Boeing 737-400
Service difficulty reports · 470
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 = '737400' 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 = '737400' 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 KNNA201304220001Bulb · burned outEMERGENCY EXIT LIGHTS, LAST RED LIGHT AT AFT GALLEY INOPERATIVE. EMERGENCY EXIT LIGHTS ROW 8-11 INOPERATIVE.SDR FOTR121420123041Frame · crackedFWD CARGO COMPARTMENT FRAME IS CRACKED AT 1.04" WIRE PENETRATION HOLE BETWEEN STR 20L AND STR 21L, BS 500G. REPAIRED ON FAS WO 22248, NR 3041.SDR 7AHR20120806001Elbow · brokenAT STATION 520 IN THE BILGE AREA THERE IS A DRAIN LINE WITH A BROKEN ELBOW DRAIN. REPAIRED THE BROKEN DRAIN UTILIZING A DER, WHO DEVELOPED A REPAIR SCHEME. THE REPAIR PART WAS MANUFACTURED PER THE DER'S INSTRUSTIONS. DRAIN WAS RETURNED TO SERVICEABLE CONDITSDR CA120301013Solenoid · failed(CAN) ON CLIMBOUT, CREW WAS UNABLE TO SELECT GEAR UP. AFTER RETURNING TO BASE, MAINTENANCE DISCOVERED THE LANDING GEAR HANDLE LOCK SOLENOID HAD FAILED. THE SOLENOID WAS REPLACED AND THE ACFT RETURNED TO SERVICE.SDR XV6A2011070200012Pump · leakingAIR TURNBACK: NR 1 ENGINE HYDRAULIC LOW PRESSURE LIGHT ILLUMINATED IN FLIGHT. REMOVED AND REPLACED NR 1 ENGINE HYDRAULIC PUMP IAW B737-400 AMM 29-15-11. OPS AND LEAK CHECKS GOOD. NOTE: PART IS "ON CONDITION" THEREFORE TIMES AND CYCLES ARE NOT TRACKED.SDR XV6A2011070100011Actuator · leakingAIR TURNBACK: LOSS OF SYSTEM "A" HYDRAULIC FLUID. FOUND SEALS LEAKING AT NR 6 SPOILER ACTUATOR. O-RINGS (P/N NAS1612-12) REPLACED IAW BOEING CMM 27-60-41. LEAK AND OPS CHECK NORMAL. NOTE: PART IS "ON CONDITION" THEREFORE TIMES AND CYCLES ARE NOT TRACKED.SDR BJNA110403Lamp · burned outL1 DOOR EMERGENCY LIGHT INOPERATIVE. R & R LAMP IAW AMM 33-51-22. OPS CK GOOD.SDR BJNA110402Battery · inoperativeAFT LT INBD EMERGENCY FLASHLIGHT CHARGE WEAK. R & R AFT F/A FLASHLIGHT BATTERY IAW AMM 33-51-02.SDR XV6A2011032100006Servo · leakingDURING FLIGHT "A" HYDRAULIC SYSTEM QUANTITY STEADILY DECREASED.SDR BJNA100701Battery Pack · dischargedBULL NOSE EMERGENCY EXIT LIGHTS AT 18DEF AND 12 DEF WEAK ILLUMINATION. R & R BATTERY PACK IAW AMM 33-51-51, OPS CK GOOD.SDR BJNA100601Lamp · burned outEXTERIOR EMERGENCY EXIT LIGHT AT R1 DOOR INOPERATIVE. RELAMPED R1 DOOR SLIDE EMERGENCY LIGHT. OPS CK GOOD.SDR BJNA100201Lamp · burned outEMERGENCY AISLE LIGHT AT ROW 12 DEF INOPERATIVE. REPLACED LAMP, OPERATIONAL CHECK GOOD.SDR BJNA100102Lamp · burned outEMERGENCY AISLE LIGHT AT 19D NOT ILLUMINATED. RELAMPED AISLE LIGHT OPS CHECK GOOD.SDR MYWA09081Starter · malfunctionedETOPS SIGNIFICANT SYSTEM - NR 1 ENG NO ROTATION OF N1 OR N2 AFTER STARTER ENGAGED START VALVE LIGHT OPEN ILLUMINATED NORMAL.SDR MYWA09078Indicator · faultyETOPS SIGNIFICANT SYSTEM - TRANSCRIBED FROM DMI CONTROL LOG 6940. AFTER FUELING AIRCRAFT NR 2 TANK QTY INDICATORS AT REFUELING PANEL AND COCKPIT INDICATE QTY 0 AND ERROR CODE 6.1.SDR BJNA091101Lamp · burned outROW 11D EMERGENCY AISLE LIGHT REQUIRES RE-LAMP. RELAMPED 11D EMERGENCY AISLE LIGHT IAW AMM 33-51-21. OPS CHECKS NORMAL. (K)SDR BJNA091102Lamp · burned outSEVERAL ROW 12 AND 13 OVERWING EXIT LIGHTS REQUIRE RE-LAMPING. RELAMPED IAW AMM 33-51-21. OPS CHECKS NORMAL. (K)SDR BJNA0900901Flashlight · inoperativeAFT F/A FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED THE FLASHLIGHT AND BATTERY. (K)SDR XV6A2009051500008Antenna · failedUPPER TCAS ANTENNA FAILED.SDR BJN2009F00000Skin · corrodedTOP AFT LT CORNER OF THE CTR WING SKIN AT S-1C AND S-2C AT LBBL 60 TO 65 HAS CORROSION ON (3) SPOTS THAT ARE OUT OF THE LIMITS (0.080, 0.070, AND 0.050) OF THE MFG SRM. INSTALLED INTERNAL AND EXTERNAL DOUBLERS IAW AEROTECH STRUCTURES INC" 8110-3 APPROVED DWG SDR BJNA090201Lamp · burned outL1 DOOR INTERIOR EMERGENCY EXIT LIGHT HAS BURNED OUT BULB. RELAMPED EMERGENCY EXIT LIGHT IAW AMM 33-51-11. (K)SDR BJNA090101Apu · overheatedAPU FIRE/OVHT LIGHT ILLUMINATED IN FLIGHT. QRH/MEMORY ITEMS FOLLOWED, BOTTLE DISCHARGED, FIRE/OVHT LIGHT EXTINGUISHED. INSPECTION FOUND HEAT DAMAGE TO OVHT/FIRE DETECTION WIRING AND POSSIBLE TURBINE WHEEL FAILURE. REMOVED AND REPLACED APU. FAILURE ANALYSISSDR XV6A20081212Light · inoperativeDURING EVACUATION EXERCISES THE FWD SERVICE DOOR (RT) EMERGENCY SLIDE DEPLOYED NORMALLY BUT THE INTEGRAL SLIDE ILLUMINATION LIGHTS DID NOT ILLUMINATE.SDR BJNA081101Light · inoperativeL1 DOOR INTERIOR EMERGENCY EXIT LIGHT AS BURNED OUT BULB. RE-LAMPED EMERGENCY EXIT LIGHT IAW AMM. (K)SDR USAA SB08113Indicator · faultyFLIGHT 1282, PBI-DCA - DURING PREPARATION TO LAND IN DCA THE FLAPS STOPPED AT 2 DEGREES WITH ASSEMBLY INDICATION. THE CREW EXECUTED A MISSED APPROACH AND DID A GO AROUND. THE CREW RECYCLED THE FLAPS AND AFTER APPROXIMATELY THREE MINUTES THE FLAPS EXTENDED NOSDR USAA SB08112Unknown · odorFLIGHT 1868, PBI-CLT - ON TAKEOFF AND LANDING THE CREW REPORTED A SOUR ODOR COMING FORM THE AIR CONDITIONING PACKS. THE ODOR DISSIPATED IN CLIMB. MAINTENANCE INSPECTED THE LEFT AND RIGHT RAM INLET, THE LEFT AND RIGHT ENGINE INLETS AND AIR MIX CHAMBER. ALL CSDR BINA081001Lamp · burned outLT FORWARD EXTERIOR OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. RE-LAMPED EMERGENCY EXIT LIGHT IAW AMM 33-51-22.SDR BJN2008F00000Lamp · burned outONE EMERGENCY AISLE LIGHT, ROW 12, RT SIDE, BURNED OUT. REPLACED EMERGENCY LIGHT BULB. (K)SDR CA080708011Wire · chafed(CAN) P5 OVERHEAD COCKPIT PANEL WAS OPENED DURING NORMAL MX ACTIVITIES AT THE C2 MX EVENT. ARCING WAS NOTED BETWEEN THE DOOR WARNING MODULE AND ADJACENT WIRE BUNDLES. DAMAGE TO WIRING WAS ALSO FOUND AT THE P5-13, ELECTRICAL METERS AND GALLEY POWER MODULE. INSPSDR BJNA080501Battery · dischargedFORWARD RT EMERGENCY FLASHLIGHT HAS DEAD BATTERY. REPLACED BATTERY IN THE FORWARD RT EMERGENCY FLASHLIGHT. (S)SDR BJNA080402Actuator · malfunctionedSTABILIZER TRIM WOULD NOT KEEP UP WITH THE COMMANDED POSITION, ASSOCIATED WITH A STAB OUT OF TRIM ANNUNCIATION. STABILIZER TRIMMED "UP" OK. REMOVED AND REPLACED STABILIZER JACK SCREW ASSEMBLY. OVERHAUL FOUND - P/N 54032-006 SCREW ASSEMBLY WORN; P/N 65C34615SDR BJNA032908002Jackscrew · damagedSTABILIZER TRIM WOULD NOT KEEP UP WITH THE COMMANDED POSITION, ASSOCIATED WITH A STAB OUT OF TRIM ANNUNCIATION. STABILIZER TRIMMED (UP), OK. REMOVED AND REPLACED STABILIZER JACK SCREW ASSY. WAITING FOR TEAR DOWN REPORT ON REMOVED UNIT. (K)SDR BJNA032908001Spring · brokenBJNA080401- ALTITUDE HOLD INTERMITTENT. FOUND ELEVATOR LOAD FEEL CENTERING SPRING (OUTER) BROKEN. REMOVED AND REPLACED ELEVATOR LOAD FEEL CENTERING SPRINGS (INNER AND OUTER). (K)SDR BJNA080201Battery · dischargedF/A EMERGENCY FLASHLIGHT BATTERY DISCHARGED. REMOVED AND REPLACED THE EMERGENCY FLASHLIGHT BATTERY. (K)SDR BJNA080202Power Supply · inoperativeEMERGENCY LIGHT AT ROW 21 WILL NOT TEST. REMOVED AND REPLACED THE POWER SUPPLY AND BATTERY. (K)SDR BJNA070601Slide · failedDURING TRAINING DEPLOYMENT OF L-1 DOOR EMERGENCY EXIT SLIDE, THE SLIDE FAILED TO COMPLETELY UNFOLD, THE BOTTOM 2 LANYARDS FAILED TO PULL THROUGH STRAP EYELETS WHICH PREVENTED APPROXIMATELY THE LAST 1.5 - 2.0 FT TO UNFOLD AND INFLATE. AN ENGINEERING EVALUATIONSDR PIDA06128Bushing · migratedREPLACED THE FUSE PIN BUSHING IN THE LEFT ENGINE STRUT MID-SPAR ATTACH FITTING PER BOEING SB 737-54-1037 DUE TO BUSHING MIGRATION.SDR PIDA06121Skin · damagedTHE EXTERIOR SKIN OF THE AFT CARGO DOOR WAS REPLACED PER SRM 52-30-01 DUE TO MULTIPLE AREAS OF DAMAGE.SDR PIDA06123Skin · corrodedCORROSION ON THE INNER SKIN OF THE RIGHT ENGINE I/B THRUST REVERSER WAS REPAIRED PER EA 71-349.SDR PIDA06122Strip · wornA WEAR STRIP WAS INSTALLED ON THE I/B SIDE OF THE LEFT ENGINE PYLON PER BOEING SB 737-54-1031 DUE TO WEAR MARKS JUST ABOVE THE THRUST REVERSER SLIDER.SDR PIDA06127Skin · dentedDENT IN FUSELAGE SKIN AT BS 867+4 JUST BELOW STR 17 LT WAS REPAIRED PER SRM 53-00-01 REPAIR 31.SDR PIDA06107Tee Fitting · crackedAFT CARGO DOOR T-CHORD CRACKED AT FASTENER HOLE ON NR 4 FRAME. REPAIRED T-CHORD PER BOEING DWG 65-47952 AND SRM 51-70-12.SDR USAA200701003Frame · crackedCRACK AT LBL 380, FRAME 1 INCH BELOW S14L. REMOVED DAMAGE, INSTALLED FILLER & 11 INCH DOUBLER PER EA 98280.SDR BJNA061001Brake Assy · seizedAT INITIAL TAXI, AFTER TURN, AIRCRAFT DRAGGED TO A STOP AS RESISTANCE FELT IN LANDING GEAR. INSPECTION FOUND NR 2 BRAKE SEIZURE. REPLACED BROKEN AND DAMAGED PARTS AND OVERHAULED BRAKE ASSEMBLY. (K)SDR 2006FA0000896Retainer · dislodged(REF: 2006FA00008996) DURING STRIP OF ENGINE 857819 FOR SCHEDULED LLP REPLACEMENT IT WAS NOTED THAT THE HPT FORWARD BLADE RETAINER HAD LIBERATED 2 SECTIONS OF MATERIAL, ONG 3.5 INCHES X .8750 INCH AND 1) 2 INCH X .8750 INCH. THE LIBERATED MATERIAL HAD CAUSED SDR CA060723004Frame · corroded(CAN) SKIN TO FRAME ATTACH ANGLE CORRODED NR BS 520, STR 27R TO 28R (TC NR20060723004)SDR CA060723003Frame · corroded(CAN) FWD CARGO PIT FRAME CORRODED AT BS 500C AND STR 28R TO 28L (TC NR 20060723003)SDR CA060723002Frame · corroded(CAN) FWD CARGO PIT FRAME TO SKIN AT BS500C CORRODED STR 27R TO 28R (TC NR 20060723002).SDR CA060723001Frame · corroded(CAN) FWD CARGO PIT FRAME TO SKIN AT BS 500B CORRODED BETWEEN STR 28R AND 28L (TC NR 20060723001).SDR BJNA060401Wire · brokenROW 13, EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED BROKEN SPLICE IAW STANDARD WIRING PRACTICES MANUAL REF 20-10-13. (K)
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