Boeing 737-76Q
Service difficulty reports · 1,627
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 = '73776Q' 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 = '73776Q' 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 SWAA2026042890560Web · crackedAPB APEX DOME HAS SURFACE WEB CRACK AT STR23R FROM UPPER LH RIVET GOING TO CENTER EDGE OF DOME. REPAIRED PER EA 26-153-01061 WITH AN INSPECTION THRESHOLD DEFINED IN 26-153-01061-DTI..SDR SWAA2025122955746Regulator · low pressureAT FL250 CABIN PRESSURE DROPPED TO -4000 PSI; ALT HORN SOUNDED. RAN QRH PRESSURE WAS CONTROLLED IN MANUAL. INSPECTED BOTH CARGO DOOR PRESSURE SEALS IAW MM 52-09-11, NO DEFECTS NOTED. PRESSURIZED ACFT TO 4.5 PSID, NO ABNORMAL LEAKS NOTED IAW MM 21-31-00. ASDR SWAA2025122956227Regulator · low pressureAT FL250 CABIN PRESSURE DROPPED TO -4000 PSI; ALT HORN SOUNDED. RAN QRH PRESSURE WAS CONTROLLED IN MANUAL. INSPECTED BOTH CARGO DOOR PRESSURE SEALS IAW MM 52-09-11, NO DEFECTS NOTED. PRESSURIZED ACFT TO 4.5 PSID, NO ABNORMAL LEAKS NOTED IAW MM 21-31-00. PESDR SWAA2025122956228Valve · low pressureAT FL250 CABIN PRESSURE DROPPED TO -4000 PSI, ALT HORN SOUNDED. RAN QRH PRESSURE WAS CONTROLLED IN MANUAL. INSPECTED BOTH CARGO DOOR PRESSURE SEALS IAW MM 52-09-11, NO DEFECTS NOTED. PRESSURIZED ACFT TO 4.5 PSID, NO ABNORMAL LEAKS NOTED IAW MM 21-31-00. SDR SWAA2025122956229Valve · low pressureAT FL250 CABIN PRESSURE DROPPED TO -4000 PSI; ALT HORN SOUNDED. RAN QRH PRESSURE WAS CONTROLLED IN MANUAL. INSPECTED BOTH CARGO DOOR PRESSURE SEALS IAW MM 52-09-11 NO DEFECTS NOTED. PRESSURIZED AIRCRAFT TO 4.5 PSID NO ABNORMAL LEAKS NOTED IAW MM 21-31-00. PSDR SWAA2025121651775Screw · missingLEFT OVERWING EMERGENCY EXIT DOOR HANDLE HOUSING MISSING SCREW LEFT OVERWING EMERGENCY EXIT DOOR HANDLE HOUSING MISSING SCREW. REPLACED LT OVERWING EMERGENCY EXIT DOOR HANDLE HOUSING SCREW IAW AMM 12-25-22.SDR SWAA2025090912957Fseu · faultedTRAILING EDGE FLAPS INOPERATIVE. FIM 27-59 TASK 808 CARRIED OUT. OHMED FOR CONTINUITY, SHORTS, INSULATION RESISTANCE & DAR TEST IAW WDM 27-53-21. NO FINDINGS. REPLACED FSEU IAW AMM 27-51-01. OPS CHECKED GOOD.SDR SWAA2025090210292Sensor · faultedAFTER PUTTING FLAP LEVER TO 5 THE FLAPS DID NOT EXTEND. WE NOTICED A VERY SMALL SPLIT IN THE TRAILING EDGE FLAPS. LE DEVICES WERE EXTENDED WITH THE ALTERNATE FLAP SWITCH PER QRH. THE LANDING WAS NORMAL AND UNEVENTFUL. R&R #8 FLAP SKEW SENSOR PER AMM 27-59-01.SDR SWAA2025082606374Cap · missingFORWARD CARGO DOOR HANDLE HAS MISSING STUD CAP. INSTALLED STUD CAP IAW AMM 52-31-14.SDR SWAA2025082206375Handle · missingAFT CARGO DOOR HANDLE HAS MISSING STUD CAP<[01] REMOVED AND REPLACED AFT CARGO DOOR HANDLE STUD CAP REFERENCE AMM52-31-14.SDR SWAA2025081804438Flap System · faultedAS WE WERE ABOUT TO SELECT FLAPS 1 (210KTS) WE NOTICED THE FLAP GAUGE INDICATING ZERO - ONE ON RT SIDE. WHEN WE SELECTED F1 THE FLAPS/SLATS DID NOT EXTEND. SELECTED F5, SAME RESULT. RETURNED FLAP HANDLE TO ZERO CHECKED CIRCUIT BREAKERS, ALL IN, AND EXECUTSDR SWAA2025081299599Girt Bar · damagedFWD ENTRY DOOR GURT BAR HOOK HAS MISSING RIVET. INSTALLED NEW RIVET IN FWD ENTRY GURT BAR HOOK REF SIPSDR SWAA2025062785458Skirt · out of positionAFT ENTRY DOOR SLIDE EXCESSIVE FABRIC<[01] REPOSITIONED AFT ENTRY SKIRT SLIDE PER AMM 25-66-01 AND TASK MT 725-61-06.SDR SWAA2025060276185Girt Bar · looseR1 DOOR GIRT BAR LOOSE <[01]. RE-SECURED R1 DOOR GIRT BAR RETAINER CLIPS PER AMM 25-66-01. OPS CHK GOOD.SDR SWAA2025051971778Slide · looseR1 SLIDE CAME LOOSE. REINSTALLED SLIDE PER MT#25-66-01.SDR SWAA2025050667536Sign · inoperativeCREW REPORTS OVER WING EMERGENCY EXIT INDICATOR LIGHT INOP. REMOVED AND REPLACED EXIT INDICATOR SIGN PER AMM 33-51-01.SDR SWAA2025050622175Battery Pack · inoperativeEMERGENCY EXIT LIGHTS ASSOCIATED WITH BATTERY PACK M2335 INOP<[01] REMOVED; REPLACED WITH SERVICEABLE UNIT AND PERFORMED GOOD INSTALLATION TEST OF EMERGENCY BATTERY PACK M2335 IAW AMM 33-51-06-960-805.;[02] VERIFIED CORRECTIVE ACTION #1SDR SWAA2025050608576Strip · crackedFWD CARGO BAY SIDEWALL PNL 122AW CAPSTRIP CRACKED<[01] RECEIVED NEW CAPSTRIP; CAPSTRIP WILL BE INSTALLED ON TTG8Q00YJCE7;[02] CORRECTIVE ACTION ITEM 1 VERIFIED; CARD COMPLETE.SDR SWAA2025050615939Strip · crackedFWD CARGO BAY SIDEWALL PNL 122EW CAPSTRIP CRACKED<[01] RECEIVED NEW CAPSTRIP; CAPSTRIP WILL BE INSTALLED ON TTG8Q00YJCE1;[02] VERIFIED CORRECTIVE ACTION ENTRY 1.SDR SWAA2025050615928Stringer Clip · crackedCRACKED STR CLIP AT PAX CABIN BS727D S-6L. MARKED<[01] REMOVED STR CLIP AT BS727D S-6L IAW SRM 51-40-02;[02] OK TO INSTALL;[03] REMOVED AND REPLACED NEW STRINGER CLIP AT BS727D S-6L PER DWG 146A1111 AND SRM 51-40-02.SDR SWAA2025050615929Stringer Clip · crackedCRACKED STR CLIP AT PAX CABIN BS727C S-7L. MARKED<[01] REMOVED SRT CLIP AT BS727C S-7L IAW SRM 51-40-02;[02] REMOVED AND REPLACED NEW STRINGER CLIP BS727C S-7L PER DWG 146A1103 REV D AND SRM 51-40-02.SDR SWAA2025050615930Stringer Clip · crackedCRACKED STR CLIP AT PAX CABIN BS727D S-4R. REMOVED STR CLIP AT BS727D S-4R IAW SRM 51-40-02. REMOVED AND REPLACED NEW STRINGER CLIP BS727D S-4R PER DWG 146A1111 AND SRM 51-40-02.SDR SWAA2025050615931Stringer Clip · crackedCRACKED STR CLIP AT PAX CABIN BS727A S-5R. REMOVED STR CLIP AT BS727A S-5R IAW SRM 51-40-02. REMOVED AND REPLACED NEW STRINGER CLIP AT BS727A S-5R PER DWG 146A1101 REV AND SRM 51-40-02.SDR SWAA2025050606638Stringer Clip · crackedCRACKED STR CLIP AT PAX CABIN BS727B S-5R. MARKED. REMOVED AND REPLACED NEW STRINGER CLIP BS727B S-5R PER DWG 146A1103 REV D AND SRM 51-40-02. CORRECTIVE ACTION ITEM 1 VERIFIED; CARD COMPLETE.SDR SWAA2025040906636Stringer Clip · crackedCRACKED STR CLIP AT PAX CABIN BS727D S-6L. MARKED <[01]. REMOVED STR CLIP AT BS727D S-6L IAW SRM 51-40-02; [02] OK TO INSTALL; [03] REMOVED AND REPLACED NEW STRINGER CLIP AT BS727D S-6L PER DWG 146A1111 AND SRM 51-40-02.SDR SWAA2025040906637Stringer Clip · crackedCRACKED STR CLIP AT PAX CABIN BS727C S-7L. MARKED <[01]. REMOVED SRT CLIP AT BS727C S-7L IAW SRM 51-40-02; [02] REMOVED AND REPLACED NEW STRINGER CLIP BS727C S-7L PER DWG 146A1103 REV D AND SRM 51-40-02.SDR SWAA2025040906639Stringer Clip · crackedCRACKED STR CLIP AT PAX CABIN BS727D S-4R. MARKED <[01]. REMOVED STR CLIP AT BS727D S-4R IAW SRM 51-40-02; [02] REMOVED AND REPLACED NEW STRINGER CLIP BS727D S-4R PER DWG 146A1111 AND SRM 51-40-02.SDR SWAA2025040906640Stringer Clip · crackedCRACKED STR CLIP AT PAX CABIN BS727A S-5R. MARKED <[01]. REMOVED STR CLIP AT BS727A S-5R IAW SRM 51-40-02; [02] REMOVED AND REPLACED NEW STRINGER CLIP AT BS727A S-5R PER DWG 146A1101 REV AND SRM 51-40-02.SDR SWAA2025050606464Skin · corrodedCORROSION ON UPPER FUSELAGE SKIN UNDER VERTICAL STAB LBL12 TO RBL12 BS1016 - BS1078 WL308.5. MARKED<[01] UPDATED TABLE; COMPLETED STEP 9.;[02] ' AS PER EA 25-153-00791; THE REWORK IS ACCEPTABLE AS A CONTINUE-IN-SERVICE CONDITION WITHOUT REPETITIVE INSPECTIONS SDR SWAA2025040906466Angle · corrodedCORROSION ON ANGLE UNDER VERTICAL STAB BS1036 LBL2 WL308.5. MARKED <[01]. ADDED DIMENSIONS TO STEP 2.SDR SWAA2025050615901Plate · crackedWIGGLE PLATE ON L/W T/E ORSS 261 IS CRACKED. REMOVED AND REPLACED WIGGLE PLATE ON L/W T/E AT ORSS 261 IAW SRM 51-40-02-0G-0 PARA. 4. VERIFIED CORRECTIVE ACTION STEP 1. TASK CARD COMPLETE.SDR SWAA2025040905686Plate · crackedWIGGLE PLATE ON L/W T/E ORSS 261 IS CRACKED <[01]. REMOVED AND REPLACED WIGGLE PLATE ON L/W T/E AT ORSS 261 IAW SRM 51-40-02-0G-0 PARA. 4.; [02] VERIFIED CORRECTIVE ACTION STEP 1. TASK CARD COMPLETE.SDR SWAA2025050605541Scuff Plate · crackedACB FWD CORNER SCUFF PLATE CRACKED(MARKED)<[01] 04 - REPAIRED PER [SRM 53-60-15-2R-1-A00967 (REPAIR 1 - AFT CARGO DOOR SURROUND STRUCTURE - PERMANENT)]SDR SWAA2025050639172Attach Fitting · corrodedCORROSION ON LEFT WING FRONT SPAR AROUND BOOST PUMP UPPER BONDING STRAP ATTACHMENT POINT - IFSS 121.<[01] REPAIRED CORROSION ON LEFT WING FRONT SPAR BOOST PUMP AT UPPER BONDING STRAP ATTACH POINT AT IFSS121 IAW WITH SWA EA 25-157-00744 (AD- N7815L - ATS(PAE) -SDR SWAA2025050615880Pressure Deck · crackedCRACK FOUND ON HORIZONTAL PRESSURE DECK AT MID PASSENGER CABIN BS663+8' RBL 40 L: 0.6'( MARKED)<[01] REMOVED AND REPLACED BEADED PRESSURE DECK WEB SECTION AT BS 663 RBL 30 TO RBL 60 PER B-737-700 SRM 53-40-51-2R-2 REPAIR 2 STEP 4 A-N.;[02] COMPLETE;[03] FAULT SDR SWAA2025040905218Pressure Deck · crackedCRACK FOUND ON HORIZONTAL PRESSURE DECK AT MID PASSENGER CABIN BS663+8' RBL 40 L: 0.6'( MARKED) <[01]. REMOVED AND REPLACED BEADED PRESSURE DECK WEB SECTION AT BS 663 RBL 30 TO RBL 60 PER B-737-700 SRM 53-40-51-2R-2 REPAIR 2 STEP 4 A-N.; [02] COMPLETE; [03] FSDR SWAA2025050604854Strut · crackedL/H MLG GEAR STRUT DOOR IS CRACKED<[01] UPDATED STEPS 1;2 FOR REMOVAL L/H MLG SHOCK STRUT DOORS;[02] COMPLETED STEPS 2;4;[03] COMPLETED STEP 1 INSTALL L/H MLG SHOCK STRUT DOORS.;[04] REMOVED; REPAIRED; REINSTALLED; ADJUSTED AND PERFORMED GOOD INSTALLATION TESTSDR SWAA2025022699482Lens · missingL/H OVER WING EMERGENCY EXIT LIGHT LENS COVER MISSING<[01] INSTALLED L/H OVER WING EMERGENCY EXIT LUGHT LENS COVER PER SIPSDR SWAA2025022699061Control Unit · malfunctionedINTERMITTANT RIGHT WING/BODY OVERHEAT LIGHT ON APPROACH LIGHT EXTINGUISHED SHORT AFTER ILLUMINATION<[01] PERFORMED COMPARTMENT OVERHEAT DETECTION CONTROL UNIT BITE CHECK PER AMM 26-18-00 AND WING BODY OVERHEAT TEST PER AMM 26-18-01; FAULT CLEARED AND OPS CHECKSDR SWAA2025012789283Shroud · misinstalledFWD ENTRY DOOR SLIDE SHROUD NOT INSTALLED PROPERLY AT BOTTOM CENTER OF SHROUD<[01] INSTALLED CORRECTLY FWD ENTRY DOOR-SLIDE IAW AMM 25-66-01-400-801.;[02] INSTALLED CORRECTLY FWD ENTRY DOOR-SLIDE IAW AMM 25-66-01/401-MT 725-61-06.;[03] VERIFIED CORRECTIVE ACTISDR SWAA2025012788590Light · inoperativeEMERGENCY LIGHT L1065 INOP APROX STA 480 LEFT<[01] RELAMPED EMERGENCY LIGHT L1065 APROX STA 480 LEFT; PERFORMED GOOD TEST PER AMM 33-51-03-960-801;[02] VERIFIED CORRECTIVE ACTION ITEM 1; CARD COMPLETE.SDR SWAA2025012388436Elec Connector · disconnectedEMERGENCY EXIT CEILING LIGHT L1419 INOP.<[01] PERFORMED TROUBLESHOOTING FOUND CONNECTOR D40038J DISCONNECT. RECONNECTED CONNECTOR D40038P FOR THE EMERGENCY LIGHT L1419 PER SWPM 20-63-02. PERFORMED GOOD OPERATIONAL TEST PER AMM 33-51-00-710-801;[02] VERIFIED COSDR SWAA2025012385910Seat Track · crackedPASSENGER CABIN SEAT TRACK AFT FASTENER HEAD HAS A CRACK AT BS 727B; RBL 24.75. (MARKED)<[01] FINISHED PER EA-25-153-00101;[02] VERIFIED CORRECTIVE ACTION COMPLETESDR SWAA2025012884184Track · crackedRT HAND FWD UPPER TRACK ASSY FOR PANEL 343AT CRACKED.<[01] REMOVED AND REPLACED RT HAND FWD UPPER TRACK ASSY FOR PANEL 343AT IAW AMM 27-41-31-400-802.; [02] VERIFIED CORRECTIVE ACTION ENTRY 1.SDR SWAA2025012283949Scuff Plate · crackedFCB FWD CORNER SCUFF PLATE CRACKED<[01] REPAIRED IAW SRM 53-30-15-2R-1; NDI CRACK FREE; FCB FWD CORNER SCUFF PLATE;[02] VERIFIED ALL STEPS; CORRECTION ACTION ITEM 1; MEASUREMENT FIELD COMPLETE; CARD COMPLETE.SDR SWAA2025012283947Scuff Plate · crackedACB AFT CORNER SCUFF PLATE CRACKED<[01] VERIFIEDSDR SWAA2025012283948Scuff Plate · crackedACB FWD CORNER SCUFF PLATE CRACKED<[01] VERIFIEDSDR SWAA2025012283447Floorbeam · crackedBS540 FLOOR SUPPORT (PANEL BREAK) IS CRACKED RBL1; WL208<[01] REOMOVED AND REPLACED NEW FLOOR SUPPORT (PANEL BREAK) BS540 RBL1 TO RBL24 IAW SRM 51-40-02 AND DWG 143A0060 ID:0002 REV: B;[02] VERIFIED CORRECTIVE ACTION 1SDR SWAA2025012283452Floorbeam · crackedBS540 FLOOR SUPPORT (PANEL BREAK) IS CRACKED LBL1; WL208<[01] REMOVED AND REPLACED FLOOR SUPPORT (PANEL BREAK) BS540 LBL1 TO LBL24 IAW SRM 51-40-02 AND DWG 143A0060 ID:0002 REV: B<BR>INSTALLED PANEL 231UF IAW AMM 53-21-00-400-801;[02] CORRECTIVE ACTION COMPLETSDR SWAA2025012083130Floor Panel · pulledPASSENGER CABIN FLOOR PANEL 231XF HAS AREAS OF PULLED STRANDS<[01] PASSENGER CABIN FLOOR PANEL 231XF WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE IAW SRM 53-00-50-2R-0; DWG 144A5810 ID:0007.;[02] VER
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