N8316H
Service difficulty reports · 189
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 = 'N8316H' 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 = 'N8316H' 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 SWAA2020051828438Angle · corrodedAFT CARGO PIT LH Z ANGLE STA. 747 TO 767 5 NUTPLATES HAVE MINOR CORROSION / REMOVED CORROSION ON L/H Z ANGLE IN AFT CARGO PIT AT STA 747 TO STA 767 IAW SRM 51-10-02-0G-0 VERIFIED WITH 10X. VERIFIED MATERIAL AS ORIGINAL .040' LOSS OF .006' REMAINING .034' FOUNDSDR SWAA2020051828439Angle · corrodedAFT CARGO PIT RH Z ANGLE STA. 747 TO 767 HAS 2 NUTPLATES WITH MINOR CORROSION / AFT CARGO PIT R/H 'Z' ANGLE WAS REPLACED FROM STA 727 + 11' TO 767 ON SWA SA-M112 DEFECT # Y173444 W/O # 40456-1600-0013 (ZEE ANGLE) P/N 146A7502-52SDR SWAA2020051828440Angle · corrodedAFT CARGO PIT LH Z ANGLE STA. 767 TO 787 HAS SEVERAL SPOTS OF CORROSION / REMOVED CORROSION AFT PIT LH Z ANGLE P/N 146A7502-31 IAW SRM 51-10-02-0G-0. OT .040 REM .034 LOSS .006. FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-2 FIG 103. ZEE ANGLE REPLACED ON N/R Y1734SDR SWAA2020051828415Angle · corrodedFWD CARGO AFT BLKD LOWER SUPPORT ANGLE CORRODED AT BS 500I WL 160 RBL 22' TO LBL22. / NO ALLOWABLE CORROSION LIMITS. REMOVED AFT BULKHEAD LOWER SUPPORT ANGLE AT STA 500I. VERIFIED NEW PART AS P/N 143A9485Y35; LOCATED AND DRILLED; INSTALLED NEW SUPPORT ANGLE. ISDR SWAA2020051828437Angle · corrodedAFT CARGO PIT LH Z ANGLE STA. 727J TO 747 HAS 3 NUTPLATES WITH MINOR CORROSION / REMOVED CORROSION AT AFT CARGO L/H Z ANGLE STA 727 J TO STA 747 I.A.W SRM 53-00-53-1A-2. VERIFIED MATERIAL LOSS ORIGINAL .040 REMOVED .006 REMAIN .034 ALLOWABLE 10% MAX FOUND OUT SDR SWAA2020051828436Angle · corrodedAFT CARGO PIT RH Z ANGLE STA. 727 J TO 747 HAS 5 NUTPLATES WITH MINOR CORROSION / BLEND CORROSION ON AFT CARGO R/H '2' ANGLE AND FOUND A MATERIAL LOSS OF .009' (ORIG=.040' REMAINING=.031') TO BE 'OUT OF LIMITS' AS PER B737 SRM 53-00-53-1A-2 FIG 103. REMOVED ANSDR SWAA2020051828423Floor Panel · frayedCABIN FLOOR PANEL #221EF; UPPER SIDE OF PANEL; AREAS OF FRAYED SKIN ON PANEL; AREAS MARKED IN BLUE / REPAIRED CABIN FLOOR PANEL #221EF UPPER SIDE IAW B737 SRM 53-00-50-2R-1 REPAIR 1 PARA 3 ' 'A36551 A98054SDR SWAA2020051828422Floor Panel · frayedCABIN FLOOR PANEL #222DF; UPPER SIDE OF PANEL; SEVERAL AREAS OF FRAYED UPPER SKIN SURFACE; AREAS MARKED IN BLUE / REPAIRED CABIN FLOOR PANEL #222DF UPPER SIDE ' 'SEVERAL AREA'S OF FRAYED SKIN I.A.W B737-800 SRM'S ' '53-00-50-2R-1 REV 68 & 53-00-50-2R-0' '(A365SDR SWAA2020051828417Angle · corrodedFWD CARGO RH Z ANGLE CORRODED AT BS 500A TO 500D +12' WL 160 RBL 22'. / EVALUATED CORROSION DAMAGE; FOUND TO BE OUT OF LIMITS; REMOVED ZEE ANGLE STA 500A TO 500I RBL 22; REMOVED ZEE ANGLE STA 400 TO 420 RBL 22; REMOVED FWD BULKHEAD LOWER ATTACH BRKT STA 400 LBSDR SWAA2020051828411Angle · corrodedFWD CARGO LH Z ANGLE CORRODED AT BS 440 +3' WL 160 LBL 22'. / REMOVED CORROSION ON FWD CARGO L/H Z-ANGLE AT ATS 440+3'; WL 160 LBL 22' IAW SRM 51-10-02 + FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2; DETAIL D. CORROSION IS NUT PLATE REPLACED NEW FABRICATED SDR SWAA2020051828407Floorboard · damagedFLOORBOARD 241AAF HAS FACE SHEET FIBERS PULLED / REPAIRED UPPER FACE SHEET ON FLOORBOARD 241 AAF IAW SRM 53-00-50-2R-1; PG'S 1;2; STEPS 3 (A-N). ' 'A05073; A94592SDR SWAA2020051828406Floorboard · crushedFLOORBOARD 242UF HAS FACE SHEET FIBERS PULLED ALSO FWD UNDERSIDE INBD CORNER CRUSHED / REPAIRED UPPER FACESHEET AND UNDERSIDE INBD CORNER ON FLOORBOARD PANEL (242 UF) WITH WET LAY-UP REPAIR IAW B737-800 SRM 53-00-50-2R-1 (3) A-M (REV 68)SDR SWAA2020051828405Floorboard · damagedFLOORBOARD 242E HAS FACE SHEET FIBERS PULLED / REPAIRED UPPER FACE SHEET PLY ON FLOORBOARD 242 E ' 'IAW SRM 53-00-50-2R-1; PG'S 1;2; STEP 3(A-N)' '' 'A05073; A94592SDR SWAA2020051828404Floorboard · damagedFLOORBOARD 242F HAS FACE SHEET FIBERS PULLED / REPAIRED UPPER FACESHEET SURFACE PULLED FIBERS ON FLOORBOARD PANEL (242F) WITH WET-LAY-UP REPAIR IAW B737-800 SRM 53-00-50-2R-1 (3) A-N (REV 68)SDR SWAA2020051828403Floorboard · damagedFLOORBOARD 241F HAS FACE SHEET FIBERS PULLED / REPAIRED UPPER FACESHEET SURFACE PULLED FIBERS ON FLOORBOARD PANEL (241F) WITH WET-LAY-UP REPAIR IAW B737-800 SRM 53-00-50-2R-1 (3) A-N (REV 68)SDR SWAA2020051828402Floorboard · damagedFLOORBOARD 242D HAS FACE SHEET FIBERS PULLED / REPAIRED UPPER FACE SHEET PLY IAW SRM ' '53-00-50-2R-1 PG'S 1;2; STEPS 3 (A-N)' 'A94592; ' 'A06130; A05073; A78614SDR SWAA2020051828401Floorboard · damagedFLOORBOARD 241D HAS FACE SHEET FIBERS PULLED / REPAIRED UPPER FACESHEET PLY ON FLOORBOARD 241D ' 'IAW SRM 53-00-50-2R-1; PG 1;2; STEPS 3 (A-N) ' '' '' 'A05073; A94592SDR SWAA2020051828400Floorboard · damagedFLOORBOARD 241YF HAS FACE SHEET FIBERS PULLED / REPAIR UPPER SURFACE PLY ON FLOORBOARD 241YF IAW SRM 53-00-50-2R-1; PG'S 1;2; STEPS 3(A-N)SDR SWAA2020051828399Floorboard · damagedFLOORBOARD 241XF FACE SHEET FIBRES PULLED / REPAIRED UPPER FACESHEET PULLED FIBERS ON ' 'FLOORBOARD PANEL (241 XF) WITH WET-LAY-UP REPAIR ' 'I/A/W B737-800 SRM 53.00.50.2R21 (3) A-N (REV 68)SDR SWAA2020021214303Angle · corrodedAFT CARGO PIT L/H Z ANGLE HAD SEVERAL SPOTS CORRODED BETWEEN BS. 767 TO BS. 787. / R&R Z ANGLE IAW SRM.SDR SWAA2020021214302Angle · corrodedAFT CARGO PIT L/H Z ANGLE HAD 4 NUTPLATES WITH MINOR CORROSION BETWEEN BS. 727F TO BS. 727G. / R&R Z ANGLE IAW SRM.SDR SWAA2020021214298Angle · corrodedAFT CARGO PIT L/H Z ANGLE HAD 3 NUTPLATES WITH CORROSION BETWEEN BS. 727J TO BS. 747. / R&R L/H Z ANGLE IAW SRM.SDR SWAA2020020651029Angle · corrodedAFT CARGO PIT R/H Z ANGLE CORRODED BETWEEN BS. 727J TO BS. 747. / R&R Z ANGLE PER SRM.SDR SWAA2021082728357Fairing · delaminatedWING TO BODY FAIRING PANEL 194CL IS DELAMINATED ON OUTER SURFACE (CIRCLED IN BLACK) / REPAIRED AND APPLIED DECORATIVE FINISH ON WING TO ' 'BODY FAIRING PANEL 194CL DELAMINATED ON OUTER ' 'SURFACE AS MARKED IAW B737 SRM 51-70-04-2R-11 REV ' '68; B737 SRM 51-70-SDR SWAA2021081728360Floor Panel · corrodedAFT CARGO FLOOR PANEL 140BF CORROSION AROUND FASTENER HOLES; AS MARKED. / FOUND CORROSION ON PANEL 140BF TO EXCEED ALLOWABLE LIMITS; VERIFIED NEW PANEL AS P/N 453A2610-32 IAW SRM 53-00-53-1A-1; AIPC 25-52-10-19 ITEM 25. P/N 453A2610-32 A TAG WN4945.SDR SWAA2021081728361Floor Panel · corrodedAFT CARGO FLOOR PANEL 140DF CORROSION AROUND FASTENER HOLES; AS MARKED. / EVALUATED FLOOR PANEL 140DF IAW B737 SRM 53-00-53-1A-1 AND FOUND TO BE OUT OF LIMITS (EXCEEDS 20') CORROSION. FABRICATED NEW PANEL 140 DF IAW BOEING DRAWING 453A2610 REV B AND REV K (PANSDR SWAA2021081728359Floor Panel · corrodedAFT CARGO FLOOR PANEL 140CF CORROSION AROUND FASTENER HOLES; AS MARKED. / FOUND CORROSION TO EXCEED ALLOWABLE LIMITS VERIFIED NEW PANEL 140CF AS P/N 453A2610-18 IAW SRM 53-00-53-1A-1; AIPC 25-52-10-19 ITEM 35 P/N 453AA2610-18 A TAG WN5161.SDR SWAA2021081728358Floor Panel · corrodedAFT CARGO FLOOR PANEL 140EF CORROSION AROUND FASTENER HOLES; AS MARKED. / EVALUATED CORODED FLOOR PNL 140EF AT AFT CARGO FOUND IS MORE THAN 20 INCHES IN LENGTH IS OUT OF LIMITS IAW SRM 53-00-53-1A-1 REPLACED FLOOR PNL WITH NEW PNL IAW IPC 25-52-10-19 AND BOEINSDR SWAA2020051828351Vapor Barrier · crackedCUSTOMER REQUEST - JC - R/H 663 VAPOR WEB HAS CRACK EMITTING FROM PREVIOUS REPAIR / EVALUATED ST 663 RH VAPOR BARRIER CRACK AND FOUND TO BE REPAIRABLE CLEANED AND PREPPED AREA FOR REPAIR ON BONDED REPAIR PER SRM 57-10-10-2R-2; SRM 51-70-04-2R-0 AND SRM 51-70-0SDR SWAA2021082228354Floor Panel · corrodedFWD CARGO COMP. PANEL 120DF CORROSION AROUND THE SIDES OF PANEL AT THE FASTNER HOLES / RECEIVED IDENTIFIED + REPLACED CORRODED FWD CARGO PANEL 120DF IAW AIPC 25-52-10-17 ITEM 35 + ATAG WN 1838 PN 4251048SDR SWAA2021081728355Floor Panel · corrodedFWD CARGO COMP. PANEL 120CF CORROSION AROUND FASTNER HOLES FWD RH SIDE OF PANEL / RECEIVED IDENTIFIED + REPLACED CORRODED FWD CARGO COMPARTMENT FLOOR PANEL 120CF IAW AIPC 25-52-10-17 ITEM 25 + ATAG WN1763 PN 4251047.SDR SWAA2020051828322Battery Pack · dischargedALL EMERGENCY LIGHTS POWERED BY M1672 (AFT R/H BATTERY) ARE INOP. / REPLACED EMERGENCY LIGHT POWER SUPPLY AND BATTERY ' 'PACK M1672; OPS CHECK GOOD IAW AMM ' '33-51-06-960-805 AND AMM 33-51-06-960-806' 'WN0071; ' 'CP4323SDR SWAA2020021741397Shield · corrodedFWD CARGO RH SHIELD CORRODED AT BS 496 TO 500A WL 160 RBL 22". / REMOVED CORROSION FROM FWD CARGO R/H SHIELD STA 496 TO 500A RBL 22, VERIFIED WITH 10X MAGNIFYING GLASS, VERIFIED MATERIAL LOSS ORIG .032" REMAINING .026" LOSS .006" FOUND TO BE OUT OF LIMITS, RESDR SWAA2020021741396Angle · corrodedFWD CARGO RH Z ANGLE CORRODED AT BS 500A TO 500D +12" WL 160 RBL 22". / EVALUATED CORROSION DAMAGE, FOUND TO BE OUT OF LIMITS, REMOVED ZEE ANGLE STA 500A TO 500I RBL 22, REMOVED ZEE ANGLE STA 400 TO 420 RBL 22, REMOVED FWD BULKHEAD LOWER ATTACH BRKT STA 400 LSDR SWAA2020021741395Angle · corrodedFWD CARGO LH Z ANGLE CORRODED AT BS 440 +3" WL 160 LBL 22". / REMOVED CORROSION ON FWD CARGO L/H Z-ANGLE AT ATS 440+3", WL 160 LBL 22" IAW SRM 51-10-02 + FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2, DETAIL D. CORROSION IS NUT PLATE REPLACED NEW FABRICATEDSDR SWAA2020021741394Angle · corrodedFWD CARGO RH Z ANGLE CORRODED AT BS 400 TO 420 WL 160 RBL 22". / EVALUATED CORROSION DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 FIG 103 DET D, REPAIR ACCOMPLISHED ON Y173420 (ZEE ANGLE) PN 143A2501-184.SDR SWAA2020021241360Battery Pack · inoperativeALL EMERGENCY LIGHTS POWERED BY M1672 (AFT R/H BATTERY) WERE INOP. / R&R BATTERY PACK IAW AMM.SDR SWAA2020021241357Support Angle · corrodedFORWARD CARGO AFT BULKHEAD LOWER SUPPORT ANGLE CORRODED AT BS. 500I, BETWEEN RBL 22 TO LBL 22. / R&R ANGLE IAW SRM & DWG.SDR SWAA2020021241356Power Supply · inoperativeALL EMERGENCY LIGHTS POWERED BY M1672 (AFT R/H BATTERY) WERE INOP. / R&R POWER SUPPLY IAW AMM.SDR SWAA2020021214275Stringer Clip · crackedFORWARD CARGO STRINGER CLIP CRACKED AT FRAME ATTACH RIVET BS. 500I, STR. 25L. / R&R STRINGER CLIP IAW SRM & DWG.SDR SWAA2020021214274Stringer Clip · crackedFORWARD CARGO COMPARTMENT STRINGER CLIP CRACKED AT BS. 500I, STR. 26R. / R&R STRINGER CLIP IAW SRM & DWG.SDR SWAA2020020544154Bulkhead Web · crackedR/H BS. 663 VAPOR WEB HAD CRACK EMITTING FROM PREVIOUS REPAIR. / REPAIRED WEB PER SRM.SDR SWAA2022031735970Seal · crackedRIGHT HORIZONTAL STAB FWD UPPER SLIDING SEAL CRACKED / REMOVED AND REPLACED RIGHT HORIZONTAL STAB FWD UPPER SLIDING SEAL PER AMM 53-13-13AMT 65147SDR SWAA2022032235969Panel · crackedFLOOR BOARD SUPPORT BRAKE PANEL CRACKED RIGHT OF CENTER AT STA 540 / R+R CRACKED FLOORBOARD SUPPORT BRAKE PANEL ASSY AS PER SRM 51-40-02 AND AMM 53-21-00; LOCATED RIGHT OF CENTER AT STA 540AMT 59828SDR SWAA2022032235968Panel · crackedFLOOR BOARD SUPPORT BRAKE PANEL CRACKED LEFT OF CENTER AT STA 540 / R+R CRACKED FLOORBOARD SUPPORT BRAKE PANEL ASSY LEFT OF CENTER AT STA 540 AS PER SRM 51-40-02 AND AMM 53-21-00AMT 59828SDR SWAA2019072235156Slide · unsecureR1 DOOR EMERGENCY SLIDE FELL FROM HOUSING. REPACKED SLIDE IAW MT.SDR SWAA2018092025409Battery Pack · dischargedL2 DOOR EMERGENCY EXIT SIGN LIGHT INOP. R&R BATTERY PACK IAW AMM.SDR SWAA2018092025392Battery Pack · dischargedL2 DOOR EXTERIOR EMERGENCY EXIT SIGN LIGHT INOP. R&R BATTERY PACK IAW AMM.SDR SWAA2018071623525Lens · looseAFT OVER WING EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.SDR SWAA2018013119470Relief Valve · malfunctionedAIR TURNBACK, ON TAKEOFF OTHER AIRCRAFT REPORTED SEEING FUEL VENTING HEAVY OUT OF LT WING. RESET PRESSURE RELIEF VALVE PER AMM.
Back to N8316H