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 EE4Y2018041806374Skin · dentedDURING A STRUCTURAL INSPECTION, SEVERAL DEFORMATIONS AND DINGS (FROM INSIDE TO OUTSIDE) WERE FOUND AT MCD SURROUNDING AREA, COMMON TO LOWER FRAME SKIN BS 360 TO 500C, STRINGERS 18L AND 26L. THE DAMAGED AREAS WERE REPAIRED IAW EOS FROM AEI, EO6387, EO6388 AND SDR CA180313021Tube · leaking(CAN) AFTER SHUTDOWN, AT GATE, FOLLOWING FLT 702, A SMALL PUDDLE OF FUEL WAS NOTICED UNDER THE LT ENGINE. MAIN FUEL SUPPLY LINE FOUND LEAKING INSIDE LT ENGINE COWL. LINE REPLACED, GROUND RUN AND LEAK CHECKS CARRIED OUT. SERVICEABLE. (TC NR 20180313021).SDR Q2SA20180303390Wire · arcedSPARKS FROM OVERHEAD PANEL DURING ROLL-OUT. FOUND ARCING BEHIND DOOR INDICATION PANEL. FOUND DAMAGED WIRING AT D642 AND D1406 D482. REPAIRED THE WIRING IAW WPM 20-10-13. DOOR WARNING SYSTEM OPS NORMAL IAW MM 52-71-00, HYD SYSTEM OPS NORMAL IAW MM 29-15-00.SDR K11A201806113011Battery Pack · no testEMERGENCY LIGHT BATTERY PACK M1133 FAILED AN EMERGENCY LIGHTS FUNCTIONAL TEST.SDR K11A201806113010Skin · crackedCRACK DETECTED ON THE FUSELAGE SKIN, BS 727F, STRINGER 25RSDR K11A201806113009Skin · crackedA CRACK WAS DETECTED IN THE FUSELAGE SKIN, BS 727D, STRINGER 23L.SDR K11A201806113008Frame · crackedFWD CARGO, BS 500E, LT SIDE FRAME, WL 182.50, 1.04 DIA HOLE CRACKED FWD INBD SIDE.SDR K11A201806113007Frame · crackedFWD CARGO BS 500B, RT SIDE FRAME, WL 182.50, 1.04 DIA HOLE CRACKED FWD INBD SIDE.SDR K11A201806113006Frame · crackedPWD CARGO BS 500C, RT SIDE FRAME, WL 182.50, 1.04 DIA HOLE CRACKED, FWD INBD SIDE.SDR K11A201806113005Frame · crackedFWD CARGO BS 500D, RT SIDE FRAME, WL 182.50 DIA HOLE, CRACKED FWD INBD SIDE.SDR K11A201806113004Frame · crackedFWD CARGO, BS 500E, RT SIDE FRAME, WL 182.50, 1.04 DIA HOLE CRACKED FWD INBD SIDE.SDR K11A201806113003Frame · crackedFWD CARGO, BS 500F, RT SIDE FRAME, WL 182.50, 1.04 DIA. HOLE CRACKED FWD INBD SIDE.SDR K11A201806113002Frame · crackedFWD CARGO, BS 500G, RT SIDE FRAME WL 182.50, 1.04 DIA HOLE CRACKED FWD INBD SIDE.SDR K11A2017110573307Skin · puncturedLEFT HAND ELEVATOR LOWER SURFACE PUNCTURED. REPAIRED LEFT ELEVATOR SURFACE PUNCTURE IAW SRM 55-20-01 REPAIR 1.SDR K11A2017110573306Skin · puncturedLEFT HAND ELEVATOR UPPER SURFACE PUNCTURED. REPAIRED PUNCTURE ON UPPER SURFACE OF LEFT ELEVATOR IAW SRM 51-70-05, REPAIR 3.SDR K11A2017110573305Bulkhead · crackedPRESSURE WEB FORWARD SIDE CRACK IN WEB. REPAIRED PRESSURE WEB AT STA 178 LBL 15 IAW SRM 53-10-08, FIG 201 REPAIR 9.SDR K11A2017110573304Flap Track · crackedNR 7 FLAP TRACK HAS CRACKS IN THE HORIZONTAL FLANGES (IB AND OB). R&R FLAP TRACK WITH OVERHAULED IAW AMM 27-51-47.SDR K11A2017110573303Support · corrodedSTRINGER SUPPORT STRUCTURE HAS CORROSION. REPAIRED STRINGER SUPPORT WEB AT STA 271R IAW SRM 51-70-13 FIG 1.SDR K11A2018011173302Web · corrodedWEB FORWARD OF R1 HAS CORROSION. REPAIRED FLOOR STRUCTURE WEB AT STA 280 RIGHT HAND IAW SRM 51-70-13 FIG 1.SDR K11A201811173302Web · corrodedWEB FORWARD OF R1 HAS CORROSION. REPAIRED FLOOR STRUCTURE WEB AT STA 280 RIGHT HAND IAW SRM 51-70-13 FIG 1.SDR K11A2018011173301Tie Down · corrodedAFT CARGO COMPARTMENT TIE DOWN CORRODED, REPAIRED IAW SRM 53-00-53 FIG 201 REPAIR 2.SDR K11A2018061130001Light · inoperativeR1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE.SDR NP1Y20171127001Line · defectiveCREW OXYGEN SYSTEM HAS A LEAK. CREW OXYGEN BOTTLES FOUND TO BE EMPTY. BOTH BOTTLES WERE DEPLETED FULLY TO 0 PSI. CAPTAINS CREW OXYGEN MASK QUICK DISCONNECT FITTING WAS FOUND DISCONNECTED INSIDE THE CREW OXYGEN STOWAGE BOX ALSO. UPON FURTHER INVESTIGATION IT WASDR K11A2017110573302Battery Pack · dischargedEMERGENCY LIGHT FAILED LIGHTS TEST. R&R BATTERY PACK IAW AMM 33-51-51, OP'S CHECK GOOD.SDR K11A2017110573301Battery Pack · dischargedEMERGENCY LIGHT FAILED LIGHTS TEST. R&R BATTERY PACK IAW AMM 33-51-51, OP'S CHECK GOOD.SDR BJNA20171017001Unknown · malfunctionedPRESSURIZATION AUTO FAIL LIGHT ILLUMINATED DURING CLIMB, CABIN PRESSURE COULD NOT BE CONTROLLED NORMAL OR STANDBY, CABIN WAS CONTROLLED IN MANUAL MODE HOWEVER CABIN DID EXCEED 10000 FEET WHILE PERFORMING CHECKLIST PROCEDURES.SDR FOTR20171013149Crease Beam · corrodedCORROSION RT CREASE BEAM BETWEEN FS 847 AND FS 867, STR 17R BL70R.SDR FOTR20171004148Threshold · corrodedLI THRESHOLD HAS CORROSION ALONG DOOR JAMB BS 312-330, WL 208.SDR FOTR201710060001Threshold · corrodedL1 THRESHOLD CHORD HAS CORROSION ALONG DOOR JAMB.SDR 6GVA20170929001Line · disconnectedTHE AIRCRAFT WAS UNDERGOING A C CHECK, THE STANDBY ALTIMETER & AIRSPEED INDICATOR WAS REPORTED INOPERATIVE UPON ARRIVAL. DURING SUBSEQUENT TROUBLESHOOTING OF THE ALTERNATE STATIC SYSTEM, THE FLEXIBLE STATIC LINE TO THE LT STATIC PORT WAS FOUND DISCONNECTED FRSDR FOTR20170919143Doubler · corrodedCORROSION ON FUSELAGE AT LWR EDGE OF FWD LAV SERVICE DOOR CUTOUT.SDR FOTR20170914142Lug · corrodedRT HORIZONTAL STABILIZER FWD ATTACH LUGS UPPER AND LOWER HAVE CORROSION AROUND BUSHINGS.SDR FOTR20170914141Lug · corrodedHORIZONTAL STABILIZER FORWARD SPAR RIGHT CLEVIS UPPER JOINT HAS CORROSION AROUND FWD AND AFT FACE OF CLEVIS HOLE.SDR FOTR20170914140Lug · corrodedHORIZONTAL STABILIZER FORWARD SPAR LEFT CLEVIS LOWER JOINT HAS CORROSION AROUND FWD FACE OF CLEVIS HOLE.SDR BJNA20170929001Skin · dentedDENT IN SKIN AT BS 350, STRINGER 17L. INSTALLED A DOUBLER IAW SRM 53-00-01, REPAIR 31, FIG 201, DETAIL XX.SDR BJNA20170911008Warning Light · illuminatedLEFT WING BODY OVERHEAT LIGHT ILLUMINATED IN FLIGHT & WOULD NOT EXTINGUISH.SDR FOTR20170824135Rub Strip · corrodedLT PYLON UPON REMOVAL OF DISCREPANT IB & OB RUB PAD FOUND SURFACE CORROSION ON PYLON SKIN.SDR BJNA20170822007Slat System · malfunctionedAFTER TAKE OFF, AND FLAPS RETRACTED, THE LEADING EDGE FLAPS TRANSIT AMBER LIGHT REMAINED ILLUMINATED. NR 2 SLAT GREEN LIGHT REMAINED ILLUMINATED. AIRPLANE WAS TAKEN OUT OF SERVICE TO PERFORMED MAINTENANCE.SDR FOTR20170816137Rub Strip · crackedLT PYLON IB FLAP RUB PAD CRACKED IN RADIUS.SDR FOTR20170816136Rub Strip · crackedLT PYLON OB SLAT RUB PAD CRACKED IN RADIUS.SDR I5EA2017080200305Battery Pack · no testEMERGENCY LIGHTS AT ROW 7 AND 10 WOULD NOT TEST. REMOVED AND REPLACED THE BATTERIES.SDR K11A2017072673001Cabin Pressure · malfunctionedCOULD NOT CONTROL CABIN IN EITHER AUTO OR MANUAL MODESSDR K11A2017072573001Cabin Pressure · malfunctionedCABIN ALTITUDE LIGHT ILLUMINATED IN FLIGHT, UNABLE TO CONTROL CABIN IN EITHER AUTO OR MANUAL MODES.SDR Q2SA20170707383Control Valve · stuckDURING CLIMB OUT PASSING 15000 FT, CABIN ALTITUDE LIGHT ILLUMINATED. PERFORMED QRH PROCEDURE, VERIFIED ALL SWITCHES WERE CORRECT. MX TROUBLESHOT AIRCRAFT BLEED AND PRESSURIZATION ISSUES IAW AMM 36-11-05, AND 21-00-05. BLEED SYSTEM ON LT & RT ENGINE OPERATESSDR EE4Y201706283749Skin · corrodedDURING THE MAINTENANCE INSPECTION PROCESS, IT WAS FOUND THE FUSELAGE SKIN WITH CORROSION LOCATED AT BS 500F+17.5, BETWEEN S-26R AND S-27R, DUE TO THIS FACT THE FUSELAGE SKIN WAS REPAIRED IAW 737-400 SRM 53-00-01 REPAIR 31.SDR EE4Y201706293803Skin · damagedDURING INSPECTION, FOUND THE FUSELAGE SKIN DAMAGED FROM BS 360 TO 500C, BETWEEN STRINGERS 22L AND 26L. THE SKIN SECTION WAS REPLACED IAW EO4757.SDR EE4Y201706283755Frame · crackedDURING THE INSPECTION PROCESS, IT WAS FOUND LOWER FUSELAGE FRAME 500B WIRE PENETRATION AREA WITH A CRACK BETWEEN S-20R AND S-21R, THE AREA IS AFFECTED BY STC DUE TO THIS SITUATION, A REPAIR IS INSTALLED UNDER EO4763 INSTRUCTIONS.SDR EE4Y201706223806Skin · damagedAFT CARGO DOOR CUTOUT DAMAGED. REPAIRED IAW EO 4565-1, REV A.SDR EE4Y201706223804Skin · dentedLOWER SKIN DENTED BS 360 TO 500C, STRINGERS 21L TO 26L. REPAIRED IAW EO 4535, REV A.SDR EE4Y201705253606Skin · corrodedLOWER FUSELAGE SKIN WITH A REPAIR AND SKIN CORRODED BETWEEN BS 967 AND 1010 AND STRINGERS 23 AND 26L. REPAIRED IAW SR: 3-3873436610.
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