N8610A
Service difficulty reports · 171
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 = 'N8610A' 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 = 'N8610A' 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 SWAA2021020144323Battery Pack · inoperativeFORWARD ENTRY HEADER PANEL EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY EXIT LIGHTS BATTERY PACK M1675. OPS CHECK GOOD IAW AMM 33-51-06-960-805. WW094SDR SWAA2021020143139Floor Panel · pulledFOUND DURING OK TO INSTALL; CABIN FLOORBOARD PANEL 222BF HAS PULLED FIBERS ON UPPER SURFACE. / REMOVED AND REPLACED APU AIR INLET SEAL I-A-W AMM 49-15-11-000-801 AND AMM 49-15-11-400-801 WW0942SDR SWAA2021020142856Intercostal · crackedDURING FWD WET AREA RESTORATION DVI FWD WET AREA INTERCOSTAL CRACKED AT FASTENER HOLE BETWEEN STA 312 TO 328 LBL45. REMOVED AND REPLACED INTERCOSTAL PN 141A5410-140 TAG WN0990 AT WET AREA STA 312 TO 328 LBL 45 IAW B737 SRM 51-10-02-0G-0 AND DWG 141A5400 REV.SDR SWAA2021020141491Floorboard · damagedCABIN FLOORBOARD PANEL 221BF HAS DAMAGED FIBERS ON UPPER SURFACE / REPAIRED CABIN FLOORBOARD PANEL 221BF WITH DAMAGED FIBERS ON UPPER SURFACE AND BROKEN TAB ON AFT O/B CORNER IAW B737 SRM 53-00-50-2R-1 AND B737 SRM 53-00-50-2R-0SDR SWAA2021020141481Floor Panel · damagedAFT PASSENGER CABIN FLOOR BOARD 241XF HAS 40% OF TOP SURFACE WITH COMPOSITE FIBER STRANDS PULLED. REPAIRED DAMAGE TO UPPER SURFACE OF FLOORBOARD 241XE IAW 737-800 SRM 53-*00-50-2R-1 REV. 71 REPAIR 1; SRM 53-00-50-2R-0 REV. 71 REPAIR GENERAL. TAP TEST GOOD.SDR SWAA2021020141482Floor Panel · damagedAFT PASSENGER CABIN FLOOR BOARD 242UF HAS TOP SURFACE WITH COMPOSITE FIBER STRANDS PULLED. REPAIRED FLOOR PANEL 242UF IAW B737-800 SRM 53-00-50-2R-0 REPAIR 1 A13436; A33702; A95094; A89382; A94665SDR SWAA2021020141483Floor Panel · damagedAFT PASSENGER CABIN FLOOR BOARD 241AAF HAS TOP SURFACE WITH COMPOSITE FIBER STRANDS PULLED. REPAIRED DAMAGE TO UPPER SURFACE OF FLOORBOARD 241AAF IAW 737-800 53-00-50-2R-1 REV. 71; SRM 53-00-50-2R-0 REV. 71 REPAIR GENERAL. TAP TEST GOOD A72547 A85487.SDR SWAA2021020141484Floorboard · pulledAFT PASSENGER CABIN FLOOR BOARD 242E HAS TOP SURFACE WITH COMPOSITE FIBER STRANDS PULLED. REPAIRED DAMAGE TO UPPER SURFACE OF FLOORBOARD 242E IAW 737-800 SRM 53-00-50-2R-1 REV. 71; SRM 53-00-50-2R-0 REV. 71 REPAIR GENERAL. TAP TEST GOOD A72547 A85487.SDR SWAA2021020141485Floorboard · damagedAFT PASSENGER CABIN FLOOR BOARD 241E HAS TOP SURFACE WITH COMPOSITE FIBER STRANDS PULLED. REPAIRED DAMAGE TO UPPER SURFACE OF FLOORBOARD 241E IAW 737-800 SRM 53-00-50-2R-1 RREV 71; SRM 53-00-50-2R-0 REV 71 REPAIR GENERAL TAP TEST GOOD. A72547 A85487SDR SWAA2021020141486Floorboard · damagedAFT PASSENGER CABIN FLOOR BOARD 241ABF HAS TOP SURFACE WITH COMPOSITE FIBER STRANDS PULLED. REPAIRED FLOOR PANEL 241ABF IAW B737-800 SRM 53-00-50-2R-0 REPAIR 1 A13436; A33702; A95094; A89382; A94665.SDR SWAA2021020141488Intercostal · corrodedFORWARD CABIN FLOOR STRUCTURE; STA 305; LBL11; WL208; INTERCOSTAL FLOOR SUPPORT UPPER SURFACE; 2 EA SPOTS OF CORROSION; MRK'D IN RED. REMOVED CORROSION AT FWD CABIN FLOOR STRUCTURE STA 305 LBL11 INTERCOSTAL FLOOR SUPPORT IAW B737 SRM 51-10-02-0G-0 AND 53-10-5SDR SWAA2021071642852Baffle · crackedFWD PIT LH BAFFLE AT BS 500E TO 500F WL 158 IS CRACKED ON THE FWD UPPER FLANGE / REMOVED AND REPLACED FWD PIT L/H BAFFLE STA 500E TO 500F WL 158 IAW SRM 51-40-02-0G-0 AND DWG: 143A7505 REV: -SDR SWAA2021051341252Skate Angle · chafedRIGHT SIDE; VERTICAL FIN SKATE ANGEL; WORN/CHAFFING; STA. 1119-1127. / REMOVED DAMAGE FROM RT VERTICAL FIN SKATE ANGLE IAW SRM 51-10-02-0G-0 ORIG THICKNESS .063' LOSS OF .001' REMAINING .062' FOUND TO BE OUT OF LIMITS DUE TO NO PUBLISHED SRM ALLOWABLES FOR THESDR SWAA2021042341323Fitting · corrodedPASSENGER CABIN FLOOR STRUCTURE;LAV FITTING AREA CORRODED INBD SIDE STA.947 LBL 50 WL 208 / REMOVED CORROSION AND VERIFIED LIMITS ON FLOOR STRUCTURE STA. 947 LBL 50 WL 208. ORIGINAL T= .180 MATERIAL LOSS = .050 REMAINING .0130 OUT OF LIMITS IAW SRM 53-70-51-1ASDR SWAA2021040241239Floor Panel · corrodedAFT PIT FLOOR PANEL 140EF HAS AREAS OF CORROSION AROUND UPPER OUTER EDGES. / EVALUATED CORROSION AT AFT CARGO PNL 140EF FOUND CORROSION THAN 20' FOUND OUT OF LIMITS IA-W SRM 53-00-53-1A-1 FABRICATED NEW FLOOR PNL IAW MM 25-52-01-201-801 AND BOEING DWG 453A2610SDR SWAA2021020141322Fitting · corrodedPASSENGER CABIN FLOOR STRUCTURE LAV FITTING AREA CORRODED INBD SIDE STA.947 LBL 31 WL 208. REMOVED CORROSION AND VERIFIED LIMITS ON FLOOR STRUCTURE STA 947 LBL 31 WL 208. ORIGINAL T=.180 MATERIAL LOSS = .065 REMAINING .115 OUT OF LIMITS IAW SRM 53-70-51-1A-1.SDR SWAA2021020141253Angle · corrodedAFT PIT STA 727C+10 TO 767 ;RBL21; Z-ANGLE HAS 18 SPOTS OF CORROSION ADJACENT TO FASTENER HOLES; MRK'D IN RED. WL 158. REMOVED CORROSION AT AFT PIT STA 727C+10 TO 767 RBL 21 Z ANGLE IAW B 737 SRM 51-10-02-0G-0 ITEM 15 ORIGINAL 'T' .040 REMAINING .029 LOSS .01SDR SWAA2021020141250Angle · corrodedAFT PIT STA 727C TO 727J+6; LBL21; Z-ANGLE HAS 21 SPOTS OF CORROSION MOSTLY ADJACENT TO FASTENER HOLES; MRK'D IN RED. WL 158. REMOVED CORROSION AT AFT PIT STA 727C TO 727J+6' Z ANGLE IAW B 737 SRM 51-10-02-0G-0 ITEM 15 ORIGINAL 'T' .040 REMAINING .029 LOSS .0SDR SWAA2021071641062Shield · corrodedAFT CARGO COMPT. STA 768 - 787; RBL22; WL156 SHIELD HAS CORROSION UPPER SURFACE / REMOVED CORROSION AT AFT CARGO COMPARTMENT STA 767-787 RBL 22 SHIELD AND VERIFIED LIMIT FOUND TO BE 100% MATERIAL LOSS IAW B737 SRM 53-60-15-1A-1 REOVED AND REPLACED SHIELD IAW BSDR SWAA2021020140905Angle · corrodedFORWARD CARGO COMPARTMENT LT Z-ANGLE; CORROSION AROUND FASTENER HOLES STA.500C-500E LBL 24' WL 158. REMOVED CORROSION FROM FWD CARGO BAY LT ZEE ANGLE STA 500C - 500E LBL 24 WL 158 IAW SRM 51-10-02-0G-0 PAR. 15 AND INSPECTED W/ 10X MAG GLASS. NO DEFECTS NOTED.SDR SWAA2021020140907Angle · corrodedFORWARD CARGO COMPARTMENT RT Z-ANGLE; CORROSION AROUND FASTENER HOLES STA.500A-500E RBL 24' WL 158. REMOVED CORROSION ON RT Z-ANGLE; STA 500A - 500E; IAW SRM 51-10-02-0G-0. VERIFIED LIMITS; ORIGINAL .040'; LOSS .007'; REMAINING .033' OUT OF LIMITS IAW SRM 53-SDR SWAA2021020140906Angle · corrodedFORWARD CARGO COMPARTMENT LT Z-ANGLE; CORROSION AROUND FASTENER HOLES STA.500E-500H LBL 24' WL 158. REMOVED CORROSION FROM FWD CARGO BAY LT ZEE ANGLE STA 500E - 500H LBL 24 WL 158 IAW SRM 51-10-02-0G-0 PAR 15 AND INSPECTED W/ 10X MAG GLASS. NO DEFECTS NOTED. SDR SWAA2021020140908Angle · corrodedFORWARD CARGO COMPARTMENT RT Z-ANGLE; CORROSION AROUND FASTENER HOLES STA 500E-500I RBL 24' WL 158. REMOVED CORROSION ON RT Z-ANGLE; STA 500E - 500I IAW SRM 51-10-02-0G-0 VERIFIED LIMITS; ORIGINAL .040'; LOSS .010'; REMAINING .030' OUT OF LIMITS IAW SRM 53-00SDR SWAA2021040240896Floor Panel · corrodedAFT CARGO COMPARTMENT FLOOR PANEL 140CF HAS CORROSION AROUND EDGES / EVALUATED CORROSION ON FLOOR PANEL 140CF FROM AFT CARGO COMPARTMENT CORROSION WAS FOUND TO BE OUT OF LIMITS EXCEEDS 20' IAW B737 SRM 53-00-53-1A-1. FABRICATED FLOOR PANEL IAW B737 AMM 25-52-0SDR SWAA2020120132997Girt Bar · stuckFWD SERVICE DOOR GIRT BAR STUCK. REPOSITIONED FWD SERVICE GIRT BAR, PER AMM 25-66-01.SDR SWAA2020100821361Bracket · looseGIRT BAR BRACKET ON FWD SERVICE DOOR APPEARS LOOSE. SECURED BRACKET WITH HARDWARE, PER SRM 51-40-02 AND COMPLIED WITH MT 725-61-06.SDR SWAA2020061090603Smoke Detector · intermittentSMOKE ALARM IN AFT LAV, FO SIDE WAS INTERMITTENT. NO SMOKE IN LAV, REPLACED SMOKE DETECTOR PER AMM 26-14-01.SDR SWAA2020022841941Battery Pack · inoperativeFORWARD R/H EXTERIOR EMERGENCY LIGHT INOPERATIVE. / R&R BATTERY PACK PER AMM.SDR SWAA2020013040876Sign · brokenSECOND WINDOW OF EMERGENCY EXIT ON FIRST OFFICER SIDE HAD A BROKEN EXIT SIGN BRACKET ON FLOOR LEVEL EMERGENCY EXIT SIGN. R&R SIGN ASSEMBLY IAW MM.SDR SWAA2019051032514Slide · unsecureL1 DOOR SLIDE FELL OUT OF COMPARTMENT. REINSTALLED SLIDE IAW MT.SDR SWAA2019040231232Sign · missingRT EMERGENCY EXIT "EXIT/SALIDA" ILLUMINATING PLACARD MISSING AT ROW 14. R&R EMERGENCY EXIT HOUSING AND LENS PER AMM.SDR SWAA2019032631057Sign · missingRT EMERGENCY EXIT "EXIT/SALIDA" ILLUMINATING PLACARD MISSING AT ROW 14. REATTACHED SIGN IAW EA.SDR SWAA2022030345518Channel · crackedAIRCRAFT DAMAGE RIGHT WING #5 FLAP TRACK UPPER U CHANNEL DOOR U CHANNEL CRACKED / REMOVED AND REPLACED R/H FLAP #5 FLAP TRACK UPPER 'U' CHANNEL FLAP TRACK FLAPPER DOOR IAW B737 DWG 149A7331 REV- AND IAW EA 190146 REV IR AND SWA EA REPAIR-57EA-0G455 REV 1 AND SSDR SWAA2022030345503Floor Panel · corrodedFWD CARGO COMPARTMENT FLOOR PANEL # 120CF CORROSION ON UPPER SURFACE. / FWD CARGO COMPTMENT FLOOR PANEL 120CF FOUND TO BE MORE THEN 20' OF CORROSION; OUT OF LIMITS IAW SRM 53-00-53-1A-1. FIG 102. REPLACED PANEL IAW IPC 25-52-10-17. PANEL INSTALLED ON S-AM 565SSDR SWAA2022030345504Floor Panel · corrodedFWD CARGO COMPARTMENT FLOOR PANEL # 120DF CORROSION ON UPPER AND LOWER SURFACE. / FWD CARGO COMPARTMENT FLOOR PANEL 120DF FOUND TO BE MORE THEN 20' OF CORROSION OUT OF LIMITS IAW SRM 53-00-53-1A-1 FIG 102. REPLACED PANEL IAW IPC 25-52-10-17. PANEL INSTALLED ONSDR SWAA2022030345505Floor Panel · corrodedFWD CARGO COMPARTMENT FLOOR PANEL # 120AF CORROSION ON UPPER SURFACE. / FWD CARGO COMPARTMENT FLOOR PANEL 120AF FOUND TO BE MORE 20' OF CORROSION; OUT OF LIMITS IAW SRM 53-00-53-1A-1. FIG 102. REPLACED PANEL IAW IPC 25-52-10-17. PANEL INSTALLED ON SA-M 565S W/SDR SWAA2022030345484Angle · crackedAFT CARGO COMPARTMENT STA 867 LBL 12 STANCHION LOWER ATTACH ANGLE CRACKED. / REMOVED DAMAGED ANGLE INSTALLED NEW ANGLE AS REQUIRED AFT CARGO STA 867 LBL 12. IAW SRM 51-40-02-0G-0SDR SWAA2022030345487Floor Panel · corrodedAFT CARGO COMPT FLOOR PANEL 140CF IS CORRODED ALONG THE EDGES. MARKED. / REPLACED AFT CARGO COMPARTMENT FLOOR PANEL 140CF P/N 453A2610-18 IAW B737-800 AIPC 25-52-10-19. SRM 51-10-02-0G-0 AND SRM 53-00-53-1A-1.SDR SWAA2022030345488Floor Panel · corrodedAFT CARGO COMPT FLOOR PANEL 140DF IS CORRODED ALONG THE EDGES. MARKED. / REPLACED AFT CARGO COMPARTMENT FLOOR PANEL 140DF P/N: 453A2610-20 IAW B737-800 AIPC 25-52-10-19 AND SRM 51-10-02-0G-0 AND SRM 53-00-53-1A-1SDR SWAA2022030345489Floor Panel · corrodedAFT CARGO COMPT FLOOR PANEL 140BF IS CORRODED ALONG THE EDGES. MARKED. / REPLACED AFT CARGO COMPARTMENT FLOOR PANEL 140BF PIN: 453A2610-32 IAW B737-800 SIPC 25-52-10-19; SRM 51-10-02-0G-0 AND SRM 53-00-53-1A-1 ATAG: WN5844SDR SWAA2022030245445Floor Panel · corrodedAFT CARGO COMPT FLOOR PANEL 140EF IS CORRODED ALONG THE EDGES. MARKED. / REPLACED AFT CARGO FLOOR PANEL 140EF; P/N 453A2610-58 IAW B737-800 AIPC 25-52-10-19; SRM 51-10-02-0G-0 AND SRM 53-00-53-1A-1. ATAG: WN4541SDR SWAA2022030245464Bracket · crackedRH WING TE; UPR TE FIXED PNL; CENTER SUPT BRKT CRACKED ON FWD SIDE. MARKED. / R/H WING T/E FIXED PNL CENTER SUPPORT BRACKET CRACKED. REMOVED CRACKED SUPPORT ANGLE I/A/W SRM 51-40-02-06-0. LOCATED AND DRILLED NEW SUPPORT ANGLE BRACKET I/A/W SRM 51-40-05-0G-0 ALSDR SWAA2022030245463Bracket · crackedRH WING TE; UPR TE FIXED PNL; OTBD SUPT BRKT FWD SIDE CRACKED AT DEFLECTOR SUPT RIB. / REMOVED AND REPLACED R/H WING T/E FIXED PANEL OUTBD SUPPORT BRACKET IAW B737 SRM 51-40-02-0G-0 PARA 4; DWG 115A6200 ID2002 REV B.SDR SWAA2022030245465Web · crackedLEFT WING; UPPER TRAILING EDGE PANEL BETWEEN SPOILERS #5 AND #6; INBOARD OF DEFLECTION RIB; HAVE WEB THAT IS CRACKED. MARKED. / REMOVED AND REPLACED WEB AT L/H WING T/E BETWEEN SPOILERS 5 & 6. P/N 115A215607 ATAG A12511 IAW BOEING DWG 115A2512 B737-800 SRM 51-SDR SWAA2022030245469Angle · corrodedFWD CARGO COMPARTMENT AT STA. 500I; LBL 25 TO RBL 25; FLOOR ANGLE HAVE SEVERAL AREAS OF CORROSION. / NO ALLOWABLE LIMITS. REMOVED DAMAGED ANGLE INSTALLED NEW ANGLE AS REQUIRED. FWD CARGO STA 500I LBL25-RBL25. IAW BOEING DWG: 143A9481 REV:-. SRM 51-40-02-0G-0SDR SWAA2022030245467Angle · corrodedFWD CARGO COMPARTMET; STA. 500C+11 - 500F; R/H Z-ANGLE HAVE SEVERAL AREAS OF CORROSION. / REMOVED AND REPLACED FWD CARGO R/H Z ANGLE STA 500A-500F + 12' IAW B737 SRM 51-10-02-0G-0; SRM 53-00-53-2R-5. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 FIG 103 DETASDR SWAA2019022730083Web · crackedLT WING UPPER TRAILING EDGE PANEL BETWEEN SPOILERS 5 AND 6, INBOARD OF DEFLECTION RIB, HAVE WEB CRACKED. R&R WEB IAW SRM AND DWG.SDR SWAA2019022730082Support Bracket · crackedRT WING TRAILING EDGE UPPER TRAILING EDGE FIXED PANEL, CENTER SUPPORT BRACKET CRACKED ON FORWARD SIDE. R&R BRACKET IAW SRM.SDR SWAA2019022129903Angle · corrodedFORWARD CARGO COMPARTMENT RT Z-ANGLE CORRODED BETWEEN BS 500C+11 TO BS 500F. R&R Z ANGLE IAW SRM.SDR SWAA2019022029861Vapor Barrier · debondedRT LOWER VAPOR BARRIER WEB INTERIM REPAIR DISBONDED AT BS 663. REPAIRED BARRIER IAW SRM.
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