N8674B
Service difficulty reports · 115
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 = 'N8674B' 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 = 'N8674B' 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 SWAA2022122284476Structure · crackedRIGHT BREAK PANEL ASSEMBLY CRACKED. RT BREAK ASSY AT STA. 520 BELOW FLOOR BOARD 231UF REMOVED REF SRM 51-40-02. REPLACED RT BREAK ASSY PER SRM 51-40-02.SDR SWAA2022122284478Structure · crackedLT BRAKE ASSY AT BS 520 CRACKED L/H BREAK ASSY. LT BRAKE ASSY AT STA. 520 BELOW FLOORBOARD 231UF REMOVED REF SRM 51-40-02. L/H BREAK ASSY AT STA. 520 BELOW FLOOR BOARD 231UF REMOVED REF SRM 51-40-02. REPLACED L/H BRAKE ASSY AT STA. 520 ON EXPANTION AREA PERSDR SWAA2022112374823Sign · detachedOVERWING EXIT SIGN MID CABIN IS MISSING. INSTALLED OVERWING EXIT SIGN @ MID CABIN?S AFT FACING & FWD FACING COVER PER S.I.P.SDR SWAA2022101760408Battery Pack · inoperativeL2 OVER DOOR EXIT SIGN; L2 ESCAPE SLIDE LIGHT; AFT CABIN LOCATOR SIGN; AND 2 AFT CABIN AISLE LIGHTS INOP. / [01] R/R BATTERY PACK AT POWER SUPPLY M1673. REF AMM 33-51-06. OPS CHK OK.SDR SWAA2022082546074Sign · missingMISSING OVERHEAD EXIT SIGN ABOVE EXIT ROWS / [01] REPLACED MISSING EXIT SIGN LENS IAW AMM 33-51-04SDR SWAA2022032887738Strip · looseFLOOR ILLUMINATION STRIP AT SEAT 12C LOOSE / [01] RE-INSTALLED FLOOR STRIP AT SEAT 12C PER SIPSDR SWAA2021121450951Battery Pack · inoperativeEMERGENCY WXIT LIGHT BATTERY PACK M2816 IS DEAD ; / [01] REPLACED FWD M2816 EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-06-960-805. TESTS GOOD; [02] VERIFIED STEP 1<BR>C/WSDR SWAA2021121450502Fairing · cracked#3 FLAP TRACK FAIRING 542BB FORWARD OUTBOARD EDGE CRACKED. ; / [01] EVALUATED AND FOUND FWD O/B EDGE CRACKED AS MARKED. TAP TEST GOOD AROUND DAMAGE. FOUND TO BE REPAIRABLE IAW SRM 57-53-70-2R-4 REPAIR 4 TABLE 201 AND SRM 51-70-04-2R-10.<BR><BR>CLEANED AND PREPSDR SWAA2021121446982None · crackedFWD CARGO FLOOR STRUCTURE; BAFFLE/INTERCOSTAL AT STATION 500H INBOARD SIDE SUPPORT CLIP CRACKED. DOT 234/10 ; / [01] DRILLED AND REMOVED CRACKED R/H STA500H CLIP IAW SRM 51-40-02-0G-0; [02] VERIFIED NEW CLIP STA 500H R/H SIDE AS P/N 143A7502-158 IAW BOEING DWGSDR SWAA2021121446983None · crackedFWD CARGO FLOOR STRUCTURE; BAFFLE /INTERCOSTAL AT STATION 500H; LEFT SIDE; CLIP CRACKED ON FWD SIDE OF FRAME. DOT 234/11 ; / [01] DRILLED AND REMOVED CLIP STA 500H L/H SIDE IAW SRM 51-40-02-0G-0; [02] VERIFIED NEW CLIP AS P/N 143A7502-159 'A' TAG A66315 IAW BOSDR SWAA2021121445939Angle · crackedA-061 DOT 003 AFT CARGO PIT WASTE TANK ENCLOSURE VERTICAL BEAM AT STA 847+18' LBL 10 LOWER ATTACH ANGLE CRACKED ; / [01] REMOVED CRACKED CLIP IAW SRM 51-40-02.; [02] LOCATED/DRILLED NEW CLIP; 149A8109U114; IAW SRM 51-40-05. A TAG # A94253.; [03] OK TO INSTALL SDR SWAA2021121445184Panel · corrodedA125-04 FWD CARGO PANEL 120 DF CORRODED ; PANEL 120DF / [01] BEGAN REMOVING CORROSION ON FWD CARGO FLOOR PANEL 120DF; FOUND OUT OF LIMITS; DAMAGE EXCEEDS MAX LENGTH IAW B737 SRM 53-00-53-1A-1 FIG 102. CORROSION STILL EXISTS; [02] VERIFIED MATERIAL FOR FWD CARGSDR SWAA2021121445189Angle · corrodedA113-85 AFT CARGO COMPARTMENT STA 767 TO STA 787 L/H Z ANGLE IS CORRODED. ; / [01] REMOVEDCORROSION IAW B737 SRM 5110-02-OG 0; [02] ORIGINAL .040' LOSS .008' REM .032'; OUT OF LIMITS I/A/W SRM 53-00-53-1A-1 FIG 103 VIEW A-A. TOOL# 36649 DUE 12AUG22; [03] CONCUSDR SWAA2021121444768Angle · corrodedA113-85 AFT CARGO COMPARTMENT STA 767 TO STA 787 L/H Z ANGLE IS CORRODED. ; / [01] REMOVEDCORROSION IAW B737 SRM 5110-02-OG 0; [02] ORIGINAL .040' LOSS .008' REM .032'; OUT OF LIMITS I/A/W SRM 53-00-53-1A-1 FIG 103 VIEW A-A. TOOL# 36649 DUE 12AUG22; [03] CONCUSDR SWAA2021121445195Angle · corrodedA113-88 AFT CARGO COMPARTMENT STA 727J TO STA 747 L/H Z ANGLE HAS SEVERAL AREAS OF CORROSION. ; / [01] REMOVED CORROSION IAW WITH B737 SRM 51-10-02-OG 0; [02] ORIGINAL .040' LOSS .006' REM .034'; OUT OF LIMITS I/A/W SRM 53-00-53-1A-1 FIG 103 VIEW A-A. TOOL# 36SDR SWAA2021121444777Angle · corrodedA113-88 AFT CARGO COMPARTMENT STA 727J TO STA 747 L/H Z ANGLE HAS SEVERAL AREAS OF CORROSION. ; / [01] REMOVED CORROSION IAW WITH B737 SRM 51-10-02-OG 0; [02] ORIGINAL .040' LOSS .006' REM .034'; OUT OF LIMITS I/A/W SRM 53-00-53-1A-1 FIG 103 VIEW A-A. TOOL# 36SDR SWAA2021121445584Angle · corrodedA113-94 AFT CARGO COMPARTMENT STA 727H TO STA 727I L/H Z ANGLE HAS SEVERAL AREAS OF CORROSION. ; / [01] REMOVED CORROSION IAW B737 SRM 51-10-02-OG-0; [02] ORIGINAL .040' LOSS .008' REM .032'; OUT OF LIMITS I/A/W SRM 53-00-53-1A-1 FIG 103 VIEW A-A. TOOL# 36649 SDR SWAA2021121444781Angle · corrodedFWD CARGO COMP.LH Z-ANGLE CORRODED AROUND FASTNER HOLES STA.500E-500D LBL25 WL158 #185-013 ; / [01] BEGAN REMOVING CORROSION ON L/H Z ANGLE AT STA 500D TO STA 500E; LBL 25 AND WL 158; ORIGINAL .040' LOSS OF .010' REMAINING .030' FOUND TO BE OUT OF LIMITS IAW SSDR SWAA2021121445192Angle · corrodedFWD CARGO COMP.RH Z-ANGLE CORRODED AROUND FASTNER HOLES STA.500C-500E RBL 25 WL 158 #185-008 ; / [01] BEGAN REMOVING CORROSION ON RH Z ANGLE AT STA 500B-500C RBL 25 AND WL 158; ORIGINAL .040' LOSS OF .011' REMAINING .029' FOUND OUT OF LIMITS IAW SRM 53-00-53-1SDR SWAA2021121444779Angle · corrodedFWD CARGO COMP.RH Z-ANGLE CORRODED AROUND FASTNER HOLES STA.500E-500G RBL 25 WL 158 #185-009 ; / [01] BEGAN REMOVING CORROSION ON RH Z ANGLE AT STA 500E TO 500G RBL 25 AND WL 158; ORIGINAL .040' LOSS OF .008' REMAINING .032' FOUND OUT OF LIMITS IAW SRM 53-00-5SDR SWAA2021121444778Angle · corrodedFWD CARGO COMP.RH Z-ANGLE CORRODED AROUND FASTNER HOLES STA.500B-500C RBL 25 WL 158 ; / [01] BEGAN REMOVING CORROSION ON RH Z ANGLE AT STA 500B-500C RBL 25 AND WL 158; ORIGINAL .029' LOSS OF .011' REMAINING .029' FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-2. CORRSDR SWAA2021121444774Angle · corrodedFWD CARGO COMP.LH Z-ANGLE CORRODED AROUND FASTNER HOLES STA.500H-500I LBL25 WL158 #185-012 / [01] BEGAN REMOVING CORROSION ON LH Z ANGLE AT STA 500H-500I LBL 25 AND WL 158; ORIGINAL .040' LOSS OF .005' REMAINING .035' FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-2.SDR SWAA2021121444773Angle · corrodedFWD CARGO COMP.RH Z-ANGLE CORRODED AROUND FASTNER HOLES STA.500G-500I RBL 25 WL 158 #185-010 ; / [01] BEGAN REMOVING CORROSION ON RH Z ANGLE AT STA 500G TO 500I RBL 25 AND WL 158; ORIGINAL .040' LOSS OF .007' REMAINING .033' FOUND OUT OF LIMITS IAW SRM 53-00-5SDR SWAA2021121445194Angle · corrodedA113-87 A113-87 AFT CARGO COMPARTMENT STA 747 TO STA 767 L/H Z ANGLE HAS SEVERAL AREAS OF CORROSION. ; / [01] REMOVED CORROSION IAW B737 SRM 51-10-02-OG-0; [02] ORIGINAL .040' LOSS .009' REM .031'; OUT OF LIMITS I/A/W SRM 53-00-53-1A-1 FIG 103 VIEW A-A. TOOL# SDR SWAA2021121444780Angle · corrodedFWD CARGO COMP.AFT BULKHEAD BOTTOM ANGLE CORRODED STA.500I LBL25-RBL25 WL 158 #185-011 ; / [01] BEGAN REMOVING CORROSION ON FWD PIT; AFT BH LOWER SUPPORT ANGLE; ORIGINAL .071' LOSS OF .027' REMAINING .044'; MIN ALLOWED .056' FOUND OUT OF LIMITS IAW SRM 53-30-0SDR SWAA2021121445585Angle · corrodedA113-95 AFT CARGO COMPARTMENT STA 727H TO STA 727I R/H Z ANGLE HAS SEVERAL AREAS OF CORROSION. ; / [01] REMOVED CORROSION IAW SRM 51-10-02-0G-0. FOUND ORIGINAL THICKNESS .040'; LOSS .018' AROUND FASTENER HOLES; OUT OF LIMITS IAW SRM 53-00-53-1A-2.; [02] REMAINSDR SWAA2021121444776Angle · corrodedA113-87 A113-87 AFT CARGO COMPARTMENT STA 747 TO STA 767 L/H Z ANGLE HAS SEVERAL AREAS OF CORROSION. ; / [01] REMOVED CORROSION IAW B737 SRM 51-10-02-OG-0; [02] ORIGINAL .040' LOSS .009' REM .031'; OUT OF LIMITS I/A/W SRM 53-00-53-1A-1 FIG 103 VIEW A-A. TOOL# SDR SWAA2021121444782Angle · corrodedA113-91 AFT CARGO COMPARTMENT STA 727I TO STA 727J L/H Z ANGLE HAS SEVERAL AREAS OF CORROSION. ; / [01] REMOVED CORROSION IAW B737 SRM 51-10-02-OG 0; [02] ORIGINAL .040' LOSS .011' REM .029'; OUT OF LIMITS I/A/W SRM 53-00-53-1A-1 FIG 103 VIEW A-A. TOOL# 36649 SDR SWAA2021121445190Angle · corrodedA113-86 AFT CARGO COMPARTMENT STA 747 TO STA 767 R/H Z ANGLE HAS SEVERAL AREAS OF CORROSION. ; / [01] REMOVED CORROSION IAW SRM 51-10-02-0G-0. FOUND ORIGINAL THICKNESS .040'; LOSS ..016' REMAINING MATERIAL .024' AROUND FASTENER HOLES; OUT OF LIMITS IAW SRM 53-SDR SWAA2021121444769Angle · corrodedA113-86 AFT CARGO COMPARTMENT STA 747 TO STA 767 R/H Z ANGLE HAS SEVERAL AREAS OF CORROSION. ; / [01] REMOVED CORROSION IAW SRM 51-10-02-0G-0. FOUND ORIGINAL THICKNESS .040'; LOSS ..016' REMAINING MATERIAL .024' AROUND FASTENER HOLES; OUT OF LIMITS IAW SRM 53-SDR SWAA2021121444783Angle · corrodedA113-93 A113-93 AFT CARGO COMPARTMENT STA 727I TO STA 727J R/H Z ANGLE HAS SEVERAL AREAS OF CORROSION. ; / [01] REMOVED CORROSION IAW SRM 51-10-02-0G-0. FOUND ORIGINAL THICKNESS .040'; LOSS .015' REMAINING MATERIAL .025' AROUND FASTENER HOLES; OUT OF LIMITS IASDR SWAA2021121444770Shield · corrodedFWD CARGO COMP.RH FLOOR SHIELD CORRODED AROUND FASTNER HOLES STA.500-500A RBL25 WL.158 ; / [01] BEGAN REMOVING CORROSION ON SPLASH SHIELD AT STA 500 TO 500A; RBL 25 AND WL 158; ORIGINAL .032' LOSS OF .007' REMAINING .025' FOUND OUT OF LIMITS IAW SRM 53-00-53-1SDR SWAA2021121445191Shield · corrodedFWD CARGO COMP.RH FLOOR SHIELD CORRODED AROUND FASTNER HOLES STA.500-500A RBL25 WL.158. BEGAN REMOVING CORROSION ON SPLASH SHIELD AT STA 500 TO 500A; RBL 25 AND WL 158; ORIGINAL .032' LOSS OF .007' REMAINING .025' FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-2. COSDR SWAA2021121444775Angle · corrodedA113-90 AFT CARGO COMPARTMENT STA 72J7 +14' R/H Z ANGLE IS CORRODED. ; / [01] REMOVED CORROSION IAW SRM 51-10-02-0G-0. FOUND ORIGINAL THICKNESS .040'; LOSS .020' REMAINING MATERIAL .020' AROUND FASTENER HOLES; OUT OF LIMITS IAW SRM 53-00-53-1A-2.; [02] ALL WORSDR SWAA2021121444771Angle · corrodedFWD CARGO COMP.RH Z-ANGLE CORRODED AROUND FASTNER HOLES STA.500C-500E RBL 25 WL 158 #185-008 ; / [01] BEGAN REMOVING CORROSION ON RH Z ANGLE AT STA 500B-500C RBL 25 AND WL 158; ORIGINAL .040' LOSS OF .011' REMAINING .029' FOUND OUT OF LIMITS IAW SRM 53-00-53-1SDR SWAA2021121445197Angle · corrodedFWD CARGO BAY RT Z-ANGLE CORRODED AROUND FASTNER HOLES BS 500E-500G, RBL 25, WL 158. BEGAN REMOVING CORROSION ON THE Z ANGLE, ORIGINAL .040' LOSS OF .008' REMAINING .032', FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-2. CORROSION STILL EXISTS. ALL WORK FOR FWD CASDR SWAA2021121445196Angle · corrodedFWD CARGO COMP.RH Z-ANGLE CORRODED AROUND FASTNER HOLES STA.500B-500C RBL 25 WL 158. BEGAN REMOVING CORROSION ON RH Z ANGLE, ORIGINAL .029' LOSS OF .011' REMAINING .029' FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-2. CORROSION STILL EXISTS. ALL WORK FOR FWD CARGSDR SWAA2021121444761Panel · corrodedA125-03 FWD CARGO FLOOR PANEL 120CF CORRODED ; / [01] REMOVED CORROSION ON PANEL 120CF IAW SRM 51-10-02. PANEL IS OUT OF LIMITS IAW SRM 53-00-53-1A-1 FIGURE 102. EXCEDES MAXIMUM LENGTH DAMAGE.; [02] INSPECTION VERIFIED OUT OF LIMITS; [03] VERIFIED MATERIAL 202SDR SWAA2021121444368Panel · corrodedA113-76 AFT CARGO COMPARTMENT PANEL 140BF EDGES HAVE CORROSION. ; / [01] CORROSION FOUND TO BE LONGER THAN 20IN & DEEPER THAN .10IN OUT OF LIMITS.; [02] INSPECTION VERIFIED LONGER THAN 20 IN.; [03] MATERIAL VERIFIED TO BE 2024-T3-.071 IAW AMM 25-52-01-201-801 SDR SWAA2021121444762None · corrodedA125-04 FWD CARGO FLOOR PANEL 120DF CORRODED ; / [01] REMOVED CORROSION ON PANEL 120DF IAW SRM 51-10-02. PANEL IS OUT OF LIMITS IAW SRM 53-00-53-1A-1 FIGURE 102. EXCEDES MAXIMUM LENGTH DAMAGE.; [02] INSPECTION VERIFIED OUT OF LIMITS; [03] MATERIAL VERIFIED TO SDR SWAA2021121445182Floor Panel · corrodedA125-03 FWD CARGO FLOOR PANEL 120CF CORRODED. REMOVED CORROSION ON PANEL 120CF IAW SRM 51-10-02. PANEL IS OUT OF LIMITS IAW SRM 53-00-53-1A-1 FIGURE 102. EXCEDES MAXIMUM LENGTH DAMAGE. INSPECTION VERIFIED OUT OF LIMITS IAW SRM 53-00-53-1A-1 STEP C. TRIMMED SDR SWAA2021121445183Floor Panel · corrodedA125-04 FWD CARGO FLOOR PANEL 120DF CORRODED ; / [01] REMOVED CORROSION ON PANEL 120DF IAW SRM 51-10-02. PANEL IS OUT OF LIMITS IAW SRM 53-00-53-1A-1 FIGURE 102. EXCEDES MAXIMUM LENGTH DAMAGE.; [02] INSPECTION VERIFIED OUT OF LIMITS; [03] MATERIAL VERIFIED TO SDR SWAA2021111944359Floorboard · corrodedAFT CARGO COMPARTMENT FLOORBOARD 140EF L/H EDGE HAS SIGNS OF CORROSION. CORROSION FOUND TO BE LONGER THAN 20IN & DEEPER THAN .10IN OUT OF LIMITS. ALL WORK FOR AFT PIT FLOOR PANEL 140EF FABRICATION WAS ACCOMPLISHED ON TTG8Q009C1DC.SDR SWAA2021102031497Sign · brokenEMERGENCY EXIT SIGN MID-CABIN BROKEN. / REINSTALLED COVERS PER SIP.SDR SWAA2021092421825Lens · missingCENTER ISLE OVERWING EXIT SIGN LENSE FELL OFF / REINSTALLED LENSE COVER PER SIP OPS CHECK GOODSDR SWAA2021031755288Lens · missingMID CABIN AISLE EXIT SIGN MISSING A LENSE / INSTALLED NEW EMER EXIT LENS AT MID CABIN CEILING AFT SIDE REF MM 33-51-01SDR SWAA2021031554151Cover · detachedCENTER AISLE; AFT-FACING OVERHEAD EMERGENCY EXIT SIGN DETACHED / RESECURED CENTER WING AFT EXIT SIGN COVER PER 'SIP'SDR SWAA2020121035432Skin · gougedGOUGE IN RIGHT HAND SIDE FUSELAGE AFT OF STATION 727H BETWEEN STRINGERS 25R AND 26R. FOUND TO BE OUT OF LIMITS IN AREA B, PER TABLE 107 PER SRM 53-00-01-1A-5. PERMANENT REPAIR REQUIRED WITHIN 50 FLIGHT HOURS. A/C 8674 IS PRE SERVICE BULLETIN 737-21-1149. RSDR SWAA2021081807731Fairing · cracked#2 AFT STRUT FAIRING CRACKED ON AFT INBD FITTINGSTOPPED DRILLED CRACK ON #2 AFT STRUT FAIRING ON AFT INBD FITTING PER EA 20-154-01348 INSPECTOR: E40330ACCOMPLISH OPTION 1 OR OPTION 2. OPTION 1: PERFORM 737-800 SRM 54-50-70-2R-6; REPAIR 6 TO REPAIR THE CRACKED SDR SWAA2021081806873Fairing · cracked#2 AFT STRUT FAIRING CRACKED ON AFT INBD FITTING / STOPPED DRILLED CRACK ON #2 AFT STRUT FAIRING ON AFT INBD FITTING PER EA 20-154-01348
Back to N8674B