N8677A
Service difficulty reports · 118
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 = 'N8677A' 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 = 'N8677A' 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 SWAA2024012936529Floor Support · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE; RIGHT SIDE PLATE HAS AREAS OF UPPER AND LOWER SURFACE CORROSION FROM STA747+2 - STA747+18<[01] REMOVED CORROSION FROM AFT CARGO R/H SIDE PLATE FROM STA 747+2 TO STA 747+18. ORIGINAL MATERIAL THICKNESS IS 0.040?; MAX MATERSDR SWAA2024012936593Plate · corrodedFWD. CARGO BILGE; R/H SIDEPLATE CORRODED HOLES FROM BS 490R-BS 500A.<[01] BLENDED CORROSION PER SRM 51-10-02. DAMAGE REMOVAL FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] VERIFIED WORK IN C/A #1;[03] REMOVED AND REPLACED SIDEPLATE SHIELD ASSY PER SRM 5SDR SWAA2024012936614Plate · corrodedFWD. CARGO; R/H SIDEPLATE HAS CORROSION AT HOLES FROM BS500B-BS500+10.<[01] BLENDED CORROSION PER SRM 51-10-02. DAMAGE REMOVAL FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] THIS SECTION OF SIDE PLATE TO BE REPLACED NON NR# TTG8Q00QLSX7 FROM STA. 500A TSDR SWAA2024012936598Plate · corrodedFWD. CARGO; R/H SIDEPLATE HAS CORROSION AT HOLES FROM BS 500E-500F.<[01] THIS SECTION TO BE REPLACED ON TASK CARD TTG8Q00QLSX7;[02] BLENDED AREAS; REMOVED .007' MATERIAL. FOUND TO BE OUT OF LIMITS PER SRM 53-020-53-1A-2. THIS SECTION TO BE REPLACED ON TASK CARSDR SWAA2024012936602Plate · corrodedFWD. CARGO; R/H SIDEPLATE HAS CORROSION AT HOLES FROM BS 500F-BS 500G.<[01] THIS SECTION TO BE REPLACED ON TASK CARD TTG8Q00QLSX7;[02] BLENDED AREAS; REMOVED .009' MATERIAL. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. THIS SECTION TO BE REPLACED ON TASK CSDR SWAA2024012936605Plate · corrodedFWD. CARGO; R/H SIDEPLATE HAS CORROSION AT HOLES FROM BS 500G-BS 500H.<[01] THIS SECTION TO BE REPLACED ON TASK CARD TTG8Q00QLSX7;[02] BLENDED AREAS; REMOVED .007' MATERIAL. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. THIS SECTION TO BE REPLACED ON TASK CSDR SWAA2024012936607Plate · corrodedFWD. CARGO; R/H SIDEPLATE HAS CORROSION AT HOLES FROM BS 500H-BS 500I.<[01] THIS SECTION TO BE REPLACED ON TASK CARD TTG8Q00QLSX7;[02] BLENDED AREAS; REMOVED .007' MATERIAL. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. THIS SECTION TO BE REPLACED ON TASK CSDR SWAA2024012636594Plate · corrodedFWD. CARGO; L/H SIDEPLATE HAS CORROSION AT HOLES FROM BS 500B+16.<[01] BLENDED AREAS. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2;[02] BLENDED AREAS; REMOVED 0.008' MATERIAL. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2;[03] FABRICATED REPLACEMENT SECTISDR SWAA2024012636601Plate · corrodedFWD. CARGO; L/H SIDEPLATE HAS CORROSION AT HOLES FROM BS 500E-BS 500F.<[01] REMOVE DAMAGE(0.008' MATERIAL) FOUND TO BE OUT OF LIMIT PER SRM 53-00-53-1A-2.<BR>THIS SECTION TO BE REPLACED ON TTG8Q00QLSX2;[02] REMOVE DAMAGE(0.008' MATERIAL) FOUND TO BE OUT OF LIMSDR SWAA2024012636603Plate · corrodedFWD. CARGO; L/H SIDEPLATE HAS CORROSION AT HOLES FROM BS 500F-BS 500G.<[01] REMOVE DAMAGE(0.008' MATERIAL) FOUND TO BE OUT OF LIMIT PER SRM 53-00-53-1A-2.<BR>THIS SECTION TO BE REPLACED ON TTG8Q00QLSX2;[02] REMOVE DAMAGE(0.008' MATERIAL) FOUND TO BE OUT OF LIMSDR SWAA2024012636486Strap · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE; MULTIPLE AREAS OF CORROSION ON FLOOR SUPPORT STRAP AT STA767+5<[01] FLOOR SUPPORT STRAP TO BE REPLACED NEW REF SRM 53-00-53;[02] VERIFIED CORRECTIVE ACTION #1SDR SWAA2024012536512Plate · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE; LEFT SIDE PLATE HAS SURFACE CORROSION AT STA 727C+16<[01] REMOVED CORROSION FROM AFT CARGO LEFT SIDE PLATE FROM STA 727C+16?. ORIGINALS MATERIAL THICKNESS IS 0.040?; MAX MATERIAL LOSS IS 0.007?; MAX ALLOWED IS 0.004?; FOUSDR SWAA2024012536467Plate · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE; LEFT SIDE PLATE HAS AREAS OF SURFACE CORROSION FROM STA 727D+3- STA727D+6<[01] REMOVED CORROSION FROM AFT CARGO LEFT SIDE PLATE FROM STA 727D+3 TO STA 727D+6. ORIGINALS MATERIAL THICKNESS IS 0.040?; MAX MATERIAL LOSS IS 0SDR SWAA2024012536468Plate · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE; LEFT SIDE PLATE HAS AREAS OF SURFACE CORROSION FROM STA 727J+6 - STA727J+14<[01] REMOVED CORROSION FROM AFT CARGO LEFT SIDE PLATE FROM STA 727J +6 - STA 727J+14. ORIGINAL MATERIAL THICKNESS IS 0.040?; MAX MATERIAL LOSS ISSDR SWAA2024012536516Plate · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE; LEFT SIDE PLATE HAS AREAS OF SURFACE CORROSION FROM STA 727I+10- STA727I+18<[01] REMOVED CORROSION FROM AFT CARGO LEFT SIDE PLATE FROM STA 727I +10- STA 727+18. ORIGINAL MATERIAL THICKNESS IS 0.040?; MAX MATERIAL LOSS IS SDR SWAA2024012536470Plate · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE; LEFT SIDE PLATE HAS AREAS OF SURFACE CORROSION FROM STA 747+6- STA747+14<[01] REMOVED CORROSION FROM AFT CARGO LEFT SIDE PLATE FROM STA 747 +6 - STA 747+14. ORIGINAL MATERIAL THICKNESS IS 0.040?; MAX MATERIAL LOSS IS 0.00SDR SWAA2024012536471Plate · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE; LEFT SIDE PLATE HAS AREAS OF SURFACE CORROSION FROM STA 767+10- STA767+15<[01] REMOVED CORROSION FROM AFT CARGO LEFT SIDE PLATE FROM STA 767 +10- STA767+15. ORIGINALS MATERIAL THICKNESS IS 0.040?; MAX MATERIAL LOSS IS 0.0SDR SWAA2024012536517Plate · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE; LEFT SIDE PLATE HAS SURFACE CORROSION AT STA807<[01] REMOVED CORROSION FROM AFT CARGO LEFT SIDE PLATE FROM STA 807. ORIGINAL MATERIAL THICKNESS IS 0.040?; MAX MATERIAL LOSS IS 0.008?; MAX ALLOWED IS 0.004?; FOUND TO BE OUSDR SWAA2024012536518Plate · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE; LEFT SIDE PLATE HAS SURFACE CORROSION AT STA727E+13<[01] REMOVED CORROSION FROM AFT CARGO LEFT SIDE PLATE FROM STA 727E+13. ORIGINAL MATERIAL THICKNESS IS 0.040?; MAX MATERIAL LOSS IS 0.008?; MAX ALLOWED IS 0.004?; FOUND SDR SWAA2024012536475Plate · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE; LEFT SIDE PLATE HAS SURFACE CORROSION AT STA727E+16<[01] REMOVED CORROSION FROM AFT CARGO LEFT SIDE PLATE FROM STA 727E+16. ORIGINAL MATERIAL THICKNESS IS 0.040?; MAX MATERIAL LOSS IS 0.008?; MAX ALLOWED IS 0.004?; FOUND SDR SWAA2024012536477Plate · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE; LEFT SIDE PLATE HAS SURFACE CORROSION AT STA727F+9<[01] REMOVED CORROSION FROM AFT CARGO LEFT SIDE PLATE FROM STA 727F +9. ORIGINAL MATERIAL THICKNESS IS 0.040?; MAX MATERIAL LOSS IS 0.008?; MAX ALLOWED IS 0.004?; FOUND TSDR SWAA2024012536520Plate · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE; LEFT SIDE PLATE HAS SURFACE CORROSION AT STA727G+6<[01] REMOVED CORROSION FROM AFT CARGO LEFT SIDE PLATE FROM STA 727+6. ORIGINAL MATERIAL THICKNESS IS 0.040?; MAX MATERIAL LOSS IS 0.008?; MAX ALLOWED IS 0.004?; FOUND TO SDR SWAA2024012536478Plate · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE; RIGHT SIDE PLATE HAS SURFACE CORROSION AT STA727+15<[01] REMOVED CORROSION FROM AFT CARGO R/H SIDE PLATE FROM STA 727+15. ORIGINAL MATERIAL THICKNESS IS 0.040?; MAX MATERIAL LOSS IS 0.008?; MAX ALLOWED IS 0.004?; FOUND TOSDR SWAA2024012536523Plate · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE; RIGHT SIDE PLATE HAS SURFACE CORROSION AT STA727A+12<[01] REMOVED CORROSION FROM AFT CARGO R/H SIDE PLATE FROM STA 727+12. ORIGINAL MATERIAL THICKNESS IS 0.040?; MAX MATERIAL LOSS IS 0.006?; MAX ALLOWED IS 0.004?; FOUND TSDR SWAA2024012536525Plate · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE; RIGHT SIDE PLATE HAS SURFACE CORROSION AT STA727E+12.5<[01] REMOVED CORROSION FROM AFT CARGO R/H SIDE PLATE FROM STA 727E+12.5. ORIGINAL MATERIAL THICKNESS IS 0.040?; MAX MATERIAL LOSS IS 0.005?; MAX ALLOWED IS 0.004?; FOSDR SWAA2024012536479Plate · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE; RIGHT SIDE PLATE HAS SURFACE CORROSION AT STA727F<[01] REMOVED CORROSION FROM AFT CARGO R/H SIDE PLATE FROM STA 727F ORIGINAL MATERIAL THICKNESS IS 0.040?; MAX MATERIAL LOSS IS 0.006?; MAX ALLOWED IS 0.004?; FOUND TO BE OSDR SWAA2024012536526Plate · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE; RIGHT SIDE PLATE HAS SURFACE CORROSION AT STA727G<[01] REMOVED CORROSION FROM AFT CARGO R/H SIDE PLATE FROM STA 727G. ORIGINAL MATERIAL THICKNESS IS 0.040?; MAX MATERIAL LOSS IS 0.008?; MAX ALLOWED IS 0.004?; FOUND TO BE SDR SWAA2024012536480Plate · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE; RIGHT SIDE PLATE HAS SURFACE CORROSION AT STA727F+9<[01] REMOVED CORROSION FROM AFT CARGO R/H SIDE PLATE FROM STA 727F+9. ORIGINAL MATERIAL THICKNESS IS 0.040?; MAX MATERIAL LOSS IS 0.008?; MAX ALLOWED IS 0.004?; FOUND TOSDR SWAA2024012536527Plate · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE; RIGHT SIDE PLATE HAS SURFACE CORROSION AT STA727F+19<[01] REMOVED CORROSION FROM AFT CARGO R/H SIDE PLATE FROM STA 727F+19. ORIGINAL MATERIAL THICKNESS IS 0.040?; MAX MATERIAL LOSS IS 0.006?; MAX ALLOWED IS 0.004?; FOUND SDR SWAA2024012536481Plate · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE; RIGHT SIDE PLATE HAS AREAS OF SURFACE CORROSION FROM STA727H+6 - STA727H+16<[01] REMOVED CORROSION FROM AFT CARGO R/H SIDE PLATE FROM STA 727H+6 TO STA 727H+16. ORIGINAL MATERIAL THICKNESS IS 0.040?; MAX MATERIAL LOSS IS SDR SWAA2024012536482Plate · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE; RIGHT SIDE PLATE HAS AREAS OF SURFACE CORROSION FROM STA727I+7 - STA727I+16<[01] REMOVED CORROSION FROM AFT CARGO R/H SIDE PLATE FROM STA 727I+7 TO STA 727I+16 ORIGINAL MATERIAL THICKNESS IS 0.040?; MAX MATERIAL LOSS IS 0SDR SWAA2024012436595Plate · corrodedFWD. CARGO; R/H SIDEPLATE HAS CORROSION AT HOLES FROM BS 500C-BS 500D.<[01] BLENDED CORROSION PER SRM 51-10-02. DAMAGE REMOVAL FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] REMOVED AND REPLACED R/H TRANSITION ANGLE FROM 727 A TO 727 I PER SRM 51-10-02;SDR SWAA2024012936189Seal · cracked343AT SLIDER SEAL RETAINER CRACKED.<[01] REPLACED BLADE SEAL ASSY PER SRM 51-40-02.;[02] C/W INSPECTIONSDR SWAA2024012936186Seal · crackedSLIDING SEAL RETAINER CRACKED ON PANEL 333AT<[01] REPLACED BLADE SEAL ASSY PER SRM 51-40-02.;[02] C/W INSPECTIONSDR SWAA2023071076473Light · inoperativeL2 EMERGENCY LIGHT INOP.<[01] RELAMPED L2 SLIDE EMERGENCY LIGHT IAW AMM. 33-51-04. OPS CHECK GOOD.SDR SWAA2023041726470Panel · crackedAFT CARGO LH CENTER PANEL 141DW IS CRACKED ALONG BOTTOM EDGE<SDR SWAA2023041426469Panel · crackedAFT CARGO LH CENTER PANEL 1412EW IS CRACKED AND DELAMINATED ALONG BOTTOM EDGE.<SDR SWAA2023012493167Bracket · brokenAFT CARGO DOOR ASSIST HANDLE BRACKET BROKEN<[01] REMOVED AND REPLACED ASSIST HANDLE CABLE BRACKET AT FLOOR STRUCTURE ;REF B737 AMM 52-31-00 .SDR SWAA2022121280484Slide · low pressureSF DOOR SLIDE LOW PRESSURE / [01] R&R FS SLIDE ASSY PER AMM 25-66-01;[02] R&R FS SLIDE ASSY PER AMM 25-66-01SDR SWAA2022100552082Lens · missingEXIT SIGN LENS COVER MISSING ON CAPTAINS SIDE OVER WING HATCH / [01] INSTALLED LENS PER M/M 33-51-01SDR SWAA2022082645280None · failedEMERGENCY LIGHT BATTERIES FAILED CAPACITY AT LOCATIONS M1672; M1670; M1675 EMERGENCY LIGHT BATTERIES FAILED CAPACITY AT LOCATIONS M1672 M1670 M1675 / [01] REPLACED M1672; M1670; AND M1675 ELBP?S REF 33-51-06;[02] AMM 33-51-06SDR SWAA2022052409880Pin · shearedFWD ENTRY DOOR WILL NOT OPEN / [01] FOUND BROKEN SCREW ON THE UPPER GUIDE ARM PIN. R/R PIN AND SCREW PER AMM 52-11-21. AND OPS CHECK OF FWD ENTRY DOOR IS O.KSDR SWAA2022021672223Battery Pack · inoperativeALL FWD CABIN EMERGENCY LIGHTS POWERED BY BATTERY PACK M2816 ARE INOP / [01] REPLACED CHARGER ASSY PACK PER AMM 33-51-06-960-806;[02] FOR FWD CEILING BATTERY M2816;[03] REPLACED BATTERY PACK IN FWD CEILING M2816 PER AMM 33-51-06-960-805;[04] OPS TEST PASSEDSDR SWAA2022021672221Battery Pack · inoperativeALL AFT CABIN EMERGENCY LIGHTS POWERED BY BATTERY PACK M1672 ARE INOP / [01] REPLACED BATTERY PACK IN AFT RIGHT CEILING M1672 PER AMM 33-51-06-960-805;[02] OPS TEST PASSED;[03] VERIFIED ITEMS 1 AND 2. AUDIT COMPLETESDR SWAA2022021670370None · crackedDOT A-24-10. PANEL 551FB AFT SUPPORT CLIP CRACKED OFF ABOUT 2 FEET O/B OF I/B END. / [01] REMOVED AND REPLACED PNL 551 FB AFT SUPPORT CLIP CRACKED WITH A NEW SUPPORT CLIP P/N 287A9152-23; A TAG# WN7755. IAW SRM 51-40-02-OG-0; IPC # 57-50-00-38.;[02] VERIFIED ISDR SWAA2022021464378Angle · corrodedAFT CARGO FWD SHIELD ATTACH ANGLE (146A8125-53) CORRODED AROUND NUTPLATE HOLES RBL 24 WL 156 ; / [01] REMOVED CORROSION ON ATTACH ANGLE IAW SRM 51-10-02-0G-0 ITEM 15; [02] EVALUATED ALLOWABLE LIMITS : .050 ORIGINAL 'T'.030 REMAINING .020 LOSS FOUND OUT OF LIMISDR SWAA2022021464377Support · crackedCABIN FLOOR PANEL SUPPORT ANGLE AT STATION 540 RBL 1' CRACKED AT FASTENER HOLE. ; / [01] REMOVED CABIN FLOOR BOARD 231UF FOR ACCESS IAW SRM 51-40-02-G0-G; [02] REMOVED CRACKED FLOOR SUPPORT ANGLE IAW SRM 41-40-02-0G-0; [03] VERIFIED NEW FLOOR SUPPORT ANGLE PN:SDR SWAA2022021463529Angle · crackedRIGHT HAND PACK BAY HORIZONTAL ANGLE COMMON TO LOWER SIDE OF CENTER FUEL TANK AT STATION 663 RBL 10 IS CRACKED AT FASTENER OUTBOARD OF KEEL BEAM VERTICAL ANGLE. ; / [01] RH PACK BAY HORIZONTAL ANGLE COMMON TO LOWER SIDE OF CENTER TANK AT STA 663 WAS REPLACED OSDR SWAA2022021664518Shield · crackedA-061 DOT 054. #1 ENGINE INBD FAN COWL ATTACH ANGLE FOR DOOR 414AR CRACKED / [01] REMOVED CRACKED FAN COWL ATTACH ANGLE IAW SRM 51-40-02-0G-0;[02] VERIFIED NEW PART; SHIELD ATTACH ANGLE P/N 314-2259-4 IAW CMM 71-13-30<BR>ATAG A111638;[03] VERIFIED STEPS 1 AND SDR SWAA2022021462279Angle · corrodedDOT#14-186 FWD CARGO COMPARTMENT Z ANGLE CORRODED STA 500E+7 TO 500I RBL 24 WL 156 ; / [01] REMOVED CORROSION IAW SRM 51-10-02-0G-0 ITEM 15; [02] EVALUATED ALLOWABLE LIMITS : .040 ORIGINAL .010 REMAINING .030 LOSS FOUND OUT OF LIMITS IAW SRM 53-00 53-1A-2 TOOL
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