Boeing 737-2P6
Service difficulty reports · 200
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 = '7372P6' 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 = '7372P6' 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 ZZDA5512497Skin · dentedDURING C-CHECK, FOUND RIGHT HORIZONTAL STABILIZER DENTED, 110 INCHES BY 5.5 INCHES BY 4 INCHES AT THE OUTBOARD END OF UPPER SKIN 5.5 INCHES FROM FORWARD UPPER SPAR. REMOVED DENT IAW B737 SRM 55-10-3. FABRICATED PLATE FROM 2024 T3 .071 INCH BY 5.375 INCHES BYSDR ZZDA5512197Skin · damagedDURING C-CHECK, FOUND LT HORIZONTAL STABILIZER LEADING EDGE REPAIR NEEDS REPLACEMENT. FABRICATED FLUSH DOUBLER FROM 2024 T3 .063 INCH, 12.625 INCHES BY 8.375 INCHES. INSTALLED REPAIR IAW B737 SRM 55-10-3. INSTALLED FILLER .040 INCH BY 8.25 INCHES BY 4.875 ISDR 97ZZZM929Skin · misrepairedDURING C-CHECK, FOUND LEFT HORIZONTAL STABILIZER LEADING EDGE REPAIR NEEDS REPLACEMENT. FABRICATED FLUSH DOUBLER FROM 2024 T3 .063 12.625 INCH BY 8.375 INCH INSTALLED REPAIR IAW B737 SRM 55-10-3. INSTALLED FILLER .040 BY 8.25 INCH BY 4.875 INCH IAW B737 SRM SDR ZZDA5311997Bulkhead · cannedDURING C-CHECK, FOUND AFT PRESSURE BULKHEAD AT BS 1016 HAS OIL CANNING AT THE 2 O'CLOCK RADIUS PIE SECTION. FABRICATED CHANNEL AND STRAP FROM 2024-0 .040 INCH, 16.8750 INCHES BY 3.25 INCHES, 2 INCHES BY 15.25 INCHES IAW B 737 SRM 53-10-4. INSTALLED IAW B 737SDR 97ZZZM876Press Blkhd · oil cannedDURING C-CHECK, FOUND AFT PRESSURE BULKHEAD AT BS 1018 HAS OIL CANNING AT THE 2 O'CLOCK RADIUS PIE SECTION. FABRICATED CHANNEL ANS STRAP FROM 2024-0 .040 16.875 INCH BY 3.75 INCH 2 INCH BY 15.25 INCH IAW B737 SRM 53-10-4. INSTALLED IAW B737 SRM 53-10-4 AND MSDR ZZDA3310497Socket · wire brokenDURING WALK-AROUND, FOUND ROW 6 EMERGENCY FLOOR LIGHT INOPERATIVE. TROUBLESHOT TO LIGHT SOCKET WIRE BROKEN. REMOVED AND REPLACED LIGHT SOCKET. OPS CHECKED NORMAL. (X)SDR ZZDA3310397Socket · failedDURING PRE-FLIGHT CHECK, FOUND E-PATH LIGHTING INOPERABLE FAR AFT OF AIRCRAFT. INSTALLED NEW SOCKET ON EMERGENCY LIGHT REFERENCE B737 MM 33-51-00. FUNCTIONALLY CHECK OK. (X)SDR 97ZZZX2935Wire · brokenDURING LINE CHECK, THE THIRD FORWARD ROW OF EMERGENCY FLOOR TRACK LIGHTS PN 08202120 WERE FOUND INOPERATIVE. APPARENTLY, WIRE WAS KICKED BY PASSENGER. REPAIRED WIRES AND SYSTEM CHECKED OK.SDR 97ZZZX2934Power Supply · shortedDURING PRE-FLIGHT INSPECTION, THE FORWARD SECTION OF EMERGENCY FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. FOUND POWER SUPPLY SHORTED, INOPERATIVE. REPLACED POWER SUPPLY AND SYSTEM CHECKED OK.SDR 97ZZZM558Lens · missingEMERGENCY AISLE LIGHTING (P/N 07912) AT ROW 2 ABC IS PROTUDING FROM CASING. REPLACED LENS COVER AT ROW 2 ABC IN AISLE PATH LIGHTING. LIGHT OPS CHECK GOOD. REFERENCE B MM 33-51-0. LENS P/N 07912. (M)SDR 97ZZZM660Bulb · missingSECOND ROW EMERGENCY TRACK LIGHT LENS AND BULB MISSING. REPLACE BULB AND LENS. OPS CHECKED OK.SDR 97ZZZM373Angle · corrodedDURNG C-1 CHECK AT AERO CORP 31J, THE RIGHT VERTICAL STABILIZER LOWER MOUNT HORIZONTAL ATTACH ANGLE WAS FOUND TO BE CORRODED BEYOND ALLOWABLE LIMITS. REMOVED AND FABRICATED NEW SUPPORT BRACKET PER BAC PRING 69-39677, MATERIAL 7075 T-6 .365 DIM, 5.5 INCH BY 2.SDR 97ZZZM194Handle · out of adjustDESCENDING THROUGH 23,000 FEET 'AFT SERVICE' DOOR LIGHT ILLUMINATED. FLIGHT ATTENDANT MOVED DOOR HANDLE, LIGHT WENT OUT. FLIGHT ATTENDANT REPORTED APPROXIMATELY 2 INCH PLAY IN HANDLE. NO EMERGENCY PROCEDURES WERE NECESSARY. MAINTENANCE ACCOMPLISHED ADJUSTMSDR 97ZZZM324Adi Wire Bundle · water contamDURING MX FOR F/O'S ADI INDICATOR MALFUNCTIONS, ELECTRONIC RACKS E-1 AND E-2 WERE REMOVED. THE REMOVAL OF THE RACKS WAS NESSITATED BY THE DISCOVERY OF 'BLUE WATER' INTRUSSION INTO THE WIRE BUNDLES FEEDING THE E-1 AND E-2 RACK CONNECTORS, WHILE THE LEAKAGE CAUSDR 97ZZZM325Pitot Line · leakingFLT 822 - MCO-MCI - AIRCRAFT ABORTED TAKEOFF AS A RESULT OF A 20 KNOT DIFFERENTIAL REFERENCE BETWEEN CAPTAIN'S AND FIRST OFFICERS AIR SPEED INDICATORS. PERFORMED LEAK CHECK OF THE PITOT STATIC SYSTEM PER B737 MM 34-12-01. FOUND LEAK IN FIRST OFFICERS STATIC SDR 97ZZZM205Fire Bottle · dischargedWHILE ATTEMPTING START AT 33,000 FEET, APU FIRE WARNING INDICATION, BOTTLE DISCHARGED. MADE VISUAL INSPECTION OF APU FOR EVIDENCE OF FIRE, NONE NOTED. REPLACED APU FIRE BOTTLE AND SQUIB. MADE OPERATIONAL TEST OF APU AND FIRE WARNING SYSTEM, ALL CHECKED OK.SDR 97ZZZM204Stringer · crackedFOUND 5 INCH FATIGUE CRACK AT STATION 787 STRINGER ISL. REPAIR COMPLETED BY INSTALLING A DOUBLER PER STRUCTURAL REPAIR MANUAL 53-30-3 FIGURE 6. (M)SDR 96ZZZX5984Skin · crackedON WALK-AROUND, CREW FOUND 5 INCH CRACK IN SKIN AT STA 787, STR 18L. INSTALLED DOUBLER PER SRM 53-30-6, FIG 6.SDR ZZDA2721696Transmitter · malfunctionedCAK - FLT 720 - ON APROACH INTO CAK, THE AIRCRAFT EXPERIENCED A FLAP ASSEMETRY TRIP. CAPTAIN ELECTED TO DIVERT INTO CVG WHERE A NORMAL LANDING WAS MADE. MECHANICS TROUBLESHOT SYSTEM AND FOUND THE RIGHT FLAP POSITION/STALL WARNING TRANSMITTER AND THE TRAILINGSDR 96ZZZM1565Wire · brokenEMERGENCY TRACK LIGHT FOUND INOPERATIVE. MAINTENANCE FOUND BROKEN WIRE, SOCKET AND LAMP.SDR 96ZZZM1566Light · serviceableWIRE STICKING OUT OF EMERGENCY FLOOR TRACK LIGHTING. PASSENGER KICKED UP TRACK LIGHTING COVERING. WIRE RESECURED IN TRACK COVER.SDR 96ZZZM1420Track · brokenDURING AN INSPECTION, IT WAS DISCOVERD THAT THE EMERGENCY FLOOR TRACK LIGHTING WAS BROKEN BY PASSENGERS WALKING AND KICKING THE TRACK AT ROW 22. BAD SECTION REPLACED AND SECURED. FLOOR LIGHTS OPS CHECKED GOOD. (M)SDR 96ZZZM1224Brake · malfunctionedDURING POST FLIGHT INSPECTION, PILOT FOUND NR 1 TIRE FLAT. MAINTENANCE INSPECTION REVEALED THAT THE THERMAL FUSE HAD MELTED DURING BRAKE OVERHEAT. PILOT REPORTED THAT NO HIGH ENERGY STOP HAD BEEN MADE. SUSPECT DRAGGING BRAKE. PERFORMED BRAKE OVERHEAT INSPESDR 96ZZZM1235Window Heat Cont · failedDURING DESCENT INTO BHM FLT, CREW EXPERIENCED SMOKE IN COCKPIT. SMOKE PROCEDURES WERE ADHERED TO, WHICH INCLUDE WINDOW HEAT OFF AND ALTERNATE BLOWER ON. CONTRACT MAINTENANCE WAS DISPATCHED UPON LANDING. TROUBLESHOOTING REVEALED R1 WINDOW HEAT INOP. HEAT COSDR 96ZZZX2544Insulation · out of positionMCO - FLT 560 - DURING CLIMB-OUT THROUGH 13,000 FEET, PRESSURIZATION CONTROL BECAME ERRATIC. THE FLIGHT CREW RETURNED THE AIRCRAFT TO MCO. AFTER INSPECTION, A PIECE OF INSULATION WAS FOUND STUCK IN THE OUTFLOW VALVE. INSULATION WAS REMOVED AND ALL RELATED SSDR 96ZZZX4766Egt Indicator · failedAIRCRAFT ON TAKEOFF ROLL AT APPROXIMATELY 80 KTS WHEN NR 1 EGT CLIMBED TO RED BAND, CREW REJECTED TAKEOFF AND RETURNED TO GATE. FOUNT NR 1 EGT INDICATOR BAD AND REPLACED. NR 1 EGT INDICATOR WAS SENT OFF FOR REPAIR AND RETURNED FOR INSTALLATION.SDR 96ZZZX2562Taxi Light · fod to engineJAX - FLT 904 - APPROXIMATE V1 SPEED HEARD LOUD POP, THOUGHT IT MIGHT BE A TIRE. LEFT GEAR DOWN AND MADE A GO-AROUND. AFTER LANDING AND BACK AT THE GATE AFTER SHUTTING ENGINES DOWN, DISCOVERED DAMAGE TO NR 1 ENGINE 1ST AND 2ND STAGE FAN. UPON INVESTIGATION, SDR 96ZZZM259Hyd Module · leakingAFTER TAKEOFF FROM OMA, LANDING GEARS WOULD NOT RETRACT RESULTING IN AN AIR TURN BACK. FOUND 'B' HYD SYSTEM MODULE UNIT (HOUSING) FAILED AT THE NR 5 PUMP PRESSURE SUPPLY PORT. REMOVED AND REPLACED MODULE PER MM 29-12-31. OPS AND LEAK CHECK GOOD. ALSO, FOUNSDR 95ZZZM760Power Supply · inoperativeFORWARD CABIN EEL POWER SUPPLY INOPERATIVE. CHANGED EEL POWER SUPPLY, OPS CHECK GOOD. (M)SDR 96ZZZX2123Frame · dentedCLT - CLT INSPECTION VISUALLY FOUND A 6 INCH BY 12 INCH DENT CAUSING INTERNAL DAMAGE TO FRAME LOCATED STA 807, BL ZERO, BETWEEN S27L AND BL ZERO. INSTALLED REPAIR ANGLES PER SRM 51-40-3.SDR 96ZZZX2122Skin · lightning strikeCLT - CLT INSPECTION VISUALLY LOCATED A LIGHTNING STRIKE LOCATED ON SKIN AT STA 875, S28R. INSTALLED EXTERNAL DOUBLER PER SRM 53-30-3.SDR 96ZZZX2121Stringer · crackedCLT - DURING A C-2 CHECK INSPECTION, VISUALLY FOUND A 1 INCH CRACK AROUND RIVET HOLE IN STR STA 503, S15L. REPAIRED PER SB. INSTALLED DOUBLER. BOEING SB 737-53-1145.SDR 96ZZZX2120Stringer · crackedCLT - DURING A C-2 CHECK INSPECTION, VISUALLY FOUND A 1 INCH CRACK AROUND RIVET HOLE IN STR STA 516, S15L. INSTALLED DOUBLER PER IAW SB 737-53-1145.SDR 96ZZZX2119Stringer · crackedCLT - DURING A C-2 CHECK INSPECTION, VISUALLY FOUND A 1 INCH CRACK AROUND RIVET IN STR STA 503, S15R. STRINGER CHANNEL AND TIE REPAIR PER BOEING 737-53-1145.SDR 95ZZZM616Fire Loop · brokenNR 2 ENGINE FIRE WARNING STARTED FLICKERING AND EVENTUALLY CAME ON STEADY. CAPTAIN PULLED BACK THROTTLE, NO HELP. SHUT DOWN ENGINE, NO HELP. FIRED ONE FIRE BOTTLE, NO HELP. DURING DESCENT, LIGHT FLICKERED AGAIN AND WENT OUT. FOUND BOTTOM FIRE LOOP FORWARDSDR 95ZZZM615Dn Lock Act · brokenNOSE GEAR WOULD NOT EXTEND NORMALLY, MANUALLY EXTENDED OK. GOOD DOWN AND LOCKED INDICATION. DOWN LOCK ACTIVATOR WAS BROKEN. (M)SDR 95ZZZX6378Fire Loop · malfunctionedMIA/PIE - ON CLIMB-OUT OF MIA TO PIE, CREW GOT A NR 2 ENGINE FIRE INDICATION. C/W SPECIAL PROCEDURE, SHUT DOWN ENGINE, AND FIRED BOTTLE. LANDED IN PIE. INSPECTED, FOUND LOWER LOOP DETECTOR BAD. REPLACED LOOP, FIRE BOTTLE, AND SQUIBS.SDR 95ZZZX4282Eel Cover · missingDURING AN INSPECTION, THE EMERGENCY FLOOR LIGHTING AT FORWARD GALLEY WAS MISSING APPROXIMATELY A 10 INCH STRIP PLASTIC COVER DUE TO PASSENGER STEPPING ON IT. INSTALLED AND SECURED FLOOR STRIP. FLOOR LIGHT OPS CHECKED GOOD PER M/M 33.SDR 95ZZZM620Escape Slide · tornESCAPE SLIDE AT POSITION L1 FRAYED AND TORN AT THE GIRT AREA. REMOVED AND REPLACED SLIDE, NOT RUBBING NOTED ON SCUFF PLATE.SDR 95ZZZM619Pbe · tornFORWARD AND AFT GALLEYS HAVE ONE EACH PBE'S UNSERVICEABLE DUE TO HOLE TORN IN CASE ONE AND LATCH BROKEN ON OTHER. REMOVED AND REPLACED PBE'S AND SECURED WELL WITH VELCRO STRAP.SDR 95ZZZM618Latch Cable · misroutedALL EMERGENCY ESCAPE SLIDES LATCH CABLE NOT PROPERLY ROUTED. REMOVED AND REPOSITIONED CABLE.SDR 95ZZZX4280Eel Socket · inopDURING INSPECTION, FOUND THE EMERGENCY PASSENGER LIGHTING SYSTEM WHITE LIGHT INOP BETWEEN ROWS 1 AND 2. BAD SOCKET WAS FOUND AND REPLACED. OPS CHECKED GOOD.SDR 95ZZZM617Overheat · defectiveNR 2 ENGINE OVERHEAT LIGHT ILLUMINATED EN ROUTE TO PIE FROM MIA. FOUND DEFECTIVE OVERHEAT LOOP NR 2 ENGINE. REMOVED AND REPLACED OVERHEAT LOOP NR 2 ENGINE, OPS CHECKED GOOD. (M)SDR 95ZZZW785Skin · crackedDURING WALKAROUND INSPECTION A CRACK WAS NOTED ON THE RIGHT WING NR 3 SLAT. THE CRACK WAS LOCATED ON THE UPPER SURFACE OUTBOARD TRAILING EDGE CORNER. THE CRACK WAS 6 INCHES IN LENGTH IN ADDITION, THE SLAT UPPER SKIN WAS DELAMINATED APPROXIMATELY 10 PERCENT. SDR 95ZZZX2027Relief Valve · missingDURING ROUTINE A-3 CHECK, NR 1 ENGINE MAIN OIL FILTER CHANGE, DISCOVERED OIL PRESSURE RELIEF VALVE ASSEMBLY WAS NOT INSTALLED. REPLACED PRESSURE RELIEF VALVE, PN 710170, RETAINING RING, PN 728373, KEY WASHER, PN 695395, AND GASKET, PN 6-961.SDR 95ZZZW346Eel Bulb · failedLEFT FORWARD ENTRY DOOR (EXTERIOR) EMERGENCY SLIDE LIGHT INOP. RELAMPED BURNED OUT BULB, OPS CHECK NORMAL IAW MM 33-51-11 AND 33-51-21. (W)SDR 95ZZZX1741Pcu · malfunctionedWITH REFERENCE TO AD T95-06-53. AIRTRAN AIRWAYS, INC., RECEIVED RUDDER PCU PN 65-44861-5, SN 855A OVERHAULED BY NORTEK REPAIR CENTER, INC., FAA. , REPAIR STATION NR YA4R667M. THE RUDDER PCU ON AIRCRAFT EI-CJW (TAT 36,134.6 AND TAC 44104) WAS REMOVED AND REPLSDR 95ZZZW347Actuator · brokenNOSE GEAR DOWNLOCK ACTUATOR UPPER ATTACH FITTING BROKEN. REMOVED AND REPLACED DOWNLOCK ACTUATOR IAW MM 32-33-21. (W)SDR 95ZZZX720Pt7 Tube · fracturedNR 2 ENGINE EPR INDICATION APPEARS LOW DURING GROUND RUN-UP. INVESTIGATION FOUND PT7 TUBE ASSEMBLY WAS BROKEN ON B-NUT. REPLACED TUBE ASSEMBLY PER PRATT AND WHITNEY MM 78-22-00.SDR 95ZZZW348Eel Bulb · failedLAST AFT RED SECTION OF FLOOR PROXIMITY LIGHTING INOP. RELAMPED BURNED OUT BULB. OPS CHECK NORMAL. (W)
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