N8628A
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 = 'N8628A' 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 = 'N8628A' 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 SWAA2022041988226Bracket · brokenWIRE SUPPORT BRACKET IS BROKEN STA 867; AT STR 3 R/H. / [01] PRIOR TO REMOVAL;FOUND PART TO HAVE NO SRM LIMITS AND SO PART IS REPAIRABLE BY REPLACEMENT;PER SRM 51-10-02;STEP 9.;[02] REMOVED WIRE SUPPORT BRACKET BROKEN STA 867;AT STR. 3 RH;IAW SRM 51-40-02.;[03SDR SWAA2022042086602Support Plate · corrodedAFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE HAS AREAS OF CORROSION BS727G+13 TO BS807 LBL21 WL 156 / [01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 747+10 LBL 21 WL 156; FOUND 0.015 REMOVED FROM ORIG 0.040 IN NUMEROUS 1'X1'SDR SWAA2022042086604Support Plate · corrodedAFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE HAS AREAS OF CORROSION BS 727E+12 TO BS767 RBL 21 WL156 / [01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 727F+10 RBL 21 WL 156; FOUND 0.015 REMOVED FROM ORIG 0.040 IN NUMEROUS 1'XSDR SWAA2022042086601Web · corrodedAFT CARGO BAY SUBTHRESHOLD WEB HAS CORROSION BS 8007+18 RBL25 WL 156 / [01] EVALUATED CORROSION ON SUBTHRESHOLD WEB BS 807+18 RBL 25 WL 156; FOUND 0.015 REMOVED FROM ORIG 0.045 IN 1'X1' AREAS FOUND TO BE OUT OF LIMITS PER SRM 53-60-15-1A-1 USING DIAL DEPTH GAUSDR SWAA2022042086600Shield · corrodedAFT CARGO BAY ATTACH ANGLE UNDER SHIELD HAS CORROSION BS 767+3 RBL21 WL 156 / [01] EVALUATED CORROSION ON ATTACH ANGLE UNDER SHIELD BS 767+3 RBL 21 WL 156; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0;[02SDR SWAA2022042086603Shield · corrodedAFT CARGO BAY SHIELD HAS CORROSION BS 767+3 RBL21 WL 156 / [01] EVALUATED CORROSION ON SHIELD BS 767+3 RBL 21 WL 156; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0;[02] VERIFIED CORRECTIVE ACTION 1.;[03] RSDR SWAA2022012462725Light · inoperativeAFT GALLEY CEILING AND AFT ENTRY DOOR EMERGENCY LIGHTS INOP ; / [01] R&R BATTERY PACK AT LOCATION M1673 PER MM 33-51-06SDR SWAA2021101830164Panel · crackedFWD CARGO PANEL 120ZAC HAS A 4' LONG CRACK 20' FROM LEFT EDGEPERFORMED INTERIM REPAIR ON PANEL 120ZAC PER EA 1-A25-3722 REV5. EVERY 8 DAYS PERFORM A DETAILED VISUAL INSPECTION OF THE REPAIRED AREA FOR ADDITIONAL DAMAGE AND REPAIR INTEGRITY. IF FURTHER DEFECTS SDR SWAA2021100425118Panel · crackedFWD CARGO PANEL 120ZAC HAS A 4' LONG CRACK 20' FROM LEFT EDGEPERFORMED INTERIM REPAIR ON PANEL 120ZAC PER EA 1-A25-3722 REV5. EVERY 8 DAYS PERFORM A DETAILED VISUAL INSPECTION OF THE REPAIRED AREA FOR ADDITIONAL DAMAGE AND REPAIR INTEGRITY. IF FURTHER DEFECTS SDR SWAA2021081807570Floor Panel · crackedFWD CARGO PANEL 120ZAC HAS A 4' LONG CRACK 20' FROM LEFT EDGEPERFORMED INTERIM REPAIR ON PANEL 120ZAC PER EA 1-A25-3722 REV5. EVERY 8 DAYS PERFORM A DETAILED VISUAL INSPECTION OF THE REPAIRED AREA FOR ADDITIONAL DAMAGE AND REPAIR INTEGRITY. IF FURTHER DEFECTS SDR SWAA2021072697894Indicator · faultedFLAPS WONT EXTEND PAST 15 / CW PSEU BYTE IAW FIM 27-51 TASK 801. NO EXISTING FAULTS OR FAULT HISTORY CW TRAILING EDGE PRIMARY COUNTER OPERATION LOCK OUT IAW FIM 27-51 TASK 836 FLAPS OPERATE NORMAL AIRCRAFT OKAY FOR SERVICE. REMOVED AND INSTALLED SERVICEABLE FLSDR SWAA2021052475224Sign · detachedRAMP REPORTS OVERWING EXIT SIGN FELL OFF. SECURED OVERWING EXIT SIGN IAW AMM 33-51-01. A/C OK FOR SERVICE.SDR SWAA2021051170721Handle · displacedFWD SVC DOOR SLIDE MANUAL INFLATION HANDLE SHOWING. REPOSITION R1 SLIDE PER MT # 7256106.SDR SWAA2021030152052Lens · missingREAR LENS COVER ON AISLE EXIT SIGN OFF / INSTALLED R5EAR LENS COVER ON EMERGENCY EXIT AISLE SIGN IAW AMM 33-51-01SDR SWAA2020092217264Battery · inoperativeFWD SERVICE DOOR EMERGENCY LIGHT IN-OP. R & R FWD SERVICE DOOR EMERGENCY LIGHT BATTERY, IAW AMM 33-51-06. OPS-CHECK GOOD.SDR SWAA2021062435304Scuff Plate · crackedFWD CARGO COMPATMENT FWD CORNER SCUFF PLATE CRACKED / VERIFIED NEW SCUFF PLATE IAW B737 AIPC 53-13-00-08. LOCATED AND DRILLED IAW B737 SRM 51-40-05-0G-0. SCUFF PLATE INSTALLED ON N/R # Y200340SDR SWAA2021051386101Skate Angle · chafedR/H VERTICAL TAIL SKATE ANGLE CHAFFING ON I/B SIDE BETWEEN STA 1016 TO STA 1016 +2' / REMOVED DAMAGE ON RH SKATE ANGEL I/B SIDE STA 1016 TO 1016+2' IAW SRM 51-10-02-0G-0. MESSURED MATERIAL LOSS TO BE .007' ORIGINAL (T) .075' REMAINING (T) .068 IN LIMITS IAW SRSDR SWAA2021051386100Skate Angle · chafedL/H VERTICAL TAIL SKATE ANGLE CHAFFING ON I/B SIDE BETWEEN STA 1016 TO STA 1016 +2' / REMOVED DAMAGE ON L/H SKATE ANGLE I/B SIDE STA 1016 TO 1016+2' IAW SRM 51-10-02-0G-0 MESSURED MATERIAL LOSS TO BE .004' ORIGINAL (T) .075' REMAINING (T) .071 FOUND TO BE IN LSDR SWAA2020041335175Baffle · crackedFWD CARGO COMPARTMENT RH SIDE BAFFLE; UNDER Z-ANGLE BS 500G - 500H IS CRACKED / REMOVED AND REPLACED FWD CARGO RH SIDE BAFFLE STA 500G- 500H PART # 143A7510-22 PER SRM 51-40-02-0G-0 AND DWG 143A7505 REV BSDR SWAA2020041335174Baffle · crackedFWD CARGO COMPARTMENT RH SIDE BAFFLE; UNDER Z-ANGLE BS 500F - 500G IS CRACKED / REMOVED AND REPLACED FWD CARGO RH SIDE BAFFLE STA 500F- 500G PART # 143A7510-22 PER SRM 51-40-02-0G-0 AND DWG 143A7505 REV BSDR SWAA2020041334930Attach Fitting · crackedFWD CARGO COMPARTMENT BAFFLE ATTACH CLIP IS CRACKED AT RBL 25 ON THE FWD SIDE OF BS 500H / REMOVED AND REPLACED FWD CARGO BAFFLE ATTACH CLIP AT STA 500H RBL 25 PART # 143A75024158 PN SRM 51-40-02-0G-0 AND DWG 143A7505 REV BSDR SWAA2021080534919Floor Panel · corrodedFWD PIT FLOOR PANEL 120DF IS CORRODED / DUE TO TOTAL CORROSION DAMAGE OF PANEL 120DF OVER 20' FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-00-53-1A-1 FIG 102. FABRICATED A NEW FLOOR PANEL IAW B737 AMM 25-52-01-201-801 STEP F. TREATED AND PRIMED PANEL IAW B737SDR SWAA2021080534920Floor Panel · corrodedFWD PIT FLOOR PANEL 120AF IS CORRODED / EVALUATED FWD CARGO PIT FLOOR PANEL 120AF OUT OF LIMITS IAW SRM 53-00-53-1A-1; FIG 102; FABRICATED NEW FLOOR PANEL 120AF IAW 737 AMM 25-52-01-201-801; TREATED LOWER SURFACE IAW 737 AMM 51-21-41-370-802 APPLIED PRIMER TO SDR SWAA2021080534918Floor Panel · corrodedFWD PIT FLOOR PANEL 120CF IS CORRODED / REPLACED CORRODED FWD PIT FLOOR PANEL 120CF; VERIFIED MATERIAL AS .071; 2024 T3; ATAG # A39946; AND FABRICATED REPLACEMENT PANEL IAW AMM 25-52-01SDR SWAA2021080534914Floor Panel · corrodedAFT PIT FLOOR PANEL 140DF IS CORRODED / REPLACED AFT PIT FLOOR PANEL 140DF; VERFIED MATERIAL AS .071; 2024 T-3; AND FABRICATED REPLACEMENT PANEL IAW AMM 25-52-01SDR SWAA2021080534915Floor Panel · corrodedAFT PIT FLOOR PANEL 140BF IS CORRODED / REPLACED AFT PIT FLOOR PANEL 140BF; VERFIED MATERIAL AS .071; 2024 T-3; AND FABRICATED REPLACEMENT PANEL IAW AMM 25-52-01 A39933SDR SWAA2021080534913Floor Panel · corrodedAFT PIT FLOOR PANEL 140CF IS CORRODED / REMOVED CORROSION IAW SRM 51-10-02-0G-0 FOUND TO HAVE CORROSION LONGER THAN 20'. FOUND TO BE OUT OF LIMITS. VERIFIED NEW MATERIAL FOUND TO BE .071 2024-43 IAW SRM 25-52-01-201-801. FABRICATED NEW FLOOR PANEL 140CF IAW SRSDR SWAA2021080534912Floor Panel · corrodedAFT PIT FLOOR PANEL 140EF IS CORRODED / AFT PIT FLOOR PANEL 140EF EXCEEDED 20' OF CORROSIION; FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-1. FABRICATED NEW PANEL IAW 25-52-01-201-801/ TREATED AND PRIMED IAW SRM 51-20-01-0G-0/ AMM 51-21-72-370-804 TAG A39935SDR SWAA2021080534921Strip · crackedAFT PIT #1 CAPSTRIP SPLICE IS CRACKED OUT / VERIFIED NEW CAP STRIP SPLICE PART # 453A21611-13; A-TAG # A03654 IAW B737 AIPC 25-52-10-04 ITEM # 460. CRACKED CAP STRIP FOR AFT PIT REPLACED WITH NEW CAPSTRIP ON WORK BENCH; INSTALLED ON SA-M 565S.SDR SWAA2021071634885Access Panel · corrodedRIGHT WING; FUEL TANK TANK ACCESS HOLE 632LB; LIP HAS FRETTING CORROSION. / REMOVED CORROSION FROM R/H WING FUEL TANK ACCESS HOLE 632LB LIP REMAINING THICKNESS 0.197' LIMITS IAW SRM 57-20-01-2R-1. REPAIRED IAW SRM 57-20-01-2R-1.SDR SWAA2020041334568Attach Angle · crackedAFT PIT BS867; LBL12; OTBD SIDE OF FLOORBOARD ATTACH ANGLE; CLIP CRACKED. / REMOVED AND REPLACED AFT CARGO ATTACH CLIP STA 867 LBL 12 OTBD SIDE OF FLOORBOARD ATTACH IAW SRM 51-40-02 AND BOEING DWG 149A8102 REV A. ATAG A34482 PN: 149A8109-114SDR SWAA2020041334415Angle · corrodedAFT CARGO PIT RIGHTHAND Z ANGLE HAS CORROSION FROM STA. 727D TO STA. 727G APPROX. WL 156 RBL 20 / AFT CARGO RH Z-ANGLE STA 727D TO 727 6 REPAIRED ON SOUTHWEST NRC Y200113; REMOVED CORROSION ON Z-ANGLE IAW SRM 51-10-02-0G-0. MEASURED MATERIAL LOSS TO BE .007' OSDR SWAA2020041334411Angle · corrodedBS727H-BS767 RBL24 WL155 AFT CARGO COMPARTMENT Z-ANGLE MANY AREAS OF CORROSION / REMOVED CORROSION ON AFT CARGO 2-ANGLE EH STA 727C+9 TO STA 767 IAW SRM 51-10-02-0G-0. MEASURED MATERIAL LOSS ORIGNIAL (TP .040' REMAINING (T) .031' LOSS OF .009' OUT OF LIMITS IASDR SWAA2020041334299Angle · corrodedFWD CARGO. STA 500I; RBL 23; WL 155; CURVED SIDEWALL BULKHEAD ANGLE HAS CORROSION ON UPPER SURFACE / REMOVED CORROSION NO SRM LIMITS GIVEN. REMOVED AND REPLACED FWD CARGO STA 500I RBL 23 CURVED SIDEWALL BULKHEAD ANGLE IAW B-737 SRM 51-40-02 AND DWGS 143A9481 RSDR SWAA2020041334298Angle · corrodedFWD CARGO. STA 500I; RBL 22 TO LBL 22; WL 155; FLOOR SUPPORT BULKHEAD ANGLE HAS CORROSION ON UPPER SURFACE. / REMOVED CORROSION FROM FWD CARGO STA 500I RBL 22 TO LBL22 WL155 FLOOR SUPPORT BULKHEAD ANGLE NO SRM REPAIR LIMITS GIVEN IAW B737 SRM 51-10-02-0G-0; RESDR SWAA2020041334297Gusset · crackedFWD CARGO STA 500I; STR 19R; STRINGER CLIP GUSSET IS CRACKED IN UPPER AFT RADIUS. / REMOVED CRACKED GUSSET AT FWD CARGO STA 500I STR 19RH AND INSTALLED NEW GUSSET ALL IAW SRM 51-40-02-0G-0 AND DWG # 143A7902 REV E. ATG # A41659SDR SWAA2020041334412Shield · corrodedBS767-787 RBL24 WL155 AFT CARGO COMPARTMENT Z-ANGLE MANY AREAS OF CORROSION / BLENDED CORROSION ON AFT CARGO STA 767-787 RBL24 SHIELD. VERFIED ORIG 'T'.050 REM 'T' .043 LOSS OF .007 FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED SHIELD. P/N 146A8127-12 ATAG WSDR SWAA2020041334413Tee Fitting · corrodedBS772 RBL14-18 WL155 AFT CARGO BAY FLOOR STRUCTURE 2 AREAS OF CORROSION / REMOVED CORROSION FROM TEE STRUCTURE LOCATED AT BS 772 RBL 14 - 18. WL 155 AFT CARGO BAY FLOOR STRUCTURE IAW B737 SRM 51-10-02-0G-0 STEP 6. ORIGINAL MATERIAL THICKNESS IS 0.080'; REMAINISDR SWAA2020041334282Support Rod · crackedR\H WING REAR SPAR; INBD OF #2 TANK BOOST PUMP; PANEL SUPPORT ROD CRACKED. / REPLACED PANEL #651BB SUPPORT ROD IAW SOPM 20-50-01 DD4029SDR SWAA2020041334296Angle · corrodedFWD CARGO. STA 500A TO 500B; RBL 23; WL 155; RH Z-ANGLE HAS CORROSION ON UPPER SURFACE. / EVALUATED FWD CARGFO STA 500A - 500I RBL 23 RH Z ANGLE. FOUND TO BE OUT OF LIMITS IAW B737 SRM 53-00-53-1A-2 FIG 103 DETAIL D Z ANGLE REPAIRED ON N/R #Y200103 P/N 143A750SDR SWAA2020041334300Angle · corrodedFWD CARGO; STA 500H+11 TO 500H+16; RBL 23; WL 155; Z-ANGLE HAS CORROSION ON UPPER SURFACE / EVALUATED FWD CARGO STA 500A TO 500I; RBL 23; WL 155; Z-ANGLE. FOUND TO BE OUT OF LIMITS IAW B737 SRM 53-00-53-1A-2 FIG 103 DETAIL D; Z ANGLE REPAIRED ON N/R # 200103 PSDR SWAA2020041334301Angle · corrodedFWD CARGO. STA 500+3 TO 500L; LBL 23; WL 155; Z-ANGLE HAS CORROSION ON UPPER SURFACE. / REMOVED CORROSION FROM FWD CARGO ZEE ANGLE BETWEEN STA 500+3 TO 500I; LBL 23; WL 155 IAW B737 SRM 51-10-02-0G-0. ORIGINAL MATERIAL THICKNESS = 0.040'; REMAINING 0.00'; LOSSSDR SWAA2020041334302Angle · corrodedFWD CARGO. STA 500C TO 500F+16; RBL 23; WL 155; Z-ANGLE HAS CORROSION ON UPPER SURFACE. / REMOVED CORROSION ON FWD CARGO STA 500A-500I; RBL 23; WL 155 Z ANGLE 100% MAT. LOSS FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 FIG 103 DETAIL D. REPAIRED Z ANGLE IAWSDR SWAA2020041334409Angle · corrodedBS807-727H LBL24 WL155 AFT CARGO COMPARTMENT Z-ANGLE MANY AREAS OF CORROSION / BLENDED CORROSION ON AFT CARGO L/H Z-ANGLE. VERIFIED 100% MATERIAL LOSS FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED L/H AFT CARGO Z-ANGLE STA 727G-827 IAW B737-800 SRM 53-00-53-SDR SWAA2020041336042Angle · nickedFWD CARGO. STA 500H+2; AND STA 500H+9.5; LBL 23; WL 155; Z-ANGLE HAS DEEP NICKS IN UPPER SURFACE / Z-ANGLE REPAIRED AT STA 500H+2 AND STA 500H+9.5 LBL 23 ACCOMPLISHED ON W/O Y200102SDR SWAA2021081734058Bracket · brokenLH WING LOWER WING PANEL #551FB HAS A BROKEN BRACKET. MARKED WITH A FLAG. / LH WING LOWER WING PANEL #551FB HAS A BROKEN BRACKET. REMOVED BROKEN BRACKET IAW SRM 51-40-02-0G-0 RECEIVED NEW BRACKET PN: 287A9152-23 AND INSTALLED NEW BRACKET IAW SRM 51-40-02-0G-0 SDR SWAA2021081734057Bracket · brokenRIGHT WING T/E PANEL 651FB CTR AFT BRACKET IS BROKEN / REMOVED BROKEN BRACKET ON R/H WING T/E PANEL 651FB IAW SRM 51-40-02-0G-0. VERIFIED NEW BRACKET PN:287A9152-24 A TAG (A41643) IAW IPC 57-50-00-38. INSTALLED NEW BRACKET IAW SRM 51-40-02-0G-0.SDR SWAA2021080529705Floor Panel · unsecureINTERMITTENT POPPING HEARD IN ASILE AT ROW 17 INTERMITTENT POPPING HEARD IN ASILE AT ROW 17 PER EA 1-A53-31403 INSPECT EVERY 100 FLIGHT CYCLES AND PERMANENT REPAIR REQUIRED IN 250 FLIGHT CYCLES. PERMANENT ACTION REQUIRED: PERFORM PERMANENT REPAIR BY REPLACING SDR SWAA2019120939384Lens · detachedEMERGENCY EXIT SIGN IN AISLE HAD COVER KNOCKED OFF. / SECURED LENS PER AMM.SDR SWAA2019101637940Light · crackedL/H PHOTO LUM PATH LIGHTING STRIPS CRACKED AT SLAT ROW. / R&R LIGHT PER AMM.
Back to N8628A