N8656B
Service difficulty reports · 168
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 = 'N8656B' 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 = 'N8656B' 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 SWAA2022082538743Attach Angle · corrodedCORROSION ON FSD THRESHOLD ATTACH ANGLE BS308-318 RBL 58 WL208 / [01] REMOVED COROSION ON FSD THRESHOLD ATTACH ANGEL AT BS 308 RBL 58 WL 208; 1''X1''X.015'' FOUND TO BE OUT OF LIMITS IAW SRM 53-10-15-1A-2.;[02] CERTIFY;[03] VERIFIED OUT OF LIMITS.;[04] REMOVEDSDR SWAA2022082538748Web · corrodedCORROSION ON FWD CARGO BAY THRESHOLD AT RBL 28 BS 440+8; BS 440+14; BS 460+2; BS 460+4; BS 460+9; BS 460+11; BS 460+18; BS 480+2; BS 480+4. / [01] REMOVED CORROSION FROM FCD THRESHOLD WEB AT BS 440+8 MEASURED 1.8'W X 1.8'L AND 0.004' DEEP; ORIGINAL THICKNESS OSDR SWAA2022082538749Shield · corrodedCORROSION ON FWD CARGO BAY AFT DOOR SHIELD AT RBL 23 BS 500+18. / [01] UPDATED MEASUREMENTS;[02] FIXED MEASUREMENTS 7-12;[03] REMOVED DAMAGE IN A 0.5'X0.5'DEPTH 0.005. AT BS500+18 RBL23. SHIELD IS OUT OF LIMITS DUE TO NO ALLOWABLE DAMAGE LIMIT. REPAIR BY REPLASDR SWAA2022082538754Sidewall Support · corrodedCORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 24 BS 500D+15; BS 500D+20; BS 500E+2; BS 500E+7; BS 500E+11; BS 500E+20; BS 500F+2; BS 500F+7; BS 500F+2; BS 500F+7. / [01] REMOVED CORROSION FROM FCB R/H FLOOR TO SIDEWALL SUPPORT AT BS 500D+20 RBL 2SDR SWAA2022091538093Stringer Clip · crackedREJECT STRINGER 10R CLIP AT B S 927 IS CRACKED / [01] UPDATED MEASUREMENT TABLE;[02] SRM DOES NOT HAVE REPAIR LIMITS FOR CRACKED STR CLIPS. OUT OF LIMITS AND TO BE REPLACED IAW SRM 51010-02-0G-0 STEP 9.;[03] REFERENCE IS SRM 51-10-02-0G-0 STEP 9;[04] CERTIFY;[SDR SWAA2022082437843Floor Panel · pulledCABIN FLOOR PANEL 232CF UPPER SKIN HAS PULLED STRANDS AT THE AFT O/B CORNER. (MARKED) / [01] IDENTIFIED PANEL 232CF IAW SRM 53-00-50-0I-1 TABLE 3 FIG 3.<BR><BR>DAMAGE NOTED IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PARA 4B<BR><BR>TO BE REPAIRED ISDR SWAA2022082437844Floor Panel · pulledFLOOR PANEL 232DF UPPER SKIN HAS PULLED STRANDS ALONG THE AFT EDGE. (MARKED) / [01] IDENTIFIED PANEL 232DF IAW SRM 53-00-50-0I-1 TABLE 3 FIG 3.<BR><BR>DAMAGE NOTED IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PARA 4B OK TO POT EXPOSED CORE IAW SRM 5SDR SWAA2022082537833Support · corrodedCORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT LBL 21 BS 727F+6; BS 727F+16; BS 727G+8; BS 727G+10; BS 727G+19; BS 727H; BS 727H+6. / [01] REMOVED CORROSION FROM ACB L/H FLOOR TO SIDEWALL SUPPORT AT BS 727H LBL 21 MEASURED 2'W X 1'L AND 100% MATERIAL SDR SWAA2022082537831Rail · corrodedCORROSION ON AFT CARGO BAY RAIL AT RBL 13 BS 767+5. / [01] SRM 53-00-53-1A-2 IS FOUND TO BE APPLICABLE;;[15] INSTALLED NEW REINFORCING CHANNEL IAW SRM 53-00-53-2R-3 REPAIR 3;[16] EDITED MEASUREMENTS;[17] VERIFIED CORRECTIVE ACTION #15; 16 AND MEASUREMENT TABLESDR SWAA2022082537830Channel · corrodedCORROSION ON AFT CARGO BAY RAIL AT RBL 8 BS 767+5. / [01] ENTERED MEASUREMENTS;[09] LOCATED AND DRILLED NEW REINFORCING CHANNEL LOT #1487793-1 IAW SRM 53-00-53-2R-2 REPAIR 2 TABLE 205 ALTERNATIVE 5. OK TO APPLY PRIMER;[10] VERIFIED CORRECTIVE ACTION #1 OK TO ASDR SWAA2022082537820Shield · corrodedCORROSION ON AFT CARGO BAY AFT DOOR SHIELD AT RBL 21 BS 847+5; BS 847+11; BS 847+14. / [01] REMOVED AFT DOOR SHIELD AT ACB RBL 21 BS 847 TO BS 867 IAW SRM 51-40-02;[02] SRM 53-00-53-1A-2 IS EFFECTIVE FOR THIS EVALUATION. NO ALLOWABLE DAMAGE FOUND FOR THIS PARSDR SWAA2022082537819Support · corrodedCORROSION ON AFT CARGO BAY AFT LOWER BULKHEAD SUPPORT AT BS 947 RBL 10; RBL 12; RBL 15. / [01] REMOVED AFT LWR BULKHEAD SUPPORT AT BS 947.5 RBL 22 TO LBL10 IAW SRM 51-40-02;[02] THERE IS NO SRM ALLOWABLE DAMAGE FOR ACB AFT LOWER BULKHEAD SUPPORT AT BS947. PARTSDR SWAA2022082537832Shield · corrodedCORROSION ON AFT CARGO BAY FWD DOOR SHIELD AT RBL 21 BS 767+5; BS 767+9; BS 767+12; BS 767+16. / [01] ENTERED MEASUREMENTS;[02] SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2 IS EFFECTIVE FOR THIS EVALUATION.<BR>NO ALLOWABLE GIVEN IN B737-800 SRM. REPAIR BY REPLACEMENT SDR SWAA2022082537841Support · corrodedCORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 21 BS 727I+1; BS 727I+3; BS 727I+6-727I+11; BS 727I+12-727J+4; 727J+5-727J+16; BS 727J+18; BS 747-747+12; BS 747+14-747+19. / [01] ENTERED MEASUREMENTS;[06] FABRICATED AND LOCATED AND DRILLED NEW SIDESDR SWAA2022082437816Intercostal · crackedCRACK ON FWD PASSENGER CABIN INTERCOSTAL AT LBL 11 BS 344+9. / [01] UPDATED MEASUREMENT TABLE;[02] REMOVED INTERCOSTAL AT BS344 TO BS360 BL0 FOR ACCESS IAW SRM 51-40-02-0G-0;[03] CRACK ON UPPER FLANGE OF INTERCOSTAL EXCEEDS REPAIRABLE LIMIT IN SRM 53-10-51-1A-SDR SWAA2022082437814Intercostal · crackedCRACK ON FWD PASSENGER CABIN INTERCOSTAL AT RBL 12 BS 344+5; BS 344+9. / [01] UPDATED CHART.;[02] REMOVED INTERCOSTAL AT RBL 12 BS 344+5 - BS 344+9 IAW <BR>SRM 51-40-02-0G-0.;[03] EVALUATED CRACK ON UPPER FLANGE OF INTERCOSTAL EXCEEDS REPAIRABLE LIMIT IN SRM 5SDR SWAA2022082437825Attach Angle · crackedCRACK ON AFT CARGO BAY AFT BULKHEAD SUPPORT ATTACH ANGEL AT LBL 10 BS 847+18. / [01] REMOVED AND REPLACED ACB AFT BULKHEAD SUPPORT ATTACH ANGLE AT LBL 10 BS 847+18 IAW SRM 51-40-02 AND BOEING DWG 149A8102;[02] INSPECTED & VERIFIED CORRECTIVE ACTION ITEM 1.;[03SDR SWAA2022082237821Web · corrodedCORROSION ON AFT CARGO BAY THRESHOLD AT RBL 21 BS 787+8; RBL 26 BS 787+14-807+6; RBL 26 BS 807+8; RBL 26 BS 807+12; RBL 26 BS 807+19; RBL 26 BS 827+1-827+11. / 02] 1.- REMOVED CORROSION FROM ACB THRESHOLD AT RBL 21; BS 787+8; IS FOUND IN LIMITS IAW SRM 53-60-1SDR SWAA2022092220224Skin · defectiveANOMALY ON EXTERNAL FUSELAGE SKIN BS970 - BS887 S-4R TO S-6R. MARKED. BS887 - BS960 S-6R TO S-8R. MARKED. BS887 - BS947 S-8R TO S-11R. MARKED. BS887 - BS928 S-11R TO S-13R. MARKED. BS887 - BS908 S-13R TO S-14R. MARKED. / [01] PERFORMED CLAD PENETRATION TEST INSDR SWAA2022092220225Skin · defectiveANOMALY ON EXTERNAL FUSELAGE SKIN BS858 - BS887 S-4R - S-10R. MARKED. / [01] PERFORMED CLAD PENETRATION TEST IN SEVERAL LOCATIONS ON SKIN PANEL BS 858 TO 887 S-4R TO S-10R LISTED BELOW PER SRM51-10-07-0G-0 PARA. 5D-E<BR><BR>1) BS 867+5.5' 3.5' BELOW STR 9R<BR>SDR SWAA2022092220227Skin · defectiveANOMALY ON EXTERNAL FUSELAGE SKIN BS887 - BS987 S-2R TO S-4R. MARKED. / [01] PERFORMED CLAD PENETRATION TEST IN SEVERAL LOCATIONS ON SKIN PANEL BS 887 TO 987 S-2R TO S-4R LISTED BELOW PER SRM51-10-07-0G-0 PARA. 5D-E<BR><BR>1) BS 907+10' 4' BELOW STR 3R<BR>2) BSDR SWAA2022092220228Skin · defectiveANOMALY ON EXTERNAL FUSELAGE SKIN BS845 - BS887 S-10R TO S-14R. MARKED. / [01] PERFORMED CLAD PENETRATION TEST IN SEVERAL LOCATIONS ON SKIN PANEL BS 845 TO 887 S-10R TO S-14R LISTED BELOW PER SRM51-10-07-0G-0 PARA. 5D-E<BR><BR>1) BS 867+13' 1.5' BELOW STR 13R<SDR SWAA2022092218943Skin · defectiveANOMALY ON EXTERNAL FUSELAGE SKIN S-2L TO S-4L BS887 - BS947+5. MARKED / [01] PERFORMED CLAD PENETRATION TEST IN SEVERAL LOCATIONS ON SKIN PANEL BS 887 TO 1016 S-2L TO S-4L LISTED BELOW PER SRM 51-10-07-0G-0 PARA. 5D-E<BR><BR>1) BS 887-907 S-2L TO S-3L<BR>2) BSDR SWAA2022092218944Skin · defectiveANOMALY ON EXTERNAL FUSELAGE SKIN S-4L TO S-6L BS887 - BS947+6. MARKED S-6L TO S-9L BS927 - BS947. MARKED S-9L TO S-11L BS887 - BS927. MARKED. S-9L TO S-10L BS927 - BS927+15. MARKED. S-11L TO S-14L BS887 - BS907. MARKED. / [01] PERFORMED CLAD PENETRATION TEST SDR SWAA2022092218946Skin · defectiveANOMALY ON EXTERNAL FUSELAGE SKIN S-10L TO S-14L BS827 - BS887. MARKED. / [01] PERFORMED CLAD PENETRATION TEST IN SEVERAL LOCATIONS ON SKIN PANEL BS 727 TO 887 S-10L TO S-14L LISTED BELOW PER SRM 51-10-07-0G-0 PARA. 5D-E<BR><BR>1) BS 827-847 S-13L TO S-14L<BR>SDR SWAA2022092218948Skin · defectiveANOMALY ON EXTERNAL FUSELAGE SKIN S-16L TO S-19L BS787 - BS827. MARKED. / [01] EVALUATED ANOMALIES ON FUSELAGE SKIN AT BS 787+14.5 6.5'BELOW STR 19L D=.0006'; BS 787+12 1'BELOW STR 18L D=.0005'; BS 787+11 6'BELOW STR 17L D=.001'; BS 807+6 6'BELOW STR 18L D=.00SDR SWAA2022092218947Skin · defectiveANOMALY ON EXTERNAL FUSELAGE SKIN S-14L TO S-16L BS827 - BS887. MARKED. / [01] PERFORMED CLAD PENETRATION TEST IN SEVERAL LOCATIONS ON SKIN PANEL BS 727 TO 887 S-14L TO S-23L LISTED BELOW PER SRM51-10-07-0G-0 PARA. 5D-E<BR><BR>1) BS 807-827 S-16L TO S-17L<BR>2SDR SWAA2022092217456Skin · corrodedSKIN PITTING AND ANOMALIES BS 907 - BS 927 STR 6L - STR 7L / [01] REMOVED SKIN PITTING AND ANOMALIES FROM FUSELAGE SKIN AT BS 907-927; STR 6L-7L IAW SRM 51-10-02-0;[02] VERIFIED CORRECTIVE ACTION ITEM 1.;[03] ACCOMPLISHED UT INSPECTION OF BLENDED AREA LOWEST TSDR SWAA2022091517245None · inoperativeEMERGENCY EXIT LIGHT BATTERY PACK AT M1673 / [01] REMOVED AND REPLACED BATTERY PACK M1673 PER AMM 33-51-06-960-805 STEPS 4. E. (1)-(5);[02] UPDATED PARTS REQUIREMENT BLOCK;[03] CERTIFIED ITEM 1 AND 2SDR SWAA2022091517244None · inoperativeEMERGENCY EXIT LIGHT BATTERY PACK AT M1670 WILL NOT CHARGE / [01] REMOVED AND REPLACED BATTERY PACK M1670 PER AMM 33-51-06-960-805 STEPS 4. E. (1)-(5);[02] UPDATED PARTS REQUIREMENT BLOCK;[03] CERTIFIED ITEM 1 AND 2SDR SWAA2022091517243None · inoperativeEMERGENCY LIGHT PATTERY PACK AT M1672 WILL NOT CHARGE / [01] REMOVED AND REPLACED BATTERY PACK M1672 PER AMM 33-51-06-960-805 STEPS 4. E. (1)-(5);[02] UPDATED PARTS INFORMATION;[03] CERTIFIED ITEM 1SDR SWAA2022050200066Skin · corrodedTRANSFERRED FROM FAULT TTG8Q00AP7ZC. AFTER PAINT STRIP FOUND SOME SKIN PITTING AND SKIN ANOMALIES FROM APPROXIMATELY STA 867 TO 928 STR 14 TO 14 OVER THE CROWN /SDR SWAA2022020869405Skin · corrodedAFTER PAINT STRIP FOUND SOME SKIN PITTING AND SKIN ANOMALIES FROM APPROXIMATLY STA 867 TO 928 STR 14 TO 14 OVER THE CROWN ; /SDR SWAA2022013164829Skin · corrodedAFTER PAINT STRIP FOUND SOME SKIN PITTING AND SKIN ANOMALIES FROM APPROXIMATELY STA 867 TO 928 STR 14 TO 14 OVER THE CROWN.SDR SWAA2021080298125Light · brokenCENTER CABIN OVERJEAD EMERGECNY EXIT LIGHT BROKEN ( MX NOTE ) / REMOVED AND REPLACED CENTER CABIN OVERHEAD EMERGENCY EXIT SIGN PER AMM 33-51-02. CLR # 91927SDR SWAA2021030452790Battery Pack · failedFWD RIGHT REAR BATT PACK FAILED / REPLACED FWD RIGHT BATT PACK PER 33-51-06 OF THE AMMSDR SWAA2021081326528Bracket · crackedRH WING BRACKET O/B OF DEFLECTION CONTROL RIB TO WEB IS CRACKED / REMOVED AND REPLACED R/H WING BRACKET O/B OF DEFLECTION CONTROL RIB TO WEB IAW SRM 51-40-02-0G-0 AND DWG 115A6200 REV A MPN 115A6260-2 A TAG A90889SDR SWAA2021072126773Panel · crackedPASSENGER CABIN; EXPANSION PNL CRACKED AT STA 540; LBL1; WL208. / REMOVED CRACKED PASSENGER CABIN EXPANSION PNL AT STA 540 LBL 1 WL 208 AND REPLACED WITH NEW EXPANSION PNL P/N 143A5240-35 IAW SRM 51-40-02-0G-0 AND BOEING DWG 143A0060 REV - ATAG WN8693SDR SWAA2021072126772Panel · crackedPASSENGER CABIN; EXPANSION PNL CRACKED AT STA 540; RBL1; WL 208. / REMOVED CRACKED PASSENGER CABIN EXPANSION PNL AT STA 540 RBL 1 WL 208 AND REPLACED WITH NEW EXPANSION PNL P/N 143A5240-36 IAW SRM 51-40-02-0G-0 AND BOEING DWG 143A0060 REV - ATAG WN8998SDR SWAA2021071626530Rib · corrodedPANEL 424 #2 ENGINE OB COWL HAS CRACK AT ACCESS DOOR CUTOUT ON INTERIOR RIB SUPPORT AT LATCH SIDE / REMOVED CRACKED SHIELD AT # 2 ENG O/B COWL PNL 424 IAW SRM 51-40-02-0G-0 DRILLED NEW SHIELD IAW SRM 51-40-05-0G-0 AND CMM 71-13-30 INSTALLED NEW SHIELD IAW SRM SDR SWAA2020111026527Lens · crackedRIGHT AFT OVERWING ILLUMINATION LIGHT LENSE CRACKED. REPLACED RIGHT AFT SLIDE/OVERWING LIGHT LENS, IAW AMM 33-51-04-960-801 STEPS 2F (1) (A) AND (D) A TAG A91524.SDR SWAA2021071526503Angle · corrodedFWD PIT STA 418 FLOOR SUPPORT SHIELD UPPER SURFACE CORRODED AT RBL24 AND W/L157 / REMOVED CORROSION ON R/H Z-ANGLE AT STA 418 IN FWD CARGO COMPARTMENT IAW SRM 51-10-02-0G-0. VERIFIED LIMITS ORIGINAL THICKNESS .040'; LOSS OF .006' REMAINING .034' OUT OF LIMITS SDR SWAA2021071526492Shield · corrodedFWD PIT STA 438 FLOOR SUPPORT SHIELD UPPER SURFACE CORRODED STA RBL24 AND W/L157 / REMOVED CORROSION ON FWD SHIELD IN FWD CARGO COMPARTMENT AT STA 438; RBL 24 IAW SRM 51-10-02-0G-0. VERIFIED LIMITS ORIGINAL THICKNESS .032; LOSS OF .013; REMAINING .019' OUT OF SDR SWAA2021071526496Rail · corrodedFWD PIT STA 500I LATERAL FLOOR SUPPORT UPPER SURFACE CORRODED FROM LBL24 TO RBL24 AND W/L157 / EVALUATED CORROSION AT FWD PIT STA 500I FLOOR SUPPORT RAIL LBL 24 RBL 24 W/L 157 100% MATERIAL LOSS FOUND. NO PUBLICATION OF LIMITS WAS FOUND. REMOVED AND REPLACED FSDR SWAA2021071526099Support Angle · bentLEFT WING TRAILING EDGE PANEL 551FB WIRE BUNDLE SUPPORT ANGLE DAMAGED/BENT. MARKED. / REMOVED AND INSTALLED NEW LEFT WING TRAILING EDGE PANEL 551FB WIRE BUNDLE SUPPORT ANGLE IAW SRM 51-40-02-0G-0 AND BOEING DWG # 115A2710 REV - A TAG # A90358SDR SWAA2021071426497Support · corrodedFWD PIT STA 500I SIDEWALL SUPPORT UPPER SURFACE CORRODED AT RBL25 AND W/L157 / REMOVED CORROSION ON FWD PIT STA 500I; RBL 25 SIDE WALL SUPPORT ANGLE ORIGINAL MATERIAL THICKNESS .071 LOSS OF .003 WITH .068 REMAINING FOUND TO BE OUT OF LIMITS DUE TO NO PUBLISHEDSDR SWAA2021040826499Angle · corrodedAFT CARGO COMPARTMEMT R/H Z-ANGLE; RBL 20; WL 156; BS 727C + 16' - 767 CORRODED IN MULTIPLE PLACES / BLENDED AND REMOVED CORROSION AFT CARGO COMPARTMENT R/H Z ANGLE RBL 20 WL 156 BS 727C+16 - 767 AND VERIFIED WITH 10X MAGNIFYING IAW SRM 51-10-02-0G-0 ORIGINAL SDR SWAA2021040726092Floor Panel · corrodedFWD CARGO COMPT. FLOOR PANEL 120AF HAS CORROSION AROUND EDGES / EVALUATED CORROSION ON FWD CARGO COMPT FLOOR PANEL 120AF TOTAL ACCUMULATED DAMAGE FOUND TO BE MORE THAN THE 20' MAXIMUM ALLOWED OUT OF LIMITS IAW SRM 53-00-53-1A-1 FABRICATED NEW FLOOR PANEL 120AFSDR SWAA2021040726091Floor Panel · corrodedFWD CARGO COMPT. FLOOR PANEL 120BF HAS CORROSION AROUND EDGES ALSO MISALIGNED HOLES ON ONE SIDE / EVALUATED CORROSION AS OUT OF LIMITS DAMAGE GREATER THAN 20' IAW SRM SRM 53-00-53-1A-1 FIGURE 102. VERIFIED NEW MATERIAL AS 2024 T3 0.071' ATAG# GO6775 IAW AMM 25SDR SWAA2021040726088Floor Panel · corrodedFWD CARGO COMPT. FLOOR PANEL 120CF HAS CORROSION AROUND EDGES / REMOVED CORROSION AT FWD CARGO COMPT FLOOR PANEL 120CF CORROSION EXCESS MORE THAN 20' INCHES IS OUT OF LIMITS IAW SRM 53-00-53-1A-1 VERIFIED NEW MATERIAL AND FABRICATED NEW PNL 120CF IAW SRM 51-40
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