N8643A
Service difficulty reports · 183
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 = 'N8643A' 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 = 'N8643A' 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 SWAA2026092887107Floor Panel · pulledFLOOR PANEL 241SF UPPER SKIN HAS AREAS OF PULLED STRANDS. FLOOR PANEL 241SF WAS REPLACED WITH A SERVICEABLE FLOOR PANEL IAW SRM 51-10-02-0G-0, PARA 9.A.1,SDR SWAA2026092827889Floor Panel · pulledFLOOR PANEL 242GF UPPER SKIN HAS AREAS OF PULLED STRANDS. REPLACED THE FLOOR PANEL IAW SRM 53-00-50-2R-0-B00275.SDR SWAA2026092832479Attach Angle · crackedCRACK FOUND AT BS 692.75, RBL 0.2, WL 207, UNDER 241AF FLOOR PANEL. REMOVED AND REPLACED THE FLOORBEAM ATTACH ANGLE IAW SRM 51-40-02, & DWG 273A9111, REV -.SDR SWAA2026092891995Floor Panel · pulledFLOOR PANEL 241HF UPPER SKIN HAS AREAS OF PULLED STRANDS. FABRICATED NEW FLOOR PANEL IAW SRM 53-00-50-2R-0 AND BOEING DWG 146A5810.SDR SWAA2026092851806Floor Panel · pulledFLOOR PANEL 241RF UPPER SKIN HAS AREAS OF PULLED STRANDS. DUE TO EXTENT OF DAMAGE FLOOR PANEL 241RF WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9.A (1).SDR SWAA2026092804217Floor Panel · pulledFLOOR PANEL 241GF UPPER SKIN HAS AREAS OF PULLED STRANDS. DUE TO EXTENT OF DAMAGE FLOOR PANEL 241GF WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9.A (1).SDR SWAA2026092844663Floor Panel · pulledFLOOR PANEL 231NF UPPER SKIN HAS AREAS OF PULLED STRANDS. DUE TO EXTENT OF DAMAGE FLOOR PANEL 231NF WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9.A (1).SDR SWAA2026092847690Sidewall Support · corroded18 AREAS OF CORROSION FOUND ON FLOOR TO SIDEWALL SUPPORT FROM BS 480 - 500D+15, WL 156, TASK CARD WILL BE ACCOMPLISHED ON CUSTOMER CARD TTG8Q01DUKN2.SDR SWAA2026092813479Floor Panel · pulledFLOOR PANEL 231GF UPPER SKIN HAD AREAS OF PULLED STRANDS. DUE TO EXTENT OF DAMAGE, THE FLOOR PANEL 231GF WAS REPLACED IAW SRM 51-10-02-0G-0, PAR 9.A (1).SDR SWAA2026092823015Floor Panel · pulledFLOOR PANEL 241PF UPPER SKIN HAS AREAS OF PULLED STRANDS. REPLACED WITH A SERVICEABLE FLOOR PANEL IAW SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.SDR SWAA2026092823001Floor Panel · pulledFLOOR PANEL 232JF UPPER SKIN HAD AREAS OF PULLED STRANDS. FABRICATED A NEW FLOOR PANEL IAW SRM 53-00-50-2R-0, AND DWG 143A5810.SDR SWAA2026092862914Floor Panel · damagedAFT FLOOR PANEL 242D UPPER SKIN ALONG THE OTBD EDGE HAD AN AREA OF EXPOSED HONEYCOMB CORE. THE AFT FLOOR PANEL 242D WAS REPAIRED IAW SRM 53-00-50-2R-1.SDR SWAA2026092806679Floor Panel · pulledFLOOR PANEL 241DF UPPER SKIN HAD AREAS OF PULLED STRANDS. THE FLOOR PANEL 241DF WAS REPLACED WITH A SERVICEABLE FLOOR PANEL IAW SRM 51-10-02-0G-0, PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.SDR SWAA2026092890908Scuff Plate · crackedACD AFT CORNER SCUFF PLATE IS CRACKED REPAIRED ACD AFT CORNER SCUFF PLATE IAW SRM 53-60-15-2R-1AND TREATED AND PRIMER IAW SRM 51-20-01-0G-0 FOR CHEMICAL CONVERSION COATING AND AMM 51-21-72-370-804 FOR PRIMER. (THE INSTALLATION PROCCES WILL BE ATTENDED ON TASK SDR SWAA2026092880434Floor Panel · pulledFLOOR PANEL 231FF UPPER SKIN HAS AREAS OF PULLED STRANDS. REPAIRED IAW SRM 53-00-50-2R-1.SDR SWAA2026092828963Stringer Clip · crackedBS 727E, STR 6R STRINGER CLIP CRACKED, REMOVED AND REPLACED THE STRINGER CLIP IAW SRM 51-40-02 AND DWG 146A1112 REV -.SDR SWAA2026092804978Floor Panel · pulledFLOOR PANEL 232CF UPPER SKIN HAS AREAS OF PULLED STRANDS. DUE TO EXTENT OF DAMAGE FLOOR PANEL 232CF WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9.A (1).SDR SWAA2026092812829Stringer Clip · crackedFOUND A CRACKED STRINGER CLIP AT STA 727B, STGR 8 LH. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-40-02 AND DWG 146A1102 REV -.SDR SWAA2026092863655Floor Panel · pulledFLOOR PANEL 231DF UPPER SKIN HAS AREAS OF PULLED STRANDS. DUE TO EXTENT OF DAMAGE FLOOR PANEL 231DF WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9.A (1).SDR SWAA2026092831840Floor Panel · pulledFLOOR PANEL 232FF UPPER SKIN HAS AREAS OF PULLED STRANDS. REPAIRED BY FABRICATING NEW PANEL IAW SRM 53-00-50-2R-0-B00275.SDR SWAA2026092861519Stringer Clip · crackedFOUND A CRACKED STRINGER CLIP AT STA 727C, STGR 5 LH. REMOVED AND REPLACED STRINGER CLIP AT BS 727C STR-5L IAW SRM 51-40-02-0G-0 AND DWG#146A1103 REV: -.SDR SWAA2026092888536Floor Panel · pulledFLOOR PANEL 241AF UPPER SKIN HAS AREAS OF PULLED STRANDS. FABRICATED NEW FLOOR PANEL 241AF IAW SRM 53-00-50-2R-0 AND BOEING DWG 144A5810-127.SDR SWAA2026092847554Floor Panel · pulledFLOOR PANEL 231ZF UPPER SKIN HAS AREAS OF PULLED STRANDS. REPAIRED DAMAGED UPPER SKIN ON FLOOR PANEL 231ZF IAW SRM 53-00-50-2R-1.SDR SWAA2026092815546Scuff Plate · crackedFCD AFT CORNER SCUFF PLATE IS CRACKED. REMOVED AND REPLACED FCD AFT CORNER SCUFF PLATE IAW 53-11-02-020-801 AND AMM 53-11-02-420-801/ PERFORMED A GOOD LEAK CHECK FCD AFT CORNER SCUFF PLATE IAW AMM 05-51-91-790-801.SDR SWAA2026092871941Floor Support · corrodedCORROSION ON FLOOR SUPPORT BS 947+2, RBL 51, WL 208. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02-0G-0, AND DWG 147A5650, REV A.SDR SWAA2026092862752Floorbeam · corrodedCORROSION ON FLOORBEAM UPPER FLANGE AT NUTPLATE HOLE, BS 986.5, LBL 43, WL 208. REPAIRED THE FLOORBEAM FWD UPPER FLANGE IAW SRM 51-40-02-0G-0 AND SRM 53-70-51-2R-6, REPAIR 6.SDR SWAA2026092835493Floor Support · corrodedCORROSION ON FLOOR SUPPORT BS 947+2 LBL51. WL208. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-40-02-0G-0 AND DWG 147A5650, REV A.SDR SWAA2026092838693Support · corrodedCORROSION ON LH SHEAR WEB ZEE SUPPORT ANGLE BS986.5+6 LBL33, WL208. REMOVED AND REPLACED ON LH SHEAR WEB ZEE SUPPORT AT BS1000 BS1016 LBL 33 IAW B737-800 SRM 51-40-02-0G-0 AND DWG:147A5700 ID:0121 REV:A VERIFIED CORRECTIVE ACTION STEP 1.SDR SWAA2026092873584Panel · debondedPANEL 192BR OUTER SKIN IS DISBONDED NEAR THE FWD EDGE. THE PANEL WAS REPAIRED IAW SRM 51-70-05-2R-2.SDR SWAA2026082106267Overheat Loop · false indicationLEFT WING BODY OVERHEAT LIGHT ILLUMINATED AFTER NR 2 ENGINE START, WITH APU BLEED SWITCH ON. BITE SHOWS CODE 44 WITH ALARM LIGHT ILLUMINATED. CHECKED AFT CARGO, FOUND FULLY LOADED. UNABLE TO CHECK FOR HOT AREAS. TROUBLESHOT IAW FIM 26-18 TASK 802, AND 8SDR SWAA2026072097679Coffeemaker · odorFWD COFFEE POT HAS SLIGHT BURNING ODOR. R & R THE COFFEE MAKER IAW AMM 25-30-01. OPS CK GOOD.SDR SWAA2026062213873Hook And Loop · detachedF/A REPORTED FLAP FOR 4 SLIDE STICK OUT. ADJUSTED FLAP ON SLIDE BY REATTACHED LOOSE PORTION OF HOOK AND LOOP INSIDE CONTAINER PER HMM 25-66-00SDR SWAA2026052105197Unknown · odorELEC BURNING ODOR IN COCKPIT OR FWD GALLEY SOURCE UNKNOWN. C/W CONDITIONAL INSP IAW AMM 05-51-56 AND TASK 21-00 TASK 806; NO DEFECTS NOTED A/C OK FOR SVCSDR SWAA2026042191147Sign · brokenLEFT FWD OVERWING DOOR EXIT SIGN BROKEN. R & R LT FWD OVERWING DOOR EXIT SIGN PER SIP.SDR SWAA2025110329295Arm · brokenSEAT 14F TRAY TABLE BROKEN. SECURED SEAT 14F TRAY TABLE AND ASSIGNED TO MEL 25-10-01 XC SP1B. R & R ARM ON SEAT 14F TRAY TABLE IAW CMM 25-22-46. THIS CLEARS MEL.SDR SWAA2025090811778Tray · brokenTRAYTABLE 14F BROKE<[01] REPLACED MISSING HARDWARE ON TRAY TABLE AT SEAT ROW 14F PER SIPSDR SWAA2025082206805Sign · missingEMRGENCY EXIT SIGN COVER MISSING<[01] INSTALLED SIGN PER S.I.P.SDR SWAA2025031906147Cover · looseWHITE PLASTIC EXIT SIGN ON THE CEILING FOR THE OVER-WING EXIT NEEDS TOBE RE-INSTALLED <[01]. RE-SECURED AISLE CEILING EXIT/SALIDA LIGHT SIGN COVER PER AMM33-51-01. OP CHECK GOOD.SDR SWAA2024111156730Girt Bar · unsecureFWD ENTRY DOOR EMERGENCY SLIDE GIRT UNSECURED FROM BACKING PAN SHELF<[01] RESECURED SLIDE GIRT TO BACKING PAN SHELF PER MT725-61-06SDR SWAA2024101545862Battery Pack · inoperativeVARIOUS CABIN EMERGENCY LIGHTS ARE INOP.<[01] REMOVED AND REPLACED BATTERY PACKS AT M1670; M1671; M1695; M2335 AND M1694 AND OPS CK GD AS PER AMM 33-51-06SDR SWAA2024101545341Vapor Barrier · crackedREJECT: CORRECTIVE ACTION #4 ON FAULT 'L/H A/C BAY; STA. 663 ANGLE TO VAPOR BARRIER CRACKED AT FASTENER HOLE LBL-9 [TTG8Q00VZFX4]' HAS INCORRECT SRM REFERENCE. SRM 57-10-10-2R-5 SHOULD BE USED.<[01] PER SRM 57-10-10-2R-5; REPAIR IS NOT APPLICABLE DUE TO SPLICESDR SWAA2024101544659Plate · crackedLEFT WING I/B WAFFLE PLATE UNDER PANEL 551EB CRACKED.<[01] REMOVED AND INSTALLED NEW L/H WING I/B WAFFLE PLATE UNDER PANEL 551EB PER SRM 51-40-02.;[02] INSPECTION C/WSDR SWAA2024101543187Battery Pack · inoperativeAISLE EMERGENCY LIGHT AT 8 ABC WILL NOT ILLUMINATE.<[01] REMOVED AND REPLACED BATTERY PACK ON M2335 ON CARD TTG8Q00WA1WG; AND OPS CK GD AS PER AMM 33-51-06SDR SWAA2024101543189Floorbeam · crackedFLOOR STRUCTURE BRACE AT STA 540 ; LBL+1 HAS EVIDENCE OF CRACKING.<[01] REMOVED AND REPLACED BROKEN FLOOR BRACE PER SRM 51-40-02;[02] INSPECTION COMPLETE ON CORRECTIVE ACTION #1 FOR FLOOR BRACE REPLACEMENT.SDR SWAA2024101541030Brace · crackedFLOOR STRUCTURE BRACE AT STA 540 ; R+1 HAS EVIDENCE OF CRACKING.<[01] REMOVED AND REPLACED FLOOR STRUCTURE BRACE PER SRM 51-40-02.;[02] INSPECTION COMPLETED ON CORRECTIVE ACTION #1 FLOOR BRACE REPLACEMENT.SDR SWAA2024101540752Fan Cowl · cracked#2 ENGINE O/B FAN COWL PNL# 424 HAS A CRACKED INNER WEB. (MARKED)<[01] REPLACED #2 OUTBOARD FAN COWL WITH SERVICEABLE PART REFERENCE BARCOD TTG8Q00S5GPU.;[02] VERIFIED REPLACED #2 OUTBOARD FAN COWL WITH SERVICEABLE PART REFERENCE BARCODE TTG8Q00S5GPU. INSPECTISDR SWAA2024101540763Fan Cowl · cracked#1 ENGINE I/B FAN COWL PNL #414 INNER WEB CRACKED. (MARKED)<[01] REPLACED #1 ENGINE INBOARD FAN COWL WITH SERVICEABLE PART REFERENCE BARCODE TTG8Q00S5GPU;[02] VERIFIED REPLACED #1 ENGINE INBOARD FAN COWL WITH SERVICEABLE PART REFERENCE BARCODE TTG8Q00S5GPU. INSDR SWAA2024101640399Angle · crackedLH A/C BAY STA 663 LBL 10' LOWER FLANGE OF ANGLE CRACKED AT FASTENER HOLE.<SDR SWAA2024101640400Angle · crackedRH A/C BAY STA 663 RBL 10' LOWER FLANGE OF ANGLE CRACKED AT FASTENER HOLE<SDR SWAA2024101539794Angle · crackedR/H A/C BAY; STA. 663 ANGLE TO VAPOR BARRIER CRACKED AT FASTENER HOLES RBL-9 AND RBL-32<[01] REMOVED R/H A/C BAY; STA. 663 DAMAGED ANGLE IAW SRM 51-40-02.;[02] EXISTING FASTENER HOLES ON REPAIR AREA OF WING CENTER SECTION REAR SPAR VAPOR BARRIER REQUIRE NDT PE
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