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 DU4R2020051800016Stringer Clip · crackedAD 2019-08-02(H) PART 2 AND BOEING SB 737-53A1360, IR PART 2 INSPECTION FIGURE 7,8,13 AND 14, STRINGER CLIP IS CRACKED VERTICAL FLANGE INBOARD HOLE S16L FORWARD SIDE OF FR BS747SDR DU4R202005180015Support Plate · crackedFORWARD LOWER CARGO COMPARTMENT R/H SIDE STR 26R SIDE PLATE CRACKED AT B.S. 500SDR 2020F00292Tear Strap · corrodedNON-ROUTINE 2794N750 DISCREPANCY. TEAR STRAP CORROSION AT STA 360 BETWEEN 28L-28R. CORRECTIVE ACTION COMPLIED WITH EA PD 37-53-3145 WITH NO DEVIATIONS IAW 8110-3.SDR 2020F00291Frame · corrodedNON-ROUTINE 2794N743 DISCREPANCY. CORROSION AT FRAME 360 STR 28L-28R BL0. CORRECTIVE ACTION REMOVED CORROSION AND REPAIRED FRAME AT STA 360 28L-28R BL-0 IAW EA PD37-53-3145 AND SRM 51-40-02. PER APPROVED 8110-3.SDR 2020F00290Frame · corrodedNON-ROUTINE 2794N743 DISCREPANCY. CORROSION AT FRAME 360 STR 28L-28R BL0.SDR K11A2020041101Power Supply · dischargedDURING A CHECK FOUND R1 & L1 DOOR EMERGENCY LIGHTING INOPSDR K11A2020032673301Skin · corrodedEVIDENCE OF CORROSION, DUE TO SKIN BULGING, BETWEEN RH HORIZONTAL REAR SPAR UPPER CHORD AND UPPER SKIN @ R/H HORIZONTAL STAB STA 270SDR K11A2020021240504Flashlight · inoperative2 EA. FLIGHT ATTENDANT, CAPTAINS, & 1ST OFFICERS EMERGENCY FLASHLIGHTS DO NOT BLINKSDR K11A2020021240503Frame · crackedUPPER EDGE OF FRAME HAS A CRACK AFT PIT BILGE STA 727B BL 0SDR K11A2020021240502Frame · crackedFRAME CRACKED IN AFT PIT AT EXISTING TOOLING HOLE STA 967 RBL 1SDR K11A2020021240501Light · inoperativeEXIT LIGHT FWD OF R1 DOOR DOES NOT ILLUMINATESDR NACA2020010824177Stringer Clip · crackedBS727A, S20L CRACKED STRINGER CLIP. REPLACED CRACKED STRINGER CLIP AT STA 727A, STR 20L WITH NEW PART, PN 69-35352-2 IAW B737-400 SRM 51-40-02, REV 104 AND BOEING DWG #65-46595 REV K.SDR NACA2020010800176Frame · crackedBS500F, S20L - S21L, 1.04" WIRING PENETRATION HOLE CRACKED IN FRAME WEB. REPAIR IAW SB 737-53A1279 B737-400, 53-00-07 REPAIR 20SDR NACA2019122400175Frame · crackedBS500B, S21R - S22R TOOLING HOLE CRACKED IN FRAME. CONTACT BOEING ENGINEERING, SDR STILL OPENSDR NACA2019122400174Skin · crackedBS340, WL208 3 CRACKS FOUND AT L1 DOOR AFT LOWER CORNER ON FUSELAGE SKIN. CONTACT PEMCO ENGINEERING, SDR STILL OPENSDR NACA2020010800173Bulkhead · crackedCRACK FOUND ON BS178 BULKHEAD WEB AT LBL5.7 BETWEEN WL207 AND WL195. REPAIR PER SRM 53-10-08 REPAIR 10SDR NACA2020010800172Probe · corrodedRIGHT HAND ELEVATOR FEEL PITOT PROBE DAMAGED/CORRODED. REPLACED L/H ELEVATOR FEEL PITOT PROBE PN: 0851CM-2 SN: 167646 WITH NEW PITOT PROBE PN: 0851CM-2 SN: 166550 IAW B737-400 AMM 27-31-94 REV 90 SEE ATTACHED MTC-114 FOR SYSTEM TESTS AND DETAILS.SDR NACA2020010800171Probe · corrodedLEFT HAND ELEVATOR FEEL PITOT PROBE DAMAGED/CORRODED. REPLACED L/H ELEVATOR FEEL PITOT PROBE PN: 0851CM-2 SN: 167646 WITH NEW PITOT PROBE PN: 0851CM-2 SN: 166550 IAW B737-400 AMM 27-31-94 REV 90 SEE ATTACHED MTC-114 FOR SYSTEM TESTS AND DETAILS.SDR NACA2020010800170Floorbeam · crackedBS660 - BS666, FLOOR BEAM LOWER CHORD, LBL24.82 CRACK INDICATION IN FORWARD HOLE. RBL24.82 CRACK INDICATIONS IN FORWARD AND AFT HOLES. UPSIZE TO REMOVE CRACK IAW SB737-57A1296SDR NACA2020010800169Intercostal · crackedBS279, S14R, CRACK FOUND ON FORWARD RADIUS TRIM OUT OF INTERCOSTAL (NDT HAS VERIFIED). REPLACED INTERCOSTAL AT STA 279 STR 14R WITH NEW PART IAW B737-400 SRM 51-10-02 REV 104 AND INSTALLED IAW B737-400 SRM 51-40-02 REV 104. INSTALLED PART NUMBER 65-45807-8 IASDR NACA2020010800168Bracket · crackedBS332.1, S8R, INTERCOSTAL T-BRACKET FOR DOOR STOP #1 CRACKED IN LOWER RADIUS. (VERIFIED BY NDT). AFT SIDE OF R1 DOOR. REPLACED STA 332.1 STR 8R, INTERCOSTAL T-BRACKET FOR DOOR STOP #1 AFT SIDE OF R1 DOOR IAW BOEING DOC# 65-45813 REV AC & INSTALLED IAW B737-40SDR NACA2020010800167Skin · crackedRIGHT HAND LOWER HORIZONTAL STABILIZER SKIN, HSS142, ZONE "C" FORWARD OF REAR SPAR, SKIN CRACKED. REPAIRED R/H LOWER H-STAB SKIN. SSTA 147.9 ZONE "C" FWD OF REAR SPAR IAW BOEING SB 737-55-1059 FIG. 4 REV. 1 DATED APRIL 6, 2016.SDR NACA2020010800166Skin · corrodedLEFT HAND HORIZONTAL STABILIZER UPPER SKIN BLISTERED @ AFT SPAR @ ES149. REPAIRED LH H-STAB UPR SKIN @ AFT SPAR @ ELEV STA 149 IAW SR# 4-4652338756, WITHOUT DEVIATION.SDR NACA2019122400165Support Fitting · crackedLEFT HAND MAIN LANDING GEAR SUPPORT FITTING, #5 HOLE IS CRACKED IN 2 PLACES. DETERMINE WHICH LAYER CRACK IS IN. SDR STILL OPEN FOR FINAL FIX.SDR NACA2019122400164Support Fitting · crackedRIGHT HAND MAIN LANDING GEAR BEAM FORWARD SUPPORT FITTING 2 CRACKS FOUND, MOST INBOARD UPPER 2 HOLES (MARKED ON AIRCRAFT). REPAIRED 2 CRACKS FOUND DURING RH MLG BEAM FWD FITTING INSPECTION IAW BOEING SR#4-4628443870. SEE FAA FORM 8100-9 FOR APPROVAL.
RII DSDR NACA2020010800163Spar · corrodedFRONT SPAR LEFT HAND UPPER WING SURFACE WS246 CORROSION. L/H UPPER WING SURFACE W.S. 246, FRONT SPAR, REPAIRED IAW BOEING SERVICE REQUEST 4-4649225247, SEE 8100-9 FOR FINAL APPROVAL.SDR NACA2019122400162Structure · crackedPOSSIBLE CRACK BS290 S11R - S12R, RIGHT HAND ON OUTER CHORD. REPLACED CRACKED OUTER CHORD AT STA 290 STR 11-12 RH WITH PART NUMBER 65-45807-31 IAW BOEING DWG #65-45807 REV K.SDR NACA2019122400161Intercostal · crackedBS867 - BS887 RBL22.5 INTERCOSTAL CRACKED. REPLACED CRACKED INTERCOSTAL AT STA 867-887 RBL 22.5 IAW B737-400 SRM 51-40-02 REV 103. PN INFO NEEDED, STILL OPENSDR NACA2019122400160Structure · crackedBS727 S18A RIGHT HAND CRACK CONFIRMED IN CHORD. REMOVE AND REPLACE IAW BOEING SB737-53-1088 REV 1 AND BOEING DWG 65C33722. REMOVED AND REPLACED CHORD AT STA 727, RH SIDE, STRINGER 17- 26R IAW BOEING SERVICE BULLETIN 737-53-1088 REV 1, DATED MAY 25, 2006 AND BSDR NACA2020010800159Structure · crackedBS727 S18A LEFT HAND CRACK CONFIRMED IN CHORD. REMOVE AND REPLACE IAW BOEING SB737-53-1088 REV 1 AND BOEING DWG 65C33722. REMOVED AND REPLACED CHORD AT STA 727, LH SIDE, STRINGER 17- 26L IAW BOEING SERVICE BULLETIN 737-53-1088 REV 1, DATED MAY 25, 2006 AND BOESDR NACA2019122400158Stop Fitting · crackedAD2018-18-03 REVEALED CRACKED #5 DOOR STOP FITTING ON FORWARD AIRSTAIR DOOR. RE&RE DOOR, REPLACE STOP FITTING, RIG DOOR & STOPS IAW SB737-53A1370 APPENDIX A. DATED DEC 13, 2017. ORIGINAL ISSUE. NEED PART INFO, STILL OPENSDR NACA2019122400157Fitting · crackedLEFT HAND ENGINE REAR ENGINE MOUNT HANGAR FITTING HAS PITTING CORROSION IN CONE BOLT MATING SURFACE. REPLACED #1 ENGINE REAR MOUNT HANGAR FITTING IAW B737-400 AMM 71-21-03 REV 90. SEE NDT REPORT NDT19-5645 FOR HANGAR BOLT INSPECTION. NO CRACKS FOUND. NEEDS PASDR NACA2019123024156Support · corrodedBS 867 - 930, RBL21 SUPPORT ZEE WAS CORRODED AT VARIOUS PLACES, UPPER AND LOWER SIDE IN THE AFT CARGO BAY. BLENDED CORROSION IAW SRM 51-10-02 PAR.14, REV 103. NOMINAL MATERIAL THICKNESS WAS .040" IAW SRM 53-60-53 DETAIL 1, FIGURE 1, REV 103. MINIMUM REMAININSDR NACA2019123024155Channel · corrodedBS 927 - 947, RBL 13.8 IN THE AFT CARGO BAY, THE FLOOR CHANNEL WAS CORRODED AT VARIOUS PLACES. REPLACED THE CHANNEL IAW SRM REV 103, 51-10-02, PARA 8 AND 65-46592, REV A.SDR NACA2019123024154Channel · corrodedBS 727A + 5.0 RBL3.0 AFT CARGO FLOOR CHANNEL CORRODED. REPAIRED THE CHANNEL IAW SRM 53-00-53, REV 103.SDR NACA2019123024153Channel · corrodedBS 727F + 5, RBL 8.1, AFT CARGO FLOOR CHANNEL CORRODED. THE CHANNEL WAS BLENDED IAW SRM 51-10-02, PARAGRAPH 14, REV 103. ORIGINAL MATERIAL THICKNESS 0.080" IAW SRM 53-60-53 REV 103. THICKNESS REMOVED 0.036", THICKNESS REMAINING 0.042", THE CHANNEL WAS FOUNSDR NACA2109123024152Bolt · corrodedLEFT WING OUTBOARD FLAP OUTBOARD GIMBAL BUSHING RETENTION BOLT CORRODED. REPLACED THE LEFT WING OUTBD FLAP OUTBAORD GIMBAL BUSHING AND RETENTION BOLT IAW AMM 27-51-37 REV 90.SDR NACA2019123024151Bushing · wornLEFT WING OUTBOARD FLAP, OUTBOARD FOREFLAP SEQUENCE CARRIAGE HARDWARE WAS CORRODED AND BUSHINGS WORN. THE HARDWARE & BUSHINGS WERE REPLACED IAW AMM 27- 51-37 C (2) (A), REV 90.SDR NACA2019123040150Access Panel · corrodedRIGHT HORIZONTAL STABILIZER LOWER SURFACE ACCESS PANEL 9222R AT HSS 56.01 WAS CORRODED UNDER AND AROUND ANCHOR NUTS. REPLACED THE ACCESS PANEL IAW SRM 51-30-01, REV 104. AND DWG 6553746, REV H.SDR NACA2019123040149Panel · corrodedLEFT VERTICAL STABILIZER PANEL 9566L CORRODED ON LOWER SURFACE. REPLACED THE PANEL IAW SRM 51-30-01 REV 104, AND SRM 51-40-02 REV 104.SDR NACA2019123040148Strap · corrodedRIGHT HORIZONTAL STABILIZER PANEL 9223R MACHINED STRAP WAS CORRODED ON BOTTOM OF PANEL. REPLACED THE STRAP IAW DWG 65-53746, REV N, AND SRM 51-40-02, REV 104.SDR NACA2019122400147Skin · corrodedWS150 STRINGER 13 LEFT HAND WING UPPER SURFACE HAS SURFACE CORROSION. L/H UPPER WING SURFACE REPAIRED @ WS 150-112, STR 13U-15U IAW BOEING SERVICE REQUEST 4-4649225247, SEE 8100-9 FOR FINAL APPROVALSDR NACA2019123040146Skin · corrodedWS271, STRINGER 13 LEFT HAND WING UPPER SURFACE HAS SURFACE CORROSION. LEFT HAND WING UPPER SURFACE, WS 232 STR 13, REPAIRED IAW BOEING SERVICE REQUEST 4-4649225247, SEE 8100-9 FOR FINAL APPROVALSDR NACA2019123040145Door · corrodedAFT PORTABLE WATER DOOR SHOWS EVIDENCE OF CORROSION. REPLACED AFT TOILET SERVICE DOOR WITH NEW IAW AMM 52-49-07, REV 90. BONDING CHECK SERVICEABLE.SDR K11A2019112977401Proximity Switch · faultyON GEAR RETRACTION RIGHT MAIN GEAR UNSAFE LIGHT REMAINED ILLUMINATED. CORRECTIVE ACTION: R&R RIGHT MAIN GEAR UPLOCK PROXIMITY SWITCH IAW AMM 32-61-21, PERFORMED OPS CHECK AND GEAR SWING IAW AMM 32-61-21SDR K11A2019111573401Controller · inoperativeDURING CLIMB OUT AT 14,000 FT CABIN PRESSURE GOES TO 10,000 FT IN STAND BY AND AUTO MODESSDR K11A2019102273401Damper · damagedUPON LANDING RIGHT HAND MAIN LANDING GEAR TORSION LINK BROKE, CORRECTIVE ACTION & OTHER PERTINENT INFORMATION: R&R THE MAIN LANDING GEAR UPPER AND LOWER TORSION LINK, TORSION LINK PIN, LEFT HAND SHIMMY DAMPER, #3 & #4 MWA, #3 BRAKE LINE, #4 BRAKE LINE AND NUMSDR K11A2019072040501Regulator · malfunctionedDURING CLIMB THE #2 BLEED TRIP OFF LIGHT ILLUMINATED. R&R HIGH STAGE REGULATOR IAW AMM 36-11-86. GROUND OPS AND LEAK CHECKED GOOD.SDR K11A2019062473301Tab · crackedR/H ELEVATOR TAB LOWER SIDE @ ELE STA 34.25 CRACKEDSDR NACA201903270031Warning System · false activationFIRE WARNING, MASTER CAUTION LIGHT & BELL ACTIVATED FOR APPROXIMATELY 1 SECOND THEN SELF CLEARED. FIRE WARN/MASTER CAUTION LIGHT & BELL ACTIVATED UNTIL CANCELLED. UPON RECALL, FIRE WARN REMAINS OFF, MASTER CAUTION ILLUMINATES. PERFORMED AMM 26-11-00 ON THE EN
Back to Boeing 737-436