N8673F
Service difficulty reports · 126
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 = 'N8673F' 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 = 'N8673F' 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 SWAA2026092148874Handle · brokenFO`S GRAB HANDLE BROKEN. REPLACED FO`S GRAB HANDLE IAW STANDARD INDUSTRY PRACTICES. OPS CHKD GOOD.SDR SWAA2026082568398Sense Line · faultedATB DUE TO RH LOW BLEED & LT PACK FLUCTUATING. O/W LANDING._ R & R NR 2 ENGINE PRECOOLER BRAIDED SENSE LINE PER MM 36-12-00SDR SWAA2026072705973Engine · failedAT APPOX 30 KTS ON T/O ROLL WITH T/O PWR SET NR 2 ENG FAILED WITH AUDIBLE BANG AND RIGHT SWERVE. PERFORMED RTO. HAD ENG FAILED ON NR 2 EGT DISPLAY. AIRPORT OPS REPORTED DEBRIS BEHIND AIRCRAFT ON RUNWAY. REMOVED AND REPLACED NR 2 ENGINE IAW AMM 71-00-02. PERFSDR SWAA2026081891593Engine · failedAT APPOX 30 KTS ON T/O ROLL WITH T/O PWR SET NR 2 ENG FAILED WITH AUDIBLE BANG AND RIGHT SWERVE. PERFORMED RTO. HAD ENG FAILED ON #2 EGT DISPLAY. AIRPORT OPS REPORTED DEBRIS BEHIND AIRCRAFT ON RUNWAY.SDR SWAA2026012062750Light · inoperative15 ABC EMERGENCY EXIT INDICATOR LIGHT INOPERATIVE. REMOVED AND REPLACED 15 ABC EMERGENCY EXIT ASSEMBLY IAW AMM 33-51-01.SDR SWAA2025121750999Wire · cutEMERGENCY EXIT LIGHT ATTACHED TO RT SIDEWALL PANEL 242ZAW, FOUND TO HAVE CUT WIRES. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-51-14-960-802. PERFORMED GOOD EMERGENCY LIGHT OPS TEST IAW AMM 33-51-00-710-801.SDR SWAA2025121849219Retainer · missingRIGHT EMERGENCY EXIT FWD LENS RETAINER FOUND MISSING. FOUND AND INSTALLED THE MISSING RT, FWD LENS RETAINER IAW AMM 33-21-00-960-804.SDR SWAA2025121643747Retainer · missingRIGHT EMERGENCY EXIT FWD LENS RETAINER FOUND MISSING.SDR SWAA2025110330438Light · unsecureF/A REPORTS 4 INCH TRIPPING HAZARD, THE PHOTO LUMINESCENT STRIP IS STICKING UP ABOUT 4 INCHES AND IS A POTENTIAL TRIPPING HAZARD. ATTACHED AS NECESSARY IAW AMM 33-51-400-899. FLOOR PROXIMITY LIGHT IAW AMM 33-51-15.SDR SWAA2025012288070Battery Pack · inoperativeFWD AND AFT LH OVERWING EMERGENCY LIGHTS INOP<[01] CHANGED REASON CODE FOR REMOVAL FROM ROB TO CAUSE BY REQUEST FROM TRAVIS MCCLESTER X316070;[02] CERTIFIED;[03] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AND OPS CHECK GOOD REF B737 AMM 33-51-06;[04] VESDR SWAA2025012287761Latch · missingCR AH - RH EMERGENCY EXIT ROW SEATS 13DEF 14DEF MISSING ONE-WAY TRAY TABLE LATCHES<[01] REMOVED AND REPLACED 6 EACH SEAT TRAY TABLE LATCHES FOR ONE WAY LOCKING LATCHES AT ROW 13DEF AND 14DEF IAW B737-800 CMM 25-22-46.;[02] REMOVED AND REPLACED 6 EACH SEAT TRAYSDR SWAA2025012383733Seal · crackedLEFT STABILIZER UPPER SLIDING SEAL WORN / CRACKED.<[01] REMOVED AND REPLACED SLIDING SEAL IAW B737-NG AMM 53-31-31;[02] VERIFIED REMOVED AND REPLACED SLIDING SEAL IAW B737-NG AMM 53-31-31SDR SWAA2025012383732Seal · crackedRIGHT HORIZONTAL STABILIZER UPPER SLIDING SEAL WORN / CRACKED.<[01] REMOVED AND REPLACED RIGHT HORIZONTAL STABILIZER UPPER SLIDING SEAL IAW B737NG AMM 53-31-31;[02] REMOVED AND REPLACED RIGHT HORIZONTAL STABILIZER UPPER SLIDING SEAL IAW B737NG AMM 53-31-31;[03SDR SWAA2025012382980Floor Support · crackedMAIN CABIN; 1 EACH FLOOR SUPPORT CRACKED AT BS 540 APPROX LBL-1. MARKED<[01] REMOVED; LOCATED; DRILLED; AND INSTALLED FLOOR SUPPORT REF B737-NG SRM 51-40-02 AND BAC DWG 143A5240-63 REV A;[02] REMOVED; LOCATED; DRILLED; AND INSTALLED FLOOR SUPPORT REF B737-NG SSDR SWAA2025012382976Floor Support · crackedMAIN CABIN; 1 EACH FLOOR SUPPORT CRACKED AT BS 540 APPROX RBL-1. MARKED<[01] REMOVED; LOCATED; DRILLED AND INSTALLED FLOOR SUPPORT REF BAC DWG 143A5240-63 REV A. AND B737-NG SRM 51-40-02;[02] REMOVED; LOCATED; DRILLED AND INSTALLED FLOOR SUPPORT REF BAC DWG 14SDR SWAA2025012382572Skin · delaminatedL/H O/B AFT FLAP DELAMINATED AT UPPER AND LOWER SKINS BETWEEN 72' INCHES AND 110' INCHES FROM I/B EDGE.<[01] 01 - REMOVED AND REPLACED PER [AMM 27-51-22-400-801-NG (OUTBOARD AFT FLAP INSTALLATION - PERMANENT)];[02] 02 - INSPECTED PER [AMM 27-51-22-400-801-NG (SDR SWAA2025012282750Strap · corrodedL/H EMERGENCY EXIT HATCH ESCAPE STRAP HOOK HAS CORROSION.<[01] REMOVED AND REPLACED L/H EMERGENCY EXIT HATCH ESCAPE STRAP IAW B737-800 SRM 51-40-02 & AMM 25-61-10-400-802.;[02] REMOVED AND REPLACED L/H EMERGENCY EXIT HATCH ESCAPE STRAP IAW B737-800 SRM 51-40-0SDR SWAA2025012282564Handle · missingFWD CARGO DOOR ASSIST HANDLE IS MISSING UPPER CHORD<[01] INSTALLED FWD CARGO DOOR ASSIST HANDLE UPPER CHORD PN: 69-41730-85; PO#: 1110113.1 PER B737-800 AMM 52-31-00-420-003 PAR. (5)(G);[02] CORRECTIVE ACTION CORRECTION: INSTALLED FWD CARGO DOOR ASSIST HANDLE SDR SWAA2025012282566Handle · missingAFT CARGO DOOR ASSIST HANDLE IS MISSING UPPER CHORD<[01] INSTALLED AFT CARGO DOOR ASSIST HANDLE UPPER CHORD PN:69-41730-86; PO#:1104656.2 PER B737-800 AMM 52-31-00-420-004 PAR.(5)(G);[02] VERIFIED INSTALLED AFT CARGO DOOR ASSIST HANDLE UPPER CHORD PN:69-41730-SDR SWAA2025012487078Bracket · damaged[DOT: Z047] RIGHT WING L/E CAVITY INBD OF PYLON HAS PNEUMATIC DUCT OTBD SUPPORT BRACKET HAS ELONGATED HOLES. (STREAMER ATTACH)<[01] REMOVED AND REPLACED R/W L/E O/B BLEED AIR SUPPORT BRACKET ASSY PN: 212A1214-12 PO# 1109767.3 IAW B737-800 SRM 51-40-02 & BAC DWSDR SWAA2025012487079Bracket · damaged[DOT: Z048] RIGHT WING L/E CAVITY INBD OF PYLON HAS PNEUMATIC DUCT INBD SUPPORT BRACKET HAS ELONGATED HOLE. (STREAMER ATTACH)<[01] REMOVED & REPLACED R/W L/E I/B BLEED AIR SUPPORT BRACKET ASSY PN: 212A1214-9ATSMRO BN: 562974 IAW B737-800 SRM 51-40-02 & BAC DWGSDR SWAA2025012282111Cap · missingAFT CARGO COMPARTMENT FWD BULKHEAD FLOOR CAP STRIP MISSING<[01] RECVD. AND INSTALLED NEW CAP STRIP PT.# 435A2511-2 IAW B737-800 SRM 51-40-02;[02] VERIFIED RECVD. AND INSTALLED NEW CAP STRIP PT.# 435A2511-2 IAW B737-800 SRM 51-40-02.SDR SWAA2025012181905Light · inoperativeFLT DECK ENTRY EMERGENCY WHITE LIGHT ON BAR STRIP LIGHT INOP<[01] RE-LAMPED AND OP CHECKED LIGHT BAR IN EMERGENCY LIGHT IAW SWA 737-800 AMM 33-51-01-960-801. LIGHTS OP CHECK GOOD.;[02] VERIFIED RE-LAMPED AND OP CHECKED LIGHT BAR IN EMERGENCY LIGHT IAW SWA 737-SDR SWAA2025012181904Light · burned outR2 DOOR EMERGENCY LIGHT STRIP HAS BURNED OUT LIGHT<[01] REPLACED LAMP AT R2 DOOR EMERGENCY LIGHT STRIP AND PERFORMED A GOOD TEST OF THE R2 DOOR EMERGENCY LIGHT IAW SWA AMM 33-51-01.;[02] REPLACED LAMP AT R2 DOOR EMERGENCY LIGHT STRIP AND PERFORMED A GOOD TEST SDR SWAA2024061300431Sign · detachedOVERWING EXIT SIGN COVER FELL OFF<[01] R&R?D OVERHEAD OVERWING EXIT SIGN ASSY PER M/M 33-51-01 OPS NORMAL.SDR SWAA2024030760334Cover · detachedOVER -WING EXIT SIGN COVER POPPED OFF<[01] 01 - REMOVED AND REPLACED PER [AMM 33-51-01-201-NG (EXIT SIGNS - MAINTENANCE PRACTICES - PERMANENT)]<BR><BR>REINSTALLED COVERSDR SWAA2024021251439Battery Pack · inoperativeFO SIDE OVER WING EMERGENCY EXIT EMERGENCY LIGHTS INOP<[01] R&R BATTERY PACK REF AMM 33-51-06 OPS CHECK NORMALSDR SWAA2023112020316Cap · corrodedAFT PIT R/H CAP STRIP AFT OF DOOR HAS CORROSION. AFT PIT R/H CAP STRIP AFT OF DOOR HAS CORROSION<[01] REMOVED AND REPLACED AFT PIT R/H CAP STRIP PER SOPM 20-50-01.;[02] REMOVED AND REPLACED AFT PIT R/H CAP STRIP PER SOPM 20-50-01.;[03] REMOVED AND REPLACED AFTSDR SWAA2023111719950Fairing · delaminatedNO. 7 FLAP TRACK SUPPORT FAIRING HAS A SMALL TEAR WITH DELAMINATION I/B SIDE OUTER SKIN<[01] REMOVED DAMAGE PER SRM 57-53-70-2R-1;[02] VERIFIED CORRECTIVE ACTION #1;[03] POTTED CORE PER SRM 51-70-05-2R-11;[04] VERIFIED CORRECTIVE ACTION #3;[05] CUT OUT REPAIR SDR SWAA2023112019867Panel · damagedRH WING TRAILING EDGE SEAL PANEL 344EB HAS ELONGATED HOLES<[01] REMOVED AND REPLACED TRAILING EDGE SEAL PANEL #344EB;[02] RH HORIZONTAL STABILIZER IS WHERE 344EB IS LOCATED...NOT RIGHT WING. CONFIRMED REPLACEMENT OF 344EB.SDR SWAA2023112019056Battery Pack · inoperativeRH FWD EMERGENCY LIGHT IN THE CABIN INOP<[01] REPLACED BATTERY PACK; LIGHTS TEST GOOD IAW AMM 33-51-06;[02] VERIFIEDSDR SWAA2023112019057Battery Pack · inoperativeLH AFT CABIN EMERGENCY LIGHTS INOP<[01] REPLACED BATTERY PACK; LIGHTS TEST GOOD IAW AMM 33-51-06;[02] VERIFIEDSDR SWAA2023112019942Nut Plate · wrong partLEFT HORIZONTAL STABILIZER LOWER TRAILING EDGE BEAM HAS INCORRECT NUT PLATE INSTALLED AT ELEVATOR STA 181.64 OUTBOARD OF NO.5 ELEVATOR HINGE. ADDITIONAL HOLE DRILLED INTO STRUCTURE.<[01] REPAIRED PER EA 23-155-03277;[02] RII; COMPLIED WITH INSPECTION; REPAIREDSDR SWAA2023112016525Tail Cone · elongatedLH WING #3 CANOE FAIRING TAIL CONE BOLT HOLES ELONGATED<[01] REMOVED AND REPLACED TAIL CONE PER AMM 27-51-18SDR SWAA2023112015139Scuff Plate · crackedAFT CARGO AFT CORNER SCUFF PLATE CRACKED.<[01] REMOVED AND REPLACED AFT CARGO; AFT CORNER SCUFF PLATE I.A.W AMM 53-11-02.;[02] REMOVED AND REPLACED AFT CARGO; AFT CORNER SCUFF PLATE I.A.W AMM 53-11-02. C/W INSPECTION;[03] VERIFIED WORK SIGNED OFFSDR SWAA2023112015218Tail Cone · delaminatedTAIL CONE HAS 2EA. SMALL AREAS OF DELAMINATION R/H SIDE UPPER AFT MKD.<[01] REMOVED DAMAGE PER SRM 51-70-05 REPAIR 1.;[02] VERIFIED REMOVED DAMAGE PER SRM 51-70-05 REPAIR 1.;[03] REPAIRED DAMAGE PER SRM 53-80-70-2R-1;[04] REPAIRED PER SRM 51-70-05-2R-1SDR SWAA2023112014406Angle · corrodedFWD CARGO HAS SURFACE CORROSION ON RT. TRANSITION ANGLE BS436-440<[01] CLEAN CORROSION PER SRM 51-10-02. REWORKED AREA IS OUT OF LIMIT PER SRM 53-00-53-1A-2 FIG 103 DETAIL D.;[02] DRILLED THE NEW ANGLE PER SRM 51-40-05;[03] VERIFIED CORRECTIVE ACTION #2;[04] OSDR SWAA2023112014408Angle · corrodedAFT CARGO STA. 727C-727G; CORROSION AROUND NUT=PLATE HOLES ON RT TRANSITION ANGLE.<[01] REMOVED CORROSION PER SRM 53-00-53-1A-2 (REMAINING THICKNESS 0.036'). TRANSITION ANGLE IS OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] REMOVED SIDEPLATE CHANNEL FROM STA 767 TSDR SWAA2023112014385Angle · corrodedAFT CARGO STA. 727G-767; CORROSION AROUND NUT=PLATE HOLES ON RT TRANSITION ANGLE.<[01] REMOVED CORROSION PER SRM 53-00-53-1A-2 (REMAINING THICKNESS 0.036'). TRANSITION ANGLE IS OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] RT TRANS ANGLE REPLACED FROM STA 727+4 TOSDR SWAA2023112014386Angle · corrodedAFT CARGO STA. 727-727H; CORROSION AROUND NUT-PLATE HOLES ON LT TRANSITION ANGLE.<[01] REMOVED CORROSION PER SRM 53-00-53-1A-2 (REMAINING THICKNESS 0.034'). TRANSITION ANGLE IS OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] RT TRANS ANGLE REPLACED FROM STA 727+4 TOSDR SWAA2023112014387Angle · corrodedAFT CARGO STA. 727H-847; CORROSION AROUND NUT-PLATE HOLES ON LT TRANSITION ANGLE.<[01] REMOVED CORROSION PER SRM 53-00-53-1A-2 (REMAINING THICKNESS 0.022'). TRANSITION ANGLE IS OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] REMOVED AND REPLACED AFT CARGO L/H TRANSISDR SWAA2023112014388Web · corrodedAFT CARGO STA. 767-790; CORROSION ON TOP AND BOTTOM SURFACES OF RT TRANSITION ANGLE AROUND NUT-PLATE HOLES.<[01] REMOVED CORROSION PER SRM 53-60-15-1A-1 (REMAINING THICKNESS 0.046'). TRANSITION ANGLE (SHIELD) IS OUT OF LIMITS PER SRM 53-60-15-1A-1.;[02] REMOVESDR SWAA2023112014390Nut Plate · corrodedAFT CARGO STA.727D+4 LBL24-RBL2; CORROSION ON FLOORBOARD NUT-PLATE STRAP.<[01] REMOVED CORROSION PER SRM 53-00-53-1A-2. (REMAINING THICKNESS 0.066'). STRAP IS OUT OF LIMITS SRM 53-00-53-1A-2 AND SRM 51-10-02.;[02] REMOVED AND REPLACED FLOORBOARD STRAP PER SRM SDR SWAA2023112014391Nut Plate · corrodedAFT CARGO STA.767+4 LBL24-RBL24; CORROSION ON FLOORBOARD NUT-PLATE STRAP.<[01] REMOVED CORROSION FROM AREA PER SRM 53-00-53-1A-2. (REMAINING THICKNESS 0.058'). STRAP OUT OF LIMITS PER SRM 53-00-53-1A-2 AND SRM 51-10-02.;[02] REMOVED AND REPLACED FLOORBOARD STRSDR SWAA2023112014413Threshold · corrodedAFT CARGO ENTRY DOOR THRESHOLD STA. 790-847; CORROSION AROUND NUT-PLATE HOLES.<[01] REMOVED CORROSION FROM AREA PER SRM 53-60-15-1A-1 (REMAINING THICKNESS 0.042'). THRESHOLD WEB IS OUT OF LIMITS PER SRM 53-60-15-1A-1.;[02] REMOVED WEB PER SRM 51-40-02;[03] LOCSDR SWAA2023112014395Support Angle · crackedAFT CARGO STA. 867 LBL 16; LAV TANK POST HAS A CRACKED SUPPORT ANGLE AT BOTTOM INSIDE SURFACE.<[01] REMOVED SUPPORT ANGLE PER SRM 51-40-02; LOCATED AND DRILL NEW SUPPORT ANGLE PER SRM 51-40-05.;[02] OK TO INSTALL SUPPORT ANGLE.;[03] R&R SUPPORT ANGLE AND REINSSDR SWAA2023112013963Support Angle · corrodedFWD GALLEY THRESHOLD SUPPORT ANGLE HAS CORROSION AT 3EA. N/P HOLES STA. 300 STA. 315 AND STA. 319 RBL 57-58. MRKD<[01] REMOVED CORROSION; FOUND OUT OF LIMITS PER SRM 53-10-51-1A-1;[02] VERIFIED REMOVED CORROSION; FOUND OUT OF LIMITS PER SRM 53-10-51-1A-1.;[03]SDR SWAA2023112013957Intercostal · crackedBETWEEN STATION 380 AND STATION 400; THE INTERCOSTAL AT LBL 51 HAS AN UPPER SURFACE CRACK.<[01] REMOVED DAMAGED PART FROM AIRCRAFT. DRILLED FASTENERS HOLES IN REPLACEMENT PART. REFERENCE SRM 51-10-02 AND SRM 51-40-02.;[02] REMOVED DAMAGED PART FROM AIRCRAFT. DSDR SWAA2023112013958Intercostal · crackedBETWEEN STATION 380 AND STATION 400; THE INTERCOSTAL AT LBL 13 HAS AN UPPER SURFACE CRACK.<[01] REMOVED DAMAGED PART FROM AIRCRAFT. DRILLED FASTENERS HOLES IN REPLACEMENT PART. REFERENCE SRM 51-10-02 AND SRM 51-40-02.;[02] VERIFIED CORRECTIVE ACTION #1;[03] OKSDR SWAA2023112014274Tail Cone · delaminatedTAIL CONE HAS MULTIPLE DELAMINATED DENTS BETWEEN MULTIPLE COMPOSITE REPAIRS ON UPPER ON L/H SURFACES<[01] REMOVED DAMAGE IN AREAS OF DENTS MARKED PER SRM 51-70-5-05. REPAIR 1;[02] INSPECTED WORK PERFORMED ON C/A #1;[03] POTTED CORE ON AFFECTED REPAIR AREAS PR
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