N8623F
Service difficulty reports · 194
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 = 'N8623F' 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 = 'N8623F' 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 SWAA2025112027439Floorbeam · crackedCRACK ON THE FLOORBEAM LOCATED BS 540 BTW LBL 0 TO LBL 24.75, WL 208.1. REPLACED FLOORBEAM IAW SRM 51-10-02-0G, ITEM 9, SRM 51-40-02-0G, AND DWG 143A0060, SHEET 64, REV -.SDR SWAA2025112027444Web · corrodedCORRODED WEB BTW BS 927 - 947.5, LBL 3, WL 156.1. WEB CLASSIFIED AS PRIMARY-OTHER IAW SRM 51-00-04. REPLACED THE WEB IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 147A7500; SHEET 38; REV -.SDR SWAA2025112826935Support Beam · crackedCRACK TRAILING EDGE DEFLECTION CONTROL RIB SUPPORT BEAM AT RT WING. PERFORMED PERMANENT REPAIR ON TRAILING EDGE DEFLECTION CONTROL RIB SUPPORT BEAM AT RT WING IAW SRM 57-51-02-2R-3SDR SWAA2025112027157Stub Frame · crackedCRACK INDICATION ON STUB FRAME, BETWEEN BS 294.5 - 296.5, BTW S8R TO S9R. LENGTH OF CRACK; 0.312 IN. REPLACED THE STUB FRAME AND FASTENERS IAW SRM 51-40-02, DWG 141A8370, SHEET 9, SHEET 10, REV D.SDR SWAA2025112027156Floor Support · crackedCRACK FLOOR SUPPORT BTW BS 277 TO 294.5, BL 0. REPLACED THE FLOOR SUPPORT IAW SRM 51-10-02, ITEM 9, AND SRM 51-40-02. MEASUREMENT OF THE CRACK IS 1.0675 INCHES.SDR SWAA2025112027155Floor Support · crackedCRACKED FLOOR SUPPORT BTW BS 344 - 360, BL 0. REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 141A5400, SHEET 32, REV -.SDR SWAA2025112027152Floor Support · crackedCRACKED FLOOR SUPPORT BTW BS 312 - 328 LBL 46 IN THE FWD GALLEY AREA. REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02, SRM 51-10-02, ITEM 9 & DWG 141A5400, SHEET 26, REV -.SDR SWAA2025112626443Support Beam · crackedCRACK DEFLECTION CONTROL RIB SUPPORT BEAM TRAILING EDGE AT LT WING. PERFORMED PERMANENT REPAIR ON DEFLECTION CONTROL RIB SUPPORT BEAM TRAILING EDGE AT LT WING IAW SRM 57-51-02-2R-3.SDR SWAA2025112026436Strap · corrodedCORROSION ON EXITING REPAIR LOCATED BS 986.5 RBL 17 WL 208.1 AT AFT GALLEY AREA. REPLACED REPAIR STRAP AND FASTENERS LOCATED BS 986.5 RBL 10 TO RBL 22 WL 208.1 AT AFT GALLEY AREA IAW SRM 53-70-51-2R-6.SDR SWAA2025112026435Plate · corrodedCORROSION ON PLATE, BS 1016 PLUS 5 INCHES, LBL 4, WL 208.1. REPLACED THE PLATE IAW SRM 51-40-02, AND DWG 147A5700, SHEET 122, REV A.SDR SWAA2025112626183Support Angle · crackedCRACK ON CARGO LINER SUPPORT ANGLE LOCATED BS 727B LBL49 AT AFT CARGO COMPARTMENT. PERFORMED PERMANENT REPAIR LOCATED ON CARGO LINER SUPPORT ANGLE LOCATED BS 727B LBL49 AT AFT CARGO COMPARTMENT IAW SRM 51-70-11-2R-0.SDR SWAA2025112026188Floorbeam · corrodedCORROSION ON FLOORBEAM LOCATED BS 986.5 LBL44 WL 208.1 AT AFT GALLEY AREA. PERFORMED PERMANENT REPAIR PART STRAP, ANGLE AND FILLER ON FLOORBEAM LOCATED BS 986.5, LBL 44, WL 208.1 AT AFT GALLEY AREA IAW SRM 51-40-02, AND SRM 53-70-51-2R-6, REPAIR 6.SDR SWAA2025112625600Light · burned outBURNED SEGMENT WINDOW EMERGENCY LIGHT ON DOOR 833 AT PASSENGER CABIN. REPLACED WINDOW EMERGENCY LIGHT ON DOOR 833 AT PASSENGER CABIN IAW AMM 33-21-00-960-805. PERFORMED OPS TEST. TESTED OK.SDR SWAA2025112025597Strap · corrodedCORROSION ON OUTER WING LEADING EDGE LOWER ATTACH STRAP AT OSS 65 RT WING. OBTAINED OK TO INSTALL NUT PLATE ON OUTER WING LEADING EDGE LOWER ATTACH STRAP LOC AT OSS 65 ON RT WING. REPAIRED RH WING - O/B FIXED LEADING EDGE - ATTACH STRAP OUTBOARD - BETWEEN SDR SWAA2025091714772Tire · failedLEFT NOSE GEAR TIRE FAILED ON T/O. NO ABNORMAL ENGINE INDICATION NOTED. NO SMELL IN CABIN. PERFORMED CONDITIONAL INSPECTION 05-51-54 TIRE TREAD LOSS OR TIRE BURST REF. TTG8Q0156579 FOR REPLACEMENT OF NOSE TIRES. PERFORMED BIRD-HAIL STRIKE CONDITIONAL INSPECTSDR SWAA2025081404418Battery · inoperativeAFT. AIRCRAFT LEFT EMERGENCY FLASHLIGHT INOP.<[01] R/R FLASHLIGHT BATTERY IAW MM 25-64-00 .SDR SWAA2025073095898Battery · inoperativeCREW REPORTS, FWD MEGAPHONE INOPERATIVE. R & R MEGAPHONE BATTERIES IAW AMM 25-64-00.SDR SWAA2025070888671Light · out of positionPIECE OF PLASTIC ON FLOOR NEXT. TO ROW 1 CAPTAIN SIDE STICKING UP<[01] RETAPED PHOTOLUMINESCENT STRIP ON CAPT SIDE IAW SIPSDR SWAA2025061079137Battery Pack · inoperativeFWD ENTRY AND FWD GALLEY EMERGENCY EXIT SIGNS INOP<[01] REMOVED AND REPLACED M01675 EMERGENCY LIGHT BATTERY PACK AND CHARGER PER AMM 33-51-06.SDR SWAA2025060274484Handle · looseR1 DOOR LINER ASSIST HANDLE LOOSE<[01] SECURED LOOSE R1 DOOR LINER ASSIST HANDLE IAW B737-800 AMM TASK 25-21-31-420-802.;[02] VERIFIED SECURED LOOSE R1 DOOR LINER ASSIST HANDLE IAW B737-800 AMM TASK 25-21-31-420-802.SDR SWAA2025060274290Battery Pack · inoperativeL1 DOOR EMERGENCY LIGHT'S INOP (OVERHEAD AND LOWER EXIT LIGHT)<[01] REMOVED AND REPLACED 1 EA BATTERY PACK M1675 (OVER L1 DOOR) AND OPS CHECK GOOD IAW SWA B737-800 AMM 33-51-06-960-805.;[02] VERIFIED REMOVED AND REPLACED 1 EA BATTERY PACK M1675 (OVER L1 DOOR) SDR SWAA2025051267221Bulb · burned outBOTH FWD OVERWING EXIT LOWER IDENTIFIERS HAVE BURNED OUT BULBS<[01] RE-LAMPED AND PERFORMED GOOD OPS CHECK OF BOTH FWD OVERWING EXIT LOWER IDENTIFIERS BULBS PER AMM 33-51-01-960-801SDR SWAA2025051267223Battery Pack · inoperativeEMERGENCY EXIT LIGHTS ASSOCIATED WITH BATT PACK M1671 ARE INOP<[01] REMOVED EMERGENCY EXIT BATTERY PACK M1671 AND INSTALLED SERVICEABLE BATTERY PACK AND PERFORMED GOOD INSTALLATION TEST PER AMM 33-51-06-960-805;[02] VERIFIED TASK C/WSDR SWAA2025051267224Battery Pack · inoperativeEMERGENCY EXIT LIGHTS ASSOCIATED WITH BATT PACK M1673 ARE INOP<[01] REMOVED EMERGENCY EXIT BATTERY PACK M1673 AND INSTALLED SERVICEABLE BATTERY PACK AND PERFORMED GOOD INSTALLATION TEST PER AMM 33-51-06-960-805;[02] VERIFIED TASK C/WSDR SWAA2025041524441Sign · detachedISLE EMERGENCY SIGN DETACHED. <[01] 01 - REMOVED AND REPLACED PER [AMM 33-51-03-960-803-NG (EMERGENCY AISLE LIGHT (EAL) - LENS REPLACEMENT - PERMANENT)].SDR SWAA2025022899141Tail Cone · elongatedNUMBER THREE AFT FLAP FAIRING HAS THREE ELONGATED FASTENER HOLES THAT ATTACH THE AFT TAIL CONE <[01]. REMOVED AND REPLACED THE #3 AFT FLAP FAIRING IAW AMM 27-51-18.;[02] REMOVED AND REPLACED THE #3 AFT FLAP FAIRING IAW AMM 27-51-18.;[03] REMOVED AND REPLACED TSDR SWAA2024111358367Cover · out of adjustLEFT FORWARD AND AFT SLIDE SIGHT COVERS LOOSE<[01] SECURED BOTH SLIDE SIGHT COVERS PER SIP.SDR SWAA2024091034793Sign · looseCABIN CEILING OWE EMERGENCY EXIT SIGN IS LOOSE<[01] ADJUSTED CABIN CEILING OWE EMERGENCY EXIT SIGN AS REQUIRED REFERENCING AMM 33-51-01.SDR SWAA2024040970922Engine · failed#1 ENGINE FAILURE DURING TO. REJECTED TO AT 135 KNOTS. SEVERE DAMAGE IN TURBINE SECTION FOUND ON POST FLIGHT. BOTH FIRE BOTTLES WERE DISCHARGED AFTER FIRE CREW REPORTED FLAMES IN TURBINE SECTION<[01] REMOVED AND REPLACED #1 ENGINE PER MT 771-00-01; REF: TTG8Q0SDR SWAA2024032566550Handle · brokenFWD SERVICE DOOR INNER PLASTIC ASSIST HANDLE BROKE<[01] R&R. FWR SERVICE DOOR INNER PLASTIC ASSIST HANDLE<BR>REF AMM 52-41-00SDR SWAA2024010336536Battery Pack · inoperativeCABIN EMERGENCY LIGHTS ON OVHD BIN BULLNOSE(VALANCE) INOP AT 5ABC; 8ABC; 12ABC; 16ABC; 19ABC AND 23ABC<[01] R&R'D BATTERY PACK LOCATED AT L/H SIDEWALL AT ROW 20ABC; OP CK GOOD IAW AMM 33-51-06.;[02] VERIFIED R&R'D BATTERY PACK LOCATED AT L/H SIDEWALL AT ROW 20SDR SWAA2024010336534Battery Pack · inoperativeCABIN EMERGENCY LIGHTS ON OVHD BIN BULLNOSE(VALANCE) INOP AT 7DEF; 10DEF; AND 14DEF.<[01] R&R'D BATTERY PACK LOCATED AT R/H SIDEWALL AT ROW 7DEF; OP CK GOOD IAW AMM 33-51-06.;[02] VERIFIED R&R'D BATTERY PACK LOCATED AT R/H SIDEWALL AT ROW 7DEF; OP CK GOOD IAW SDR SWAA2024010336535Battery Pack · inoperativeEMERGENCY LIGHTS INOP AT L/H OVERWING EXIT DOOR(#2) LOWER(INNER) AND THREE EXTERNAL LIGHTS(2 AT DOOR 1 AT WING-TO-BODY T/E)<[01] R&R'D BATTERY PACK LOCATED AT L/H SIDEWALL AT ROWS 7ABC AND 13ABC; OP CK GOOD IAW AMM 33-51-06.;[02] VERIFIED R&R'D BATTERY PACK LOSDR SWAA2024010336537Battery Pack · inoperativeEMERGENCY LIGHTS INOP AT R/H OVERWING EXIT DOOR BOTH UPPER PANELS; SECOND DOOR LOWER LIGHT; AND FWD EXTERNAL LIGHT.<[01] R&R'D BATTERY PACK LOCATED AT R/H SIDEWALL AT ROW 13DEF; OP CK GOOD IAW AMM 33-51-06.;[02] VERIFIED R&R'D BATTERY PACK LOCATED AT R/H SIDEWSDR SWAA2024010836342Web · cracked#2 ENGINE O/B FAN COWL OIL DOOR LOWER REINFORCEMENT WEB IS CRACKED.<[01] REPLACED WEB PER SRM 51-10-02 & SRM 51-40-02.;[02] C/W;[03] INSPECTED AS REQUIREDSDR SWAA2024010436343Flap · debondedRIGHT WING AFT FLAP INBOARD LOWER SIDE HAS A REPAIR AND THE METAL BOND OF THE REPAIR IS DISBONDED; AND THE TOP HAS A DELAMINATED ON THE OPPOSITE SIDE.<[01] REMOVED AND REPLACED RH OTBD AFT FLAP. IAW AMM 27-51-22 STEP A-F;[02] VERIFIED THE REMOVAL AND REPLACEMESDR SWAA2024010335391Light · damagedTHE CEILING LIGHT BULLNOSE ON TOP OF OVERHEAD BIN 17DEF AND 18DEF IS DAMAGED.<[01] REMOVED AND REPLACED CELING LIGHT BULLNOSE PANEL PER AMM 25-21-71 AND OPS CHECK EMERGENCY LIGHT OK PER 33-51-03.SDR SWAA2024010834378Web · chafedFLIGHT COMPARTMENT FLOOR STRUCTURE WEB HAS CHAFFING AT STA. 259.5-3; LBL 10. (MARKED)<[01] REPAIRED PER EA # M-153-00734.SDR SWAA2024010432389Slat · delaminated#8 SLAT T/E WEDGE LOWER SURFACE HAS A DELAM 4' FROM TOP 1' FROM O/B EDGE.<[01] REMOVED #8 SLAT IN REF TO AMM 27-81-21.;[02] OK TO INSTALL NEW #8 SLAT.;[03] INSTALLED NEW #8 SLAT PER M/M REF. 27-81-21.;[04] RII INSPECTION C/W FOR CA #3SDR SWAA2024010831752Tab · crackedR/H WING T/E AT APROX ORSS 261 CANNON PLUG DISCONNECT BRACKET MOUNT WEB TAB CRACKED AT RIB . PICTURE ATTACHED INFO: PART REQUIRED IS MPN 287A9152-98. NOT IN MAINTENIX SUBMITTED PAR APP DCN-038641. BOB W. 33000<[01] REMOVED R/H WING T/E AT APROX ORSS 261 CANNONSDR SWAA2024010831750Tab · crackedR/H WING INBD FIXED T/E UPPER PANEL BULB SEAL WEB ATTACH TAB CRACKED AT DEFLECTION CONTROL RIB . PICTURE ATTACHED<[01] REMOVED AND REPLACED R/H WING INBD FIXED T/E UPPER PANEL WEB ATTACH TAB PER SRM 51-4-02.;[02] REMOVED AND REPLACED R/H WING INBD FIXED T/E UPSDR SWAA2024010531733Angle · crackedAFT CARGO COMPARTMENT; L/H SIDEPLATE/ TRANSITION ANGLE CRACKED AT STA. 767+3; LBL 24.<[01] CUT OUT DAMAGED SECTION L/H TRANSITION ANGLE FROM STA.747+11 TO STA. 787+11 PER SRM 53-00-53-REPAIR 5.;[02] FABRICATED REPAIR PARTS;LOCATED AND DRILLED; ALODINE AND PRIMSDR SWAA2024010431286Floor Support · crackedPASSENGER CABIN FLOOR SUPPORT IS CRACKED IN 2(EA) PLACES NEAR FASTENER. BS 540 RBL 1<[01] REMOVED AND REPLACED PASSENGER CABIN FLOOR ASSEMBLY SUPPORT AT STA 540 RBL 1 PER SRM 51-40-02.;[02] REMOVED AND REPLACED PASSENGER CABIN FLOOR ASSEMBLY SUPPORT AT STA 540SDR SWAA2024010830809Panel · corrodedR/H WING FUELING SERVICE PANEL FUEL QUANTITY GUAGES BRACKET HAS AREAS OF SURFACE CORROSION. MRKD<[01] REMOVED AND REPLACED R/H WING REFUELINGF PANEL AND OPS CHECKS GOOD PER MM 28-41-61SDR SWAA2024010431050Girt Bar · out of adjustFWD ENTRY DOOR SLIDE BOX GIRT BAR RETAINER CLIP HAS 2 EA. LOOSE RIVETS<[01] SECURED 2EA FASTENERS ON FWD GIRT BAR BRACKET PER SRM 51-40-02.;[02] C/W;[03] INSPECTION C/WSDR SWAA2022013161277Angle · crackedA-061 R/H WING UPPER FIXED TRAILING EDGE PNL JUST OUTBD OF #7 GROUND SPOILER ATTACH ANGLE CRACKED ; / [01] REMOVED ATTACHED ANGLE I.A.W SRM 51-40-02-0G-0; [02] VERIFIED NEW ATTACH ANGLE PART # 115A2156U8 ATAG: A111293 IAW DWG # 115A2512 REV:-; [03] VERIFIED STSDR SWAA2022013161419Beam · wornA-061 R/H WING DEFLECTION CONTROL RIB UPPER TAB AND SUPPORT BEAM WORN AT 2 EA FASTENER HOLES ; / [01] EVALUATED WEAR - DEFLECTION CONTROL RIB UPPER TAB LOSS OF .051'; MAX ALLOWED .040' OUT OF LIMITS<BR>EVALUATED WEAR - SUPPORT BEAM ORIGINAL THICKNESS .090' LOSSDR SWAA2022013160786Light · inoperativeALL EMERGENCY LIGHTS POWERED BY BATTERY PACK AT M1675 (STA 317 LBL 10) ARE INOP ; / [01] REPLACED BATTERY PACK M1675; OPS CHECK GOOD IAW AMM 33-51-06-960-805.; [02] VERIFIED STEP 1<BR>AUDIT CWSDR SWAA2022013159059Web · corrodedA-061 DOT 024. AFT CARGO PIT THRESHOLD WEB STA 787+8' TO STA 827+19' RBL 25 W/L 155 HAS SEVERAL SPOTS OF CORROSION (MARKED) ; / [01] UT IAW B737 NDT PART 4; 51-00-00 PROC 2. ORIG .050'; LOSS .008'; REMAINING .042'. TOOL#40084; DUE 11AUG22; [02] REMOVED CORROSISDR SWAA2022013159066Shield · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE SHIELD; STA 767+10 TO 792; RBL 20; WL 156 UPPER AND LOWER SURFACE HAS CORROSION. A224-22 ; / [01] REMOVED CORROSION IAW SRM 51-10-02 AND VERIFIED WITH 10X MAG. ORIGINAL MATERIAL THICKNESS .050 LOSS OF .008 WITH .042 REMIAN
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