N8674B
Service difficulty reports · 115
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
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 n_number = 'N8674B' AND registry_match = 'registration' 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 n_number = 'N8674B' AND registry_match = 'registration' 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 SWAA2026080541372Wire · shortedDURING DESCENT BELOW 7,000, WITH LANDING GEAR UP & LANDING GEAR LEVER OFF, THE GREEN LIGHT ILLUMINATED INTERMITTENTLY ON THE FWD PANEL. THE OVERHEAD PANEL WAS NORMAL, WITH THE LANDING GEAR DOWN AND LANDING GEAR LEVER DOWN, GREEN LT GEAR LIGHT WOULD INTERMITSDR SWAA2026072080561Trim Motor · failedOTS - ATB- ELEC. STAB TRIM FAIL ON CLIMB AROUND 1000 FT AGL._ REMOVED AND REPLACED STABILIZER TRIM MOTOR IAW AMM 27-41-71. OPS CHKD GOOD.SDR SWAA2026072096284Trim System · lockedSTAB TRIM WONT TRIM FWD PAST 4 UNITS WITH THE ELECTRIC TRIM SWITCH WITH FLAP IN UP POSITION. PERFORMED STAB TRIM WHEEL FREE MOVEMENT TEST IAW AMM 27-41-00 SYS, OPERATES NORMALLYSDR SWAA2026061009716Cover · brokenCAPTAIN SIDE EMG EXIT COVER BACKPLATE BROKEN. LIGHT WORKS BACKPLATE EDGE BROKEN. WONT HOLD LIGHT COVER. OK TO CONTINUE PER MEL 25-10-01. SP 1B AUTH 322927. R&R LT EMERGENCY EXIT LIGHT ASSY IAW AMM 33-51-01.SDR SWAA2026060809189Unknown · odorSTRONG ODOR NOTICED ON TAXI IN. PERFORMED GENERAL VISUAL NR 1 & 2 ENG. AND PACKS. RAN LT AND RT PACKS ON APU BLEED ONLY . GROUND RUN NR 1 & 2 ENG. BLEED ONLY IAW AMM 71-00-00. NO ODOR OR DEFECTS NOTED.SDR SWAA2026052003840Power Supply · inoperativeLEFT OVERWING EMERGENCY EXIT LIGHTS WILL NOT ILLUMINATE. R & R LT OVERWING EMERGENCY EXIT LIGHT POWER SUPPLY AND BATTERY PACK IAW 33-51-06.SDR SWAA2026052004561Battery Pack · inoperativeLEFT OVERWING EMERGENCY EXIT LIGHTS WILL NOT ILLUMINATE. R & R LT OVERWING EMERGENCY EXIT LIGHT POWER SUPPLY AND BATTERY PACK IAW 33-51-06.SDR SWAA2026051903841Power Supply · inoperativeEMERGENCY EXIT SIGN ROW 13DEF WILL NOT ILLUMINATE. R & R ROW 13DEF EMERGENCY EXIT SIGN POWER SUPPLY IAW AMM 33-51-06 AND ROW 13DEF EMERGENCY EXIT SIGN ASSY PER AMM 33-51-01.SDR SWAA2026042791778Light · unsecureEMERGENCY FLOOR LIGHTING STRIP PEELING UP AT 13C. SECURED THE LIGHT STRIP IAW AMM 33-51-15.SDR SWAA2026040786331Light · loosePHOTOILLUMINESCENT STRIP COMING LOOSE FROM FLOOR AT ROW 12 FO SIDE. NO ABNORMAL SMELLS OR ENGINE INDICATIONS. RESECURED STRIP LIGHTING PER MM 33-51-15.SDR SWAA2026031278221Battery Pack · inoperativeBOTH OVERWING EMERGENCY EXITS SIGNS ON THE RIGHT SIDE ARE INOPERATIVE. R & R THE M1695 EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-06. OPS CHECK GOOD.SDR SWAA2026010959181Ground Wire · pulledEMERGENCY LIGHT OUTSIDE OF MAIN ENTRY DOOR IS INOPERATIVE. FUTHER INVESTIGATION FOUND GROUND WIRE PULLED FROM GROUND BLOCK GD3876 DC. TERMINATED THE WIRE ONTO THE GROUND BLOCK GD3876 DC IAW WDM 33-51-12, SWPM 20-90-15. PERFORMED GOOD FUNCTIONAL TEST OF EMERSDR SWAA2025051970280Angle · crackedOUTER ATTACHMENT CLIP FOR SUPPORT RIB UNDER LEFT WING PANEL 551GB CRACKED<[01] REMOVED + REPLACED OUTER ATTACHMENT CLIP FOR SUPPORT RIB UNDER LEFT WING PANEL 551GB IAW SRM 51-40-02.SDR SWAA2025051970279Support · crackedSUPPORT RIB UNDER LEFT WING PANEL 551GB CRACKED AT UPPER RIVET ROW<[01] REMOVED + REPLACED SUPPORT RIB UNDER LEFT WING PANEL 551GB IAW SRM 51-40-02.SDR SWAA2024122777915Skin · delaminatedL/H WING O/B AFT FLAP DELAMINATED AT THE I/B AFT CORNER AT LOWER SKIN. MARKED<[01] 01 - REMOVED AND REPLACED PER [AMM 27-51-22-400-801-NG (OUTBOARD AFT FLAP INSTALLATION - PERMANENT)];[02] VERIFIED 01 - REMOVED AND REPLACED PER [AMM 27-51-22-400-801-NG (OUTBOASDR SWAA2024122777470Seal · crackedR-HORIZONTAL STABILIZER UPPER SLIDDING SEAL CRACKED DOT# J802<[01] REMOVED AND REPLACED UPPER SLIDING SEAL IAW B737-800 AMM 53-31-31-401. FUNCTION CHECK GOOD;[02] 02 - INSPECTED PER [AMM 53-31-31-401 CONFIG 1-NG (STABILIZER TO BODY FRONT SPAR SLIDING SEAL - RESDR SWAA2024122777471Seal · crackedL-HORIZONTAL STABILIZER UPPER SLIDING SEAL CRACKED DOT# J804<[01] REMOVED AND REPLACED UPPER SLIDING SEAL IAW B737-800 AMM 53-31-31-401. FUNCTION CHECK GOOD;[02] 02 - INSPECTED PER [AMM 53-31-31-401 CONFIG 1-NG (STABILIZER TO BODY FRONT SPAR SLIDING SEAL - REMSDR SWAA2024122777092Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 241AF IS BURNT/DELAMINATED<[01] REMOVED AND REPLACED FLOOR PANEL ASSY 241AF IAW B737-800 AMM 53-21-00-400-801. DISPALCED & REINSTALLED TO F.O.M. SEATS 14ABC; 15ABC; 16ABC; & 17ABC IAW B737-800 AMM 25-22-00-400-802; SUBTASK 25-22-00-420-SDR SWAA2025010275799Angle · crackedCR -- L/H VAPOR BARRIER ANGLE REQUIRES GVI INSP FOR CRACKS<SDR SWAA2025010275800Angle · crackedCR -- R/H VAPOR BARRIER ANGLE REQUIRES GVI INSP FOR CRACKS<SDR SWAA2024122776208Angle · crackedL/H VAPOR LOWER ANGLE BARRIER CRACKS (2) FOUND @ STA 663.75<[01] REMOVED ANGLE PER B737-800 SRM51-40-02. FABRICATED NEW ANGLE PER DWG 111A1322 REV A. INSTALLED NEW ANGLE PER DWG 111A1000 AND B737-800 SRM 51-40-02;[02] REMOVED ANGLE PER B737-800 SRM51-40-02. FASDR SWAA2024122776209Angle · crackedCRACK FOUND ON R/H VAPOR BARRIER LOWER BRACKET @ STA 663.75<[01] REMOVED AND REPLACED ANGLE PER DWG 111A1000 AND B737-800 SRM 51-40-02;[02] REMOVED AND REPLACED ANGLE PER DWG 111A1000 AND B737-800 SRM 51-40-02SDR SWAA2024100343537Megaphone · inoperativeAFT MEGAPHONE SOUNDS WEAK PER INSPECTION<[01] REPLACED BATTERIES ON MEGAPHONE PER AMM 25-64-00. OPS CHECK GOOD REPLACED PLACARD NEXT INSPECTION DUE DATE SEP 25SDR SWAA2024090534386Seat Back · out of adjustPASSENGER SEAT 15D EMERGENCY EXIT ROW SHOULD NOT RECLINE.<[01] ADJUSTED HYDROLOCK IAW AMM 25-22-00SDR SWAA2024090533985Sign · missingMISSING EXIT SIGN IN THE MID CABIN.<[01] REPLACED MID CABIN ?EXIT? SIGN ASSEMBLY AND LENS PER <BR>AMM 33-51-01. OPS CHECK GOOD.SDR SWAA2024082629139Slide · dislodgedCAPTAINS SIDE AFT SLIDE MATERIAL HANGING OUT.<[01] REPOSITIONED SLIDE AND ACCOMPLISHED MT 725-61-06.SDR SWAA2024053090701Lens · detachedMID CABIN OVERHEAD EMERGENCY EXIT SIGN LENS KNOCKED DOWN<[01] REINSTALLED LENS PER AMM 33-51-01SDR SWAA2024052388715Cover · missingMIDDLE AISLE EMERGENCY SIGN MISSING COVER<[01] REPLACED MIDDLE AISLE EMERGENCY SIGN IAW AMM 11-32-01.SDR SWAA2024041574296Lens · missingOVERWING EMERGENCY EXIT SIGN MISSING LENS.<[01] REINSTALLED OVERWING EMERGENCY EXIT LIGHT LENS PER AMM 33-51-01.SDR SWAA2024020547154Cover · detachedEXIT LIGHT COVER TO THE LEFT OF STARBOARD SIDE FWD GALLEY DOOR WONT STAY ON.<[01] R&R'D R1 DOOR EMERGENCY LIGHT LENS PER AMM 33-51-01.SDR SWAA2023121129427Lens · missingEXIT SIGN FRONT COVER MISSING MID CABIN<[01] RESECURED LENS AS REQUIRED PER SIP.SDR SWAA2023111420571Cowl Door · crackedNUMBER 1 ENGINE I/B FAN COWL HAS CRACK FWD OF THE FORWARD LATCH APPROXIMATELY 9 INCHES LONG GOING THROUGH 2 RIVETS<[01] REMOVED AND REPLACED #1 I/B FAN COWL PER AMM 71-11-02;[02] VERIFIED THE FOLLOWING:<BR>REMOVED AND REPLACED #1 I/B FAN COWL PER AMM 71-11-02SDR SWAA2023101909455Scuff Plate · crackedAFT CARGO LOWER MAIN SEAL SCUFF PLATE REQUIRES REPLACEMENT<[01] INSTALLED NEW SCUFFPLATE IAW AMM 53-11-02.;[02] INSTALLED NEW SCUFFPLATE IAW AMM 53-11-02. INSP C/W;[03] INSPECTION C/W INSTALLED NEW SCUFF PLATE IAW AMM 53-11-02. LEAK CHECK GOOD PER STEP 1SDR SWAA2023101912433Battery Pack · inoperativeSEVERAL EMERGENCY BULLNOSE LIGHTS INOP IN CABIN.<[01] REPLACED 4 BATTERY PACKS. 2 FWD LEFT AND RIGHT AND 2 AFT LEFT AND RIGHT. OPS CHECK GOOD. REF AMM 33-51-06.;[02] REPLACED 4 BATTERY PACKS. 2 FWD LEFT AND RIGHT AND 2 AFT LEFT AND RIGHT. OPS CHECK GOOD. REF ASDR SWAA2023101912434Battery Pack · inoperativeSEVERAL EMERGENCY BULLNOSE LIGHTS INOP IN CABIN.<[01] REPLACED 4 BATTERY PACKS. 2 FWD LEFT AND RIGHT AND 2 AFT LEFT AND RIGHT. OPS CHECK GOOD. REF AMM 33-51-06.;[02] REPLACED 4 BATTERY PACKS. 2 FWD LEFT AND RIGHT AND 2 AFT LEFT AND RIGHT. OPS CHECK GOOD. REF ASDR SWAA2023101912435Battery Pack · inoperativeSEVERAL EMERGENCY BULLNOSE LIGHTS INOP IN CABIN.<[01] REPLACED 4 BATTERY PACKS. 2 FWD LEFT AND RIGHT AND 2 AFT LEFT AND RIGHT. OPS CHECK GOOD. REF AMM 33-51-06.;[02] REPLACED 4 BATTERY PACKS. 2 FWD LEFT AND RIGHT AND 2 AFT LEFT AND RIGHT. OPS CHECK GOOD. REF ASDR SWAA2023101908284Battery Pack · inoperativeSEVERAL EMERGENCY BULLNOSE LIGHTS INOP IN CABIN.<[01] REPLACED 4 BATTERY PACKS. 2 FWD LEFT AND RIGHT AND 2 AFT LEFT AND RIGHT. OPS CHECK GOOD. REF AMM 33-51-06.;[02] REPLACED 4 BATTERY PACKS. 2 FWD LEFT AND RIGHT AND 2 AFT LEFT AND RIGHT. OPS CHECK GOOD. REF ASDR SWAA2023102007096Panel · delaminatedWING TO BODY PANEL 194FL HAS A SMALL DENT WITH DELAMINATION. DAMAGE IS MARKED<[01] REMOVED DAMAGE PER SRM 51-70-05-2R-1. POTTED CORE PER SRM 51-70-05-2R-11.;[02] INSPECTED WORK PERFORMED ON C/A #1;[03] INSTALLED REPAIR PLIES IAW SRM 51-70-05-2R;[04] INSPECTED SDR SWAA2023102305590Stringer · separatedINSPECTION OF BS 727 INNER CHORD AT STRINGER 18A RIGHT SIDE HAS .008 GAP BETWEEN STRINGER AND CHORD AS MEASURED DURING 5311-I-14624-NG STEPS 8 & 9<[01] CORRECTED EXCESSIVE GAP WITH COMPLETION OF EO 5311-E-14625-NG.;[02] CORRECTED EXCESSIVE GAP WITH COMPLETION SDR SWAA2023102305589Stringer · separatedBS 727 INNER CHORD AT STRINGER 18A LEFT SIDE HAS .008 INCH GAP AS MEASURED DURING 5311-I-14576-NG STEP 9<[01] CORRECTED EXCESSIVE GAP WITH COMPLETION OF EO 5311-E-14577-NG.;[02] CORRECTED EXCESSIVE GAP WITH COMPLETION OF EO 5311-E-14577-NG.SDR SWAA2023102004240Angle · corrodedAFT CARGO STA 767-787 RBL 23 TRANSITION ANGLE HAS CORROSION AROUND NUT PLATE HOLES.<[01] REMOVED CORROSION FROM AREA PER SRM 53-60-15-1A-1 (REMAINING THICKNESS 0.045'). TRANSITION ANGLE IS OUT OF WITHIN LIMITS PER<BR>SRM 53-60-15-1A-1.;[02] REMOVED RH TRANSITISDR SWAA2023102004242Angle · corrodedAFT CARGO STA 767-747 RBL 23 TRANSITION ANGLE HAS CORROSION AROUND NUT PLATE HOLES.<[01] REMOVED CORROSION FROM AREA PER SRM 53-00-53-1A-2 (REMAINING THICKNESS 0.037'). TRANSITION ANGLE IS OUT OF WITHIN LIMITS PER<BR>SRM 53-00-53-1A-2.;[02] REMOVED RH TRANSITISDR SWAA2023102004265Angle · corrodedAFT CARGO STA 727J-727I RBL 23 TRANSITION ANGLE HAS CORROSION AROUND NUT PLATE HOLES.<[01] REMOVED CORROSION FROM AREA PER SRM 53-00-53-1A-2 (REMAINING THICKNESS 0.037'). TRANSITION ANGLE IS OUT OF WITHIN LIMITS PER<BR>SRM 53-00-53-1A-2.;[02] REMOVED RH TRANSISDR SWAA2023102004244Web · corrodedAFT CARGO STA 776-849 RBL 27 THRESHOLD WEB HAS CORROSION.<[01] REMOVED CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-60-15-1A-1;[02] REMOVED WEB PER SRM 51-40-02;[03] LOCATED AND DRILLED HOLES FOR WEB PER SRM 51-40-05;[04] C/W INSP. LOCATED AND DRILLED HOLES SDR SWAA2023101904472Scuff Plate · crackedAFT CARGO AFT CORNER SCUFF PLATE CRACKED.<[01] INSTALLED NEW CORNER SCUFFPLATE IAW AMM 53-11-02.;[02] INSTALLED NEW CORNER SCUFFPLATE IAW AMM 53-11-02. INSP. C/W;[03] INSPECTION C/W INSTALLED NEW CORNER SCUFF PLATE IAW AMM 53-11-02 AND ACCOMPLISHED CABIN PRESSSDR SWAA2023102003747Floorbeam · corrodedAT BS 947; RBL 14 TIE DOWN LUG HAS CORROSION.<[01] REMOVED CORROSION FROM FLOOR BEAM AT STA 947; RBL 26 TO 27 AND FOUND DAMAGE TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1. TIE DOWN LUG IS AT RBL 26;[02] REMOVED DAMAGED SECTION OF UPPER CHORD I.A.W SRM 53-70-51-2SDR SWAA2023101910550Flap · delaminatedL/H WING ; O/B FLAP; AFT FLAP IS DELAMINATED AT I/B AFT CORNER.<[01] REMOVED L/H WING ; O/B FLAP; AFT FLAPIAW AMM 27-51-22;[02] OK TO INSTALL SERVICEABLE L/H WING ; O/B FLAP; AFT FLAP;[03] INSTALLED SERVICEABLE L/H WING ; O/B FLAP; AFT FLAP ASSY IAW AMM 27-51-SDR SWAA2023072481275Battery Pack · inoperativeFWD ENTRY DOOR EXIT SIGN AND EXIT LOCATOR SIGN INOP<[01] REMOVED AND REPLACED BATTERY PACK M1675 PER AMM 33-51-01. OPS CHECK GOOD.SDR SWAA2023052552453Battery · weakFORWARD MEGAPHONE WEAK TRANSMIT<[01] R&R BATTERIES PER M/M 25-64-00SDR SWAA2023011690514Access Panel · crackedPANEL 621 PB RT WING CRACKED<[01] DRILLED; COUNTERSUNK AND INSTALLED PANEL PER SRM 51-40-05; AND 51-40-02
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