Boeing 737-436
Service difficulty reports · 390
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 = '737436' 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 = '737436' 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 NACA2024042600002Angle · crackedMAIN ENTRY DOOR LOW AFT CORNER SCUFF PLATE ANGLE CRACK. 1EA.SDR NACA2024042400002Frame · crackedDO HFEC INSP. FOUND FRAME INTEGRAL INBOARD CHORD CRACKED ABOUT 0.2" IN LENGTH AT BS 380 BETWEEN S-20L AND S-21L AS MARKED.SDR NACA2024042400001Frame · damagedDO HFEC INSP. FOUND FRAME STANDOFF/TOOLING HOLE EDGE CRACKED ABOUT 0.2" IN LENGTH AT BS 500D S-21L AS MARKEDSDR NACA2024041800001Skin · bulgedBULGED (3.0" X 3.0") AT LH SIDE FUSELAGE EXTERNAL SKIN AT STA 1104, S-6L.SDR NACA2024041600005Beam · corrodedCORROSION(3.0" X 3.0") AT LH HORIZONTAL STABILIZER TRAILING EDGE BEAM UPPER SURFACE AT STAB STA 168.SDR NACA2024041600004Strap · corrodedCORROSION ON NO.2 ENG LH THRUST REVERSER AFT COWL PANEL FRAME-STRAP AT 7 O'CLOCK POSITION.SDR NACA2024041600003Support Angle · crackedLH WING T/E UPPER PANEL SUPPORT ANGLE WAS CRACKED , WBL 84.24.SDR NACA2024041600002Support Angle · corrodedLH WING T/E UPPER PANEL SUPPORT ANGLE WAS CORRODED , WBL 185.SDR NACA2024041500003Angle · crackedTWO EA "L" ANGLES CRACK ON RH NACELLE NAC.STA.278.52 AT WBL.192 AND WBL.204SDR NACA2024041200002Seat Track · crackedPILOT SIDE SEAT TRACK CRACK ON FWD I.B STOP STUD AREA.SDR NACA2024041100007Plug · corrodedCORROSION AT LH WINDOWS PLUG PANE , BETWEEN STA907 AND STA927 (L:2",W:0.5")SDR NACA2024041100006Seal · corrodedLH AFT OVERWING EMER EXIT HATCH LOW PORTION CORROSION AROUND DOOR SEAL AREA..SDR NACA2024041100005Panel · bulgedBULGE ON NO.1 ENG LH THRUST REVERSER UPPER BIFURCATION PANEL AT NAC STA 256SDR NACA2024041000001Support · corrodedRH MLG CENTER DOOR UPPER SHOCK STRUT DOOR SUPPORT LINK CORRODED.SDR NACA2024022100005Seat Track · crackedPILOT SEAT TRACK CRACK ON FWD INBORD, LOCATED END OF TRACK AROUND FWD STOP SCREW HOLE. 1. REMOVE PILOT SEAT CRACK TRACK 2. INSTALL PILOT SEAT NEW TRACK COMPLETED REF: AMM 53-42-00 P1. 20-50-11 PAGE 201 R98 PME: 006162 DUE DATE: JUL 06 2024SDR NACA2024022100004Battery · dischargedRECHARGE EMERGENCY LIGHTS BATTERY PACKS , FOUND EMERGENCY LIGHTS BATTERY PACK MALFUNCTION , PACK:M01133. REPLACE THE EMER BATTERY PACK AND TEST NORMAL REF AMM 33-51-51-962-015 REV98SDR NACA2024022100003Battery Pack · dischargedRECHARGE EMERGENCY LIGHTS BATTERY PACKS , FOUND EMERGENCY LIGHTS BATTERY PACK MALFUNCTION , PACK:M01132. REPLACE THE EMER BATTERY PACK AND TEST NORMAL REF AMM 33-51-51-962-015 REV98SDR NACA2024020600002Skin · crackedTHE CRACK WAS FOUND AT #3 SLAT OUTER SKIN SS.S. 88.4 AND S.S. 94.4 AREA. PERFORMED REPAIR AT #3 SLAT OUTER SKIN 55.88.4 & 94.4 AREA. I.A.W. B737-400 SSRM 57-43-01 REPAIR 6 PAGE 201-205 (REV.115) & DMG 65C26603SDR NACA2024020500001Warning Message · activatedTO CONFIG WARNING ANNUNCIATED ON TAKEOFF. CYCLED SPEEDBRAKE HANDLE AND TAKEOFF WARNING TEST GOOD OK IAW AMM 32-09-00.SDR NACA2024020200002Skin · crackedACCORDING TO AD 2019-08-03 INTERNAL OPEN HOLE HFEC INSPECTION , 2 EA FASTENERS HOLE SKIN CRACKED(UP L: 0.4" LOWER L:0.35") AT BS380 IB CHORD BETWEEN S20L AND S21L. REPAIRED DAMAGED CHORD AT BS 380L BETWEEN STRANGER S21 & S22 AS PER NAC EO 737-53-3507 REV. IRSDR NACA2024020100005Web · crackedA CRACK AT WEB FASTERNER HOLE, STA 710 LBL 0.07, LENTH:0.250". 1. REMOVE THE STIFFENER & FILLER 2. CUT-OUT THE WEB FROM DAMAGED AREA 3. INSTALL REPAIR KIT (NEW, DOACER & WEB) 4. ALL ASSY REINSTALL WITH SEALANT PER: SB 737-57-1210 FIG 5 PAGE 86, PEMCO EA PD 37-SDR NACA2024020100004Skin · dentedDENT (3.2" X 2.0" IN AREA, MAX. DEPTH= 0.080") AT BS STA 1148, RBL+4". PERFORM PERMANENT REPAIR AT BS STA 1148 RBL+4" PER NAC EO737-53-0336SDR NACA2024013000002Skin · corrodedDURING NRC:CA1528/152 , CORROSION WAS FOUND AT LH WING UPPER SURFACE , WBL79 , S-11 AREA. REMOVED CORROSION LEVEL 2 AT LH WING UPPER SURFACE WBL 83,S11 AREA FROM P/N 65C25204-15 ORIGINAL THICKNESS 0.160" REMOVES 0.028"AND REMAINING THICKNESS IS 0.132" IS OVER SDR NACA2024012900004Skin · dentedDENT ( 7.0" X 2.0" IN AREA, MAX DEPTH =0.120") AT RH HROIZONTAL STABILIZER LEADING EDGE AT STAB STA 186~193. PERFORMED PERMANENT REPAIR AT RH HORIZONTAL STABILIZER LEADING EDGE AT STAB STA 186~190 CATEGORY A PER: 737-400 SRM 55-70-01 REPAIR 3 (R115)SDR NACA2024012900003Torque Box · corrodedCORROSION AT APU RH SIDE LOWER TORQUE BOX AT STA 1126. TEE ANGLE REPLACED AT APU RH SIDE LOWER TORQUE BOX AT STA 1126 PER: DRAWING 65-46579 SHEET 4 #531, SRM 51-40-02 PARA 4 R115SDR NACA2024012900002Skin · dentedTHE DENT WAS FOUND AT #3 SLAT OUTER SKIN S.S.55 AREA , L:2.6 INCH , W:1.3 INCH , Y (DEPTH OF DENT) :0.076 INCH . PER SRM 57-43-01 ALLOWABLE DAMAGE 1 , A/Y: 1.3/0.076=17.1 , OVER LIMIT.
PERFORMED REPAIR AT #3 SLAT OUTER SKIN 5.5.55 AREA, 2:2.6", W:1.3". I.A.WSDR NACA2024012900001Skin · crackedTHE CRACK WAS FOUND AT #1 SLAT OUTER SKIN S.S.299.53 ,L:0.1 INCH. PERFORMED REPAIR AT #1 SLAT OUTER SKIN 5.5.299.53, L: 0.1INCH. I.A.W.B737-400 SRM 57-43-01 REPAIR 6 PAGE 201-205 (REV.115) & DWG 65C26601SDR NACA2024012600005Retainer · corrodedOVERWING ENERGENCY HATCH SEAL RETAINER HAS BEEN CORRODED AROUND LOWER PORTION OF THE DOOR. RH FWD(2415R). 1. CORROSION REMOVED. THE SEAL RETAINER AND LOWER PORTION WERE OVER LIMIT 2. CUT-OUT THE DAMAGED AREA AND MADE REPAIR PARTS AND INSTALL WITH SEALANT. 3. SDR NACA2024012600004Retainer · corrodedOVERWING ENERGENCY HATCH SEAL RETAINER HAS BEEN CORRODED AROUND LOWER PORTION OF THE DOOR. LH FWD(2414L). 1. CORROSION REMOVED. THE DOOR LOWER PORTION & SEAL RETAINER WERE OVER LIMIT. 2. CUT OUT THE DAMAGED AREA & MADE REPAIR PARTS AND INSTALL WITH SEALANT. PSDR NACA2024012600003Retainer · corrodedOVERWING ENERGENCY HATCH SEAL RETAINER HAS BEEN CORRODED AROUND LOWER PORTION OF THE DOOR. LH AFT(2403L). OVERWING EMERGENCY HATCH SEAL RETAINER HAS BEEN CORRODED AROUND LOWER PORTION OF THE DOOR, RH AFT (2404R). 1. CORROSION REMOVED. THE DOOR LOWER PORTION SDR K11A2024020200257Tie Down · crackedAFT CARGO COMPARTMENT B.S 727D RBL 14 HAS CRACK ON TRACK TIE DOWN LWR LEG.SDR NACA2024012400002Skin · debondedRH WING O/B AFT FLAP DISBOND BETWEEN WBL.230.68 ~ WBL.234.68 .(L:4 INCH , W:0.3 INCH). PERFORMED CATEGORY A REPAIR OF A DISBOND AT THE EDGE OF ALUM HONEYCOMB STRUCTURE, RH WING O/B AFT FLAP BETWEEN WBL 230.68~WBL 234.68 I.A.W. B737-400 SRM 57-53-02-2R-2 & SRSDR K11A2024012400251Controller · failedDURING TAKEOFF ROLL ALL AIR DATA INFORMATION ON F/O SIDE NO ANALOG AIRSPEED, DIGITAL AIRSPEED, AC ALTIMETER, NO VSI, AND VAU WOULD NOT ENGAGE. DURING TAKEOFF CLIMB, FWD ENTRY LIGHT ILLUMINATED. CABIN ALT UNCONTROLLABLE IN AUTO MODE. ALL OF THESE RELATE TO TSDR NACA2024011700001Actuator · crackedSYSTEM A HYDRAULIC FAILURE. FOUND 1 EACH SPOILER ACTUATOR CRACKED/SPLIT OFF AT TOP OF ACTUATOR. REPLACED ACTUATOR IAW AMM 27-12-74 OPS AND LEAK CHECK GOOD. NO TIME INFO, PART UNKNOWN TO TRAX.SDR K11A2024022600259Torque Box · corrodedEVIDENCE OF CORROSION ON UPPER WEB AROUND NUTPLATES AT APROX STA 1104 INSIDE LH TORQUE BOX.SDR K11A2024012400252Skin · delaminatedLH WING IB AFT FLAP IB SECTION HAS DELAMINATION.SDR K11A2024020200256Tie Down · corrodedAFT CARGO COMPARTMENT AT B.S. 727D RBL 14, EVIDENCE OF CORROSION AT CARGO TIE DOWN.SDR NACA2023122200002Smoke Detector · failedLAVATORY SMOKE ALARM ACTIVATED IN FLIGHT, RESULTING IN MI @ 1740Z. DEFERRED PER MEL 26-16-02 CAT D. LAV SMOKE DETECTOR REMOVED AND REPLACED. PART INFO UNKNOWN TO TRAX.SDR NACA2023120700006Unknown · unknownIN FLIGHT 2020Z AT FL360 SMOKE IN CABIN. DECLARED EMERGENCY WITH ATC ASK FOR DIRECT KRFD. LF RECIRC FAN FOUND SHORTING AND POPPING CIRCUIT BREAKER. DEFERRED LH RECIRC FAN PER MEL 21-31-05.SDR K11A2024012500254Unknown · corroded#2 PYLON HAS EVIDENCE OF CORROSION ON TOP SIDESDR K11A2024012500253Skin · corroded#1 PYLON HAS EVIDENCE OF CORROSION ON TOP SIDESDR NACA2023112800001Power Supply · failedOPERATIONAL TEST FOUND THE EMERGENCY LIGHT FAILURE, EQUIP.NO: M1675, S/N:32476. REPLACED THE EMERGENCY LIGHT POWER SUPPLY REF AMM 33-51-51-962-016.SDR K11A2023120700245Mount Fitting · crackedL/H WING GROUND SPOILER INBOARD ACTUATOR MOUNT FITTING CRACKED.SDR K11A2023112900244Tie Down · corrodedAFT CARGO COMPARTMENT STA 947 RBL 14 TRACK TIE DOWN HAS EVIDENCE OF CORROSION.SDR K11A2023112800243Channel · corrodedAFT CARGO COMPARTMENT STA 947 LBL 3 FLOOR CHANNEL HAS EVIDENCE OF CORROSION.SDR K11A2023112700240Channel · corrodedAFT CARGO COMPARTMENT STA 947 RBL 3 FLOOR CHANNEL HAS EVIDENCE OF CORROSION.SDR K11A2023112700239Channel · corrodedAFT CARGO COMPARTMENT STA 812 RBL 8 FLOOR CHANNEL HAS EVIDENCE OF CORROSION.SDR K11A2023112700242Floor Support · corrodedFWD GALLEY APPROX STA 300 LBL 11 FLOOR SUPPORT HAS EVIDENCE OF CORROSION.SDR K11A2023112700241Floorbeam · corrodedFWD GALLEY APPROX STA 312 LBL 11 FLOOR BEAM HAS EVIDENCE OF CORROSION.SDR NACA2023102600001Unknown · unknownCABIN WINDOW FRAME GOT CORROSION ON STA 767+10 (R33) 1. BS767+7 S-11R+1.5'' 2. BS767+16 S-11R+13''. REPAIRED PER SRM 56-20-02
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