Boeing 737-214
Service difficulty reports · 209
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 = '737214' 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 = '737214' 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 BJNA961104Skin · crackedRIGHT WIND NR 4 SLAT INBOARD AUXILLARY TRACK CUT OUT, SKIN HAS .5 INCH LONG CRACK WBL 254. CUT OUT CRACKED FABRICATED AND INSTALLED FILLER AND DOUBLER IAW B737 SRM 57-30-4 AND 57-50-1 FIG 2. (M)SDR BJNA961102Skin · crackedRIGHT WING NR 4 SLAT AUXILLARY TRACK CUTOUT HAS .5 INCH LONG CRACK CENTER OF CUTOUT WSL 425. MECHANICALLY BLENDED CRACK EC VERIFIED NO FURTHER CRACKS. AFTER EVALUATION DETERMINED NOT TO BE ON SDR. (M)SDR BJNA961101Skin · crackedRIGHT WING NR 5 SLAT DE-ICE DUCT CUTOUT HAS .25 INCH LONG CRACK TOP CENTER. REMOVED CRACK FABRICATED AND INSTALLED REPAIR DOUBLER IAW B737 SRM 57-30-4 ND 57-50-3 FIG. (M)SDR BJNA961103Seat Track · corrodedDURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL CORROSION WAS FOUND IN THE FORWARD CARGO COMPARTMENT AROUND FASTENER HOLES AND THE TIE DOWN PAD ON THE FLOR TRACKS AT FS 500B TO FS 520 STRINGER 27L. CUT OUT CORRODED SECTION OF TRACK. FABRICATED ANSDR BJNA961112Rib · crackedDURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA THE LEFT WING INBOARD MID FLAP SEVENTH RIB FROM THE INBOARD END WAS FOUND WITH A CRACK ON THE LOWER FLANGE. REMOVED AND REPLACED WITH A NEW NR 7 RIB IAW B737 SRM 51-10-01, 51-30-02 PAGE 1 AND AESDR BJNA961107Rib · crackedDURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, THE LEFT WING INBOARD FLAP SECOND RIB FROM INBOARD END WAS FOUND WITH A CRACK AT THE LOWER AFT CORNER. GAINED ACCESS TO AREA. REMOVED CRACKED RIB. DRILLED AND INSTALLED NEW RIB AND KIT IAW 73SDR BJNA961106Rib · crackedDURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, THE LEFT WING INBOARD MID FLAP SIXTH RIB FROM INBOARD END WAS FOUND WITH TWO CRACKS ON THE LOWER FLANGE. REMOVED THE NR 6 RIB, CUT OUT GOUGED AND CRACKED SECTION OF WEB. FABRICATED AND INSTALLSDR BJNA961113Spar · corrodedDURIGN A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL THE LEFT WING INBD MID FLAP TRAILING EDGE WAS FOUND WITH DELAMINATION IN TWO PLACES 16 INCHES AT THE OUTBOARD EDGE AND 6 INCHES AT PREVIOUS REPAIR AT INBOARD EDGE. CUT OUT CORRODED HONEY COMB COMPOSISDR BJNA961111Floor Beam · corrodedDURING A SCHEDULED INSPECTION AT AERO COPR IN LAKE CITY, FLORIDA, THE LATERAL FLOOR SUPPORT ANGLE AT BS 268 BL 11L WAS FOUND WITH EXFOLIATED CORROSION ON THE UNDERSIDE OF THE FLT DECK. REMOVED CORRODED FLOOR BEAM. FABRICATED AND INSTALLED NEW FLOOR BEAM IAW SDR ZZDA7921396Elbow · looseMCI/MCO - FLT 823 - DURING CRUISE POWER, OIL QUANTITY ON NR 1 ENGINE DROPPED TO .6 GALLONS WITH PRESSURE AND TEMPERATURE NORMAL. REDUCED RPM TO IDLE AND DIVERTED TO BNA WHERE A NORMAL LANDING WAS MADE. MECHANICS INSPECTED NR 1 ENGINE AND FOUND DIFFERENTIAL OSDR ZZDA7921296O-Ring · leakingMCO/OMA - FLT 800 - ON FLIGHT, NR 1 ENGINE OIL QUANTITY STARTED TO DECREASE ACCOMPANIED BY A DROP IN OIL PRESSURE (TO 30 PSI) FOLLOWED BY THE NR 1 ENGINE OIL PRESSURE LIGHT ON STEADY. POWER WAS REDUCED TO IDLE RPM ON NR 1 ENGINE AND AIRCRAFT WAS DIVERTED TO MSDR CALA9601368Floorbeam · crackedINSPECTION FOUND A 1 INCH CRACK IN MAIN CABIN FLOORBEAM AT STA 724, BL 0. THE WEB AND STIFFENER WERE REMOVED IAW SRM 51-30-2. A WEB AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-20-4, 57-30-2, ECRA 5710-01755 AND REO 02209.SDR CALA9601367Fitting · gougedINSPECTION FOUND THE RT HORIZONTAL STABILIZER UPPER AFT SPAR INBOARD ATTACH FITTING GOUGED. THE ATTACH FITTING WAS REPAIRED IAW ECRA 5510-01338.SDR CALA9601366Floorbeam · crackedINSPECTION FOUND A 1.5 INCH CRACK IN FLOORBEAM AT STA 684, LBL 24.8. THE FLOORBEAM WAS REPAIRED IAW EA 5710-01638 AND SRM 51-40-4.SDR CALA9601365Skin · crackedINSPECTION FOUND FOUR .125 INCH CRACKS IN SECTION 41, LT FORWARD FUSELAGE EXTERNAL SKIN PANEL. THE CRACKED AREA WAS CUT OUT, FILLERS AND DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 51-10-2 AND EA 5310-01188.SDR CALA9601364Skin · crackedINSPECTION FOUND THREE .125 INCH CRACKS IN SECTION 41R, RT FORWARD FUSELAGE EXTERNAL SKIN PANEL. THE CRACKED AREA WAS CUT OUT, FILLERS AND DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 51-10-2 AND EA 5310-01188.SDR CALA9601363Keel Beam · galledINSPECTION FOUND LT KEEL BEAM FAYING FLANGE FROM BS 663 TO 727 GALLED ON LOWER SURFACE AND WORN AROUND FASTENER HOLES ON UPPER SURFACE. EXISTING HOLES WERE OVERSIZED AND 3 EACH PRESS FIT BUSHINGS WERE INSTALLED. A REPAIR STRAP WAS FABRICATED AND INSTALLED. SDR CALA9601362Flange · galledINSPECTION FOUND RT KEEL BEAM FAYING FLANGE FROM BS 663 TO BS 727 GALLED ON LOWER SURFACE AND WORN AROUND FASTENER HOLES ON UPPER SURFACE. A REPAIR STRAP WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-30-2 AND ECRA 5310-03324.SDR CALA9601361Frame · crackedINSPECTION FOUND A 2.5 INCH CRACK IN FRAME AT STA 947, STRINGER 18R. THE FRAME WAS REPAIRED IAWS SRM 53-10-2, 53-10-4, 51-10-7, 51-10-2 AND 51-30-2.SDR CALA9601360Floorbeam · crackedINSPECTION FOUND A 2 INCH CRACK IN FLOORBEAM AT STA 684, RBL 24.8. THE FLOORBEAM WAS REPAIRED IAW EA 5710-01638 AND SRM 51-40-4.SDR CALA9601359Chord Angle · crackedINSPECTION FOUND A 3.25 INCH CRACK IN MAIN CABIN FLOORBEAM LOWER CHORD ANGLE AT STA 673, BL 0. THE AREA WAS REPAIRED IAW BOEING DRAWING 65-45410, CAL ENGINEERING ORDER 031-5710-01322, SRM 51-40-4 AND 51-30-2.SDR CALA9601358Angle · crackedINSPECTION FOUND A .5 INCH CRACK THROUGH RADIUS OF RT WING ROOT FORWARD FILLET PANEL SUPPORT ANGLE. THE CRACK WAS LOCATED AT STA 540, 10 INCHES BELOW LOWER CAP OF FORWARD SPAR ADJACENT TO FORWARD END OF HINGED RAM AIR DUCT ACCESS PANEL. THE ANGLE WAS REPAIRESDR CALA9601357Stiffener · crackedINSPECTION FOUND A .5 INCH CRACK IN STIFFENER BETWEEN STRINGER 10L AND 11L AT FS 295. THE CRACKED SECTION OF STIFFENER WAS REMOVED AND A NEW SECTION WAS FABRICATED AND INSTALLED IAW SRM 53-10-3 AND 51-10-2.SDR CALA9601356Floorbeam · corrodedINSPECTION FOUND FLOORBEAM AND SUPPORT CORRODED AT AFT CABIN L-2 DOOR THRESHOLD, STA 986. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-9, 51-10-2 AND 51-30-2.SDR CALA9601355Skin · corrodedINSPECTION FOUND SKIN BULGED/CORRODED WITH POPPED FASTENERS AT FORWARD INBOARD CORNER OF AFT LAV DUMP CHUTE DOOR CUTOUT. THE CORRODED AREA OF SKIN WAS REMOVED IAW SRM 53-30-3. SKIN FILLER, DOUBLER AND SHIMS WERE FABRICATED IAW SRM 53-30-2. STRINGER 26R WAS SDR CALA9601354Stringer · crackedINSPECTION FOUND A 1.25 INCH CRACK IN WING SUPPORT STRINGER AT RIGHT WBL 70.85, WS 6. THE CRACKED SECTION OF STRINGER WAS CUT OUT, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-10-4, FIGURE 8 AND SRM 57-10-2.SDR CALA9601353Skin · dentedINSPECTION FOUND A 3 BY 5 INCH AREA OF FUSELAGE SKIN DENTED AT BS 890, LT SIDE, TOP OF WINDOW BELT. THE DENTED AREA WAS CUT OUT, DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 53-30-2, 51-10-2 AND SRM 51-30-2.SDR CALA9601352Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED BETWEEN SEAT TRACK ROW D AND CUSP LINE AT STA 360. A NEW FLOORBEAM WAS FABRICATED AND INSTALLED IAW SRM 53-10-9, 51-10-2 AND 51-30-3.SDR CALA9601351Bulkhead · crackedINSPECTION FOUND A 3.25 CRACK IN R/H SIDE OF PRESSURE BULKHEAD AT STA 178. THE BULKHEAD WAS REPAIRED IAW SRM 53-10-11 AND 53-10-2.SDR CALA9601350Beam · crackedINSPECTION FOUND A 3 INCH CRACK IN RADIUS OF TRANSVERSE BEAM AT STA 685. THE CRACK WAS STOP DRILLED, REPAIR ANGLES AND RADIUS FILLERS WERE FABRICATED AND INSTALLED IAW SRM 51-10-1 AND BAC DRAWING NR 65C17103.SDR CALA9601349Stringer · crackedINSPECTION FOUND A 1.125 INCH CRACK IN STRINGER 17R BELOW CABIN FLOOR AT FS 837. REPAIR DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 51-40-4, 51-10-2 AND 51-30-2.SDR CALA9601348Stringer · crackedINSPECTION FOUND A .75 INCH CRACK AT RT OUTBOARD END OF CENTER WING BOX UPPER STRINGER NR 3. THE CRACKED SECTION OF STRINGER WAS CUT OUT, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-10-4, FIGURE 4 FIGURE 8 AND SRM 57-10-2.SDR CALA9601347Stringer · crackedINSPECTION FOUND A .75 INCH CRACK IN STRINGER 12L AT STA 295. THE STRINGER WAS REPAIRED IAW SRM 53-10-2.SDR BJNA96802C1/C2 Disk · looseON WALK AROUND INSPECTION, FOUND C1/C2 SPACER RETAINING NUT AND KEY WASHER INSIDE HUB ASSY. REMOVED ENGINE. (M)SDR CALA9601149Gcu · inoperativeTHE LEFT BUS OFF LIGHT COME ON SHORTLY AFTER TAKEOFF. THE LIGHT WAS ACCOMPANIED BY AN ELECTRICAL ODOR OR AIR CONDITIONING PACK SMELL AND A CLICKING SOUND, LIKE THAT OF A RELAY OPENING AND CLOSING, THE SOUND WAS HEARD COMING FROM BEHIND THE SECOND OFFICER'S SESDR 96ZZZM1225Bypass Switch · dirtyFLT 670 - MCO-GSO - AFTER REACHING FL 250, THE NR 1 ENG OIL FILTER BYPASS LIGHT BEGAN FLICKERING. THE NR 1 ENG WAS SHUTDOWN AND AN EMERGENCY WAS DECLARED INTO DAYTONA. AIR TRAN MECHANICS REMOVED THE ENG OIL FILTER AND INSPECTED. ENG OIL FILTER WAS CLEAN. MSDR CALA9601042Hyd Line · leakingTHE A-SYSTEM HYDRAULIC QUANTITY BEGAN TO DROP SHORTLY AFTER TAKEOFF. THE AIRCRAFT WAS RETURNED TO CLE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NOSE GEAR DOWNLOCK ACTUATOR UPPER LINE LEAKING. THE LINE WAS REMOVED AND REPLACED, LEAK CHECK WAS GSDR 96ZZZM1436Fire Loop · crushedFLT 800 - MCO-OMA - 35 MINS INTO FLT APU FIRE WARNING CAME ON. APU WAS NOT IN USE AT THE TIME. FLT CREW PULLED THR FIRE HANDLE AND DISCHARGED THE FIRE BOTTLE. AN EMERGENCY WAS DECLARED INTO GAINSVILLE, FL. AN UNEVENTFUL LANDING WAS MADE. MECHANICS OPENEDSDR 96ZZZM1226Fire Loop · out of positionMCO-GSO - FLT 670 - IN FLT, THE APU FIRE WARNING CAME ON (AUDIBLE AND VISUAL). APU WAS NOT IN USE AT TIME. CREW PULLED THE FIRE HANDLE AND DISCHARGED THE FIRE BOTTLE, THE WARNING SYSTEM REMAINED ON. EMERGENCY WAS DECLARED, EMERGENCY DESCENT MADE. AFTER LANSDR BJNA96601Wire · brokenROWS 10 AND 15, EMERGENCY EXIT LIGHTS INOPERATIVE. REPAIRED BROKEN WIRES AS REQUIRED. (X)SDR BJNA96302Battery Pack · dischargedLEFT EMERGENCY OVERWING EXIT LIGHT WILL NOT ILLUMINATE. REMOVED AND REPLACED BATTERY PACK IW MM 33-51-41. OPS CHECK GOOD. (X)SDR BJNA96301Battery Pack · dischargedL2 DOOR EMERGENCY LIGHTS ARE DIM. REMOVED AND REPLACED L2 DOOR EMERGENCY LIGHTS BATTERY PACK. OPS CHECK GOOD. (X)SDR BJNA96101Splice · failedOVERWING SEAT EMERGENCY LIGHT LEFT, INOPERATIVE. REPAIRED SPLICE AND OPS CHECK OK IAW 20-30-12 AND 30-51-0. (X)SDR BJNA951201Battery Pack · inoperativeEMERGENCY EXIT LIGHTS FORWARD BATTERY PACK LOW. REMOVED AND REPLACED FORWARD EMERGENCY EXIT LIGHT BATTERY PACK PER BMM 33-51-51. OPS CHECK GOOD AT THIS STATION. (M)SDR CAL951064Dnlock Actuator · brokenFLT NR 1249 - EWR - THE RIGHT MLG WOULD NOT RETRACT AFTER DEPARTING BDL FOR CLE. THE GEAR WAS VISUALLY CONFIRMED DOWN AND LOCKED AND THE AIRCRAFT WAS DIVERTED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RIGHT MLG DOWNLOCK ACTUATOR BROKEN. SDR 95ZZZM669Motor · inopON APPROACH WHEN FLAP HANDLE WAS SELECTED TO 15, THE FLAPS REMAINED AT 5. THE POSITION OF THE FLAP HANDLE HAD NO EFFECT ON THE FLAP POSITION BEYOND 5 DEGREES. INSPECTED FLAP SYSTEM AND FOUND ALTERNATE SYSTEM ALSO INOP. REPLACED ALTERNATE FLAP DRIVE MOTOR. SDR BJNA95901Eel Bulb · failedROW 20 LEFT SIDE EMERGENCY EXIT LIGHT MISSING. REMOVED AND REPLACED MISSING EMERGENCY EXIT LIGHT IAW BSWP 20. OPSCHECKS GOOD THIS STATION. (M)SDR 95ZZZM519Skin · delaminatedNR 8 SPOILER DELAMINATED LOWER SURFACE APPROXIMATELY 612 SQUARE INCHES. REPLACED SPOILER PANEL. (M)SDR CAL950661Frame · crackedGSO - INSPECTION FOUND A .5 INCH CRACK IN FRAME AT STATION 440L BETWEEN STRINGERS 19L-20L. THE CRACKED FRAME SECTION WAS CUT OUT. A NEW FRAME AND CHORD SPLICES WERE FABRICATED AND INSTALLED IAW SRM 51-30-2 AND BOEING DRAWING NR 65C27113. (M)SDR CAL950659Frame · crackedGSO - INSPECTION FOUND A .5 INCH CRACK IN FRAME AT BS 639R, STRINGER 16. REMOVED CRACKED UPPER CHORD AND FRAME WEB AND INSTALLED REPAIR PARTS IAW BOEING DRAWING NR 65C31658 AND SRM 51-30-2. (M)
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