL 34,000 FEET WHEN THEY ATTEMPTED TO START, AS PER CHECK LIST, THE APU WHEN SDR KNNA200700069Apu · unknownTHERE WAS AN APU FIRE INDICATION IN FLIGHT AFTER PILOTS FOLLOWED ABNORMAL CHECK LIST FOR CSD LOW OIL PRESSURE LIGHT ILLUMINATION. ACCORDING TO PILOT'S REPORT, THEY WERE AT FLIGHT LEVEL 34,000 FEET WHEN THEY ATTEMPTED TO START, AS PER CHECK LIST, THE APU WHEN SDR KNNA200700064Ball Joint · leakingWHILE EN ROUTE, THE CREW WAS ALERTED BY A NR 1 ENGINE FIRE WARNING ALARM BELL/LIGHTS. DECLARING AN IN-FLIGHT EMERGENCY, AND SHUTTING DOWN NR 1 ENGINE, AND A SINGLE ENGINE LANDING WAS MADE. THE CREW WAS TOLD TO WAIT AT THE END OF THE RUNWAY AND WAS MET BY THESDR KNNA200700042Skin · crackedCRACK ON FUSELAGE SKIN AT LWR HINGE CUTOUT DOOR-R2 STA 951. REPAIRED AREA BY CUTTING OUT THE DAMAGE AND INSTALLING A REPAIR IAW SRM 53-30-3 FIG 45 AND ACO-0753104.SDR KNNA200700067Skin · dentedSEVERAL DENTS IN FUSELAGE SKIN AT STA 410 TO STA 445. REPAIRED AREA BY CUTTING OUT THE DAMAGE AND FABRICATING THEN INSTALLING REPAIR PARTS IAW SRM 53-30-3-FIG 46 AND SKYKING ACO-0753104.SDR KNNA200700066Skin · bulgedPREVIOUS REPAIR ON FUSELAGE SKIN AT STA 907 AND STR-25R. REPAIRED BY REMOVING EXISTING REPAIR AND CUTTING OUT THE DAMAGED AREA, THEN FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-30-03 FIG 48 AND SKYKING ACO-0753116SDR CA070504004Skin · cracked(CAN) DURING WASHING PROCEDURE MAINTENANCE DETECTED A SKIN CRACK AT BS727, WL215, APPROXIMATELY 1.5 INCHES LONG. THIS IS KNOWN AREA ADDRESSED BY SB 737-53-1065. THE AREA WAS REPAIRED IAW THE MANUFACTURERS SRM AND RETURNED TO SERVICE (TC NR 20070504004)SDR KNNA200700019Frame · cracked3 INCH CRACK OVER BODY STATION 360 FRAME BETWEEN STRINGERS 23 TO 22. REPAIR IS IN PROGRESS IN ACCORDANCE WITH SERVICE BULLETIN B737-53A1064 AND DRAWING NUMBER 65C23267.SDR 02072007Light · failedWHILE LANDING AT KLAX, DID NOT GET A GREEN LIGHT AFTER EXTENDING THE GEAR. THE MARKS ON THE LEFT MAIN GEAR. THE MARKS SEEN THROUGH THE VIEW PORT DUE TO THE MIRROR BEING DIRTY. CREW HAD TO BURN SOME FUEL AND REQUESTED EMERGENCY EQUIPMENT TO STANDBY. NORMAL SDR KNNA200700005Attach Fitting · corrodedCORRODED REINFORCING CLIP ON STRINGER 27-L, BS 1016. COMPLIED ACO 0653125, REPLACE CORRODED PRODUCTION SPLICE.SDR KNNA200700007Frame · crackedCRACKED VERTICAL FITTING ON RBL-26 AND BS 727 AT UPPER LIGHTENING HOLE. REPAIR SKIN PER ACO NR 0653124.SDR KNNA200700008Frame · crackedFOUND CRACKED FRAME ON LBL-24, B-STA727. INSTALLED INTERIM REPAIR, REQ, INSP EVERY 5,000 F/HRS.SDR KNNA200700006Frame · crackedFOUND CRACKED FRAME ON BL-0, B,STA-727. REPAIRED FRAME IAW ACO NR 0653122. INTERIM REPAIR INSP EVERY 5,000 FLIGHT HOURS.SDR KNNA200700004Floorbeam · crackedFOUND CRACK AT FLOORBEAM INTERIOR MAIN PASS CABIN, B-STA 678, LBL25. REPAIRED FLOORBEAM IAW ACO NR 653121.SDR KNNA200700003Skin · corrodedCORROSION AT LOWER LOBE EXTERIOR SURFACE BETWEEN BS 727 AND BS 727A, STRINGER 28-L. COMPLIED ACO NUMBER 0653120. INSTALL REPAIR FUSELAGE SKIN AND DOUBLER BS- 727 KEEL BEAM.SDR KNNA200700001Door Frame · damagedINSTALLED INTERIM REPAIR AT R1 DOOR CUTOUT AT THE AFT LOWER CORNER. REMOVED INTERIM REPAIR AND INSTALLED PERMANENT REPAIR.SDR KNNA200700002Frame · damagedINSTALLED INTERIM REPAIR AT L2 DOOR CUTOUT AT THE FWD LOWER CORNER. REMOVED INTERIM REPAIR AND INSTALLED PERMANENT REPAIR.SDR KNNA200600001Bulkhead · crackedCOMPRESSION FRAME CRACKED ON BULKHEAD BS 727 AT BL 0 FWD WALL OF AFT CARGO COMPARTMENT. CO 0653105 PROVIDE REPAIR INSTRUCTIONS ON REPAIR OF CRACKED WEB ANGLE IN WHEEL WELL AFT BULKHEAD BS 727 BL 0.SDR KNNA200600004Floorbeam · corrodedFOUND CORROSION AT FLOORBEAM STA 344 LBL 62.50 TO RBL 24.75.SDR 46504Floorbeam · corrodedFOUND CORROSION AT FLOORBEAM STA 344 LBL 62.50 TO RBL 24.75.SDR 46501Structure · crackedCOMPRESSION CHORD CRACKED ON BULKHEAD B-STA727 AT BL-0 FWD WALL OF AFT CARGO COMPARTMENT.SDR 465C7Structure · crackedCOMPRESSION CHORD CRACKED ON BULKHEAD B-STA727 AT BL-0 FWD WALL OF AFT CARGO COMPARTMENT.SDR KNNA200600003Floorbeam · corrodedFOUND CORROSION AT FLOORBEAM STA 328 BL-0 TO RBL 62.50.SDR 46503Floorbeam · corrodedFOUND CORROSION AT FLOORBEAM STA 328 BL-0 TO RBL 62.50SDR KNNA200600005Skin · damagedFOUND LIGHTNING STRIKE AT STA 216R BELOW RT EMERGENCY EXIT HANDLE. PROVIDE INSTRUCTIONS ON REPAIR OF LIGHTNING STRIKE AT FUSELAGE DRAIN HOLE STA 218, UNDER WINDOW NR 2.SDR KNNA20060001AAngle · corrodedCOMPRESSION CHORD CRACKED ON BULKHEAD OF BS 727, BL 0 (TOP) FWD WALL OF THE AFT CARGO COMPARTMENT. PROVIDE REPAIR INSTRUCTIONS ON REPAIR OF CRACKED WEB ANGLE IN WHEEL WELL AFT BULKHEAD BS 727 BL 0.SDR 2006F00053Relay · defectiveAFTER THE FA'S REQUESTED MORE HEAT IN THE CABIN, SMOKE APPEARED IN THE CABIN AND COCKPIT. INDICATION LIGHTS WERE (1) RT PACK OVERHEAT, (2) RT AIR MIX VALVE. INITIAL INSPECTION BY THE FLIGHT MECHANIC DID NOT FIND ANYTHING WRONG; WHEN OUR ACY STATION MECHANIC TSDR 2006F00052Relay · defectiveAFTER THE FA'S REQUESTED MORE HEAT IN THE CABIN, SMOKE APPEARED IN THE CABIN AND COCKPIT. INDICATION LIGHTS WERE (1) RT PACK OVERHEAT, (2) RT AIR MIX VALVE. INITIAL INSPECTION BY THE FLIGHT MECHANIC DID NOT FIND ANYTHING WRONG; WHEN OUR ACY STATION MECHANIC SDR CA061011008Control Unit · malfunctioned(CAN) ON TAXI FOR DEPARTURE THE CREW OBSERVED A NR 2 CARGO PIT CAUTION INDICATION. THE AIRCRAFT RETURNED TO COMPANY RAMP WHERE MAINTENANACE DETERMINED THE SMOKE DETECTOR SYSTEM CONTROL ELECTRONICS UNIT IN THE NR 2 PIT WAS AT FAULT. THE UNIT WAS REPLACED AND THSDR 2006F00034A/C Pack · failedAIRCRAFT N464AT DEPARTED EWN FOR ISO WITH THE LEFT HAND AIR CONDITIONING PACK AIRFLOW SHUTOFF VALVE ON DMI (MEL 21-02) AND FLYING UNDER PACK PRESSURIZED OPERATIONS PROCEDURE. EN ROUTE TO ISO AT A FL OF 22,000 FEET THE FLIGHT CREW NOTICED THE RIGHT HAND AIR COSDR 2003F00570Floorbeam · corrodedDURING C-CHECK INSPECTION, THE FLOORBEAM UPPER CHORD WAS FOUND TO BE CORRODED AT THE L1 DOOR AT STATION 344 LBL 24. THE DAMAGE EXCEEDS THE ALLOWABLE DAMAGE LIMITATIONS AND IS BEING REPAIRED ON NON ROUTINE 031642. (M)SDR 2003F00545Skin · delaminatedMSY-BNA - DURING POST REPOSITIONING FLIGHT INSPECTION, FLIGHT CREW OBSERVED UPPER SKIN DELAMINATION OF THE TRAILING EDGE NR 2 L/E SLAT, P/N 65-46422-267. A FOUR INCH SECTION OF THE UPPER SKIN HAD DELAMINATED THE ENTIRE LENGTH OF THE LE SLAT AND DEPARTED THE ASDR 2003F00563Clip · crackedDURING C-CHECK INSPECTION AND WHILE ACCOMPLISHING SERVICE BULLETIN SB 737-53-1204, THE UPPER AND LOWER ATTACH ANGLES WHERE FOUND TO BE CRAKCED AT THE INTERCOSTAL ATTACH POINT, BS 294.5 AND STRINGER 12L. THE REPAIRS ARE BEING ACCOMPLISHED ON NON-ROUTINE 031770SDR 2003F00566Frame · crackedDURING C-CHECK INSPECTION, A CRACK WAS FOUND AT THE 0 BBL FUSELAGE FRAME AT BS 663. THE CRACK EXTENDS THROUGH THE UPPER CHORD AND THROUGH THE WEB. THE REPAIRS HAVE BEEN ACCOMPLISHED ON NON ROUTINE 031284, USING SB KIT 65C34537-1. RELATED TO THIS REPAIR IS A SDR 2003F00567Floorbeam · corrodedDURING C-CHECK INSPECTION SURFACE CORROSION WAS FOUND TO BE BEYOND LIMITS AT FLOORBEAM BS 947.5. DURNG EVALUATION OF THE AREA A PREVIOUS WAS NOTED ON THE SAME FLOORBEAM. IN ORDER TO REPAIR THIS SKYKING OPTED TO REPLACE THE ENTIRE FLOORBEAM CAP. AIRCRAFT CHANSDR 2003F00565Door Frame · crackedDURING C-CHECK INSPECTION A 2.5 INCH CRACK WAS FOUND THROUGH TWO FASTENERS AT THE FORWARD AIRSTAIR DOOR UPPER STOP FRAME. THE REPAIRS WHERE ACCOMPLISHED ON NON ROUTINE 031245. (M)SDR 2003F00562Stiffener · crackedDURING C-CHECK INSPECTION, FOUND A .625 INCH CRACK IN AFT CARGO FLOOR OUTER EDGE STIFFENER AT LEFT SIDE BS 727B. THE DAMAGED WAS CORRECTED ON NON ROUTINE 031140. A NEW PART WAS FABRICATED AND INSTALLED. TOTAL AIRCRAFT TIME 46985.2. TOTAL CYCLES 41351. (M)
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