N8529Z

Service difficulty reports · 69

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 = 'N8529Z' 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.

SDR SWAA2023042621296Structure · corrodedCORROSION ON FWD SERVICE DOORWAY MOPSILL VERTICAL FLANGE; STA 310-331; RBL 58-59; WL 209 AND STA 327-329 ON HORIZONAL FLANGE; RBL 58 WL 208.<REMOVED CORROSION ON STEP 2;[04] ADDED BLEND TO STEP 1;[05] ADDED BLEND TO STEP 1;[06] REMOVED 26 EA FASTENERS ON FWD SMar 27, 2023 · N8529Z · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2023042521294Support · corrodedCORROSION FWD CARGO BAY AFT LOWER BULKHEAD SUPPORT HAS MULTIPLE AREAS AROUND FASTENER HEADS BS500I LBL22 TO RBL22<[01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 500I RBL 10 REMAINING THICKNESS LESS THAN 0.056' IN A AREA OF 1X1 FOMar 27, 2023 · N8529Z · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2023042521288Intercostal · crackedCRACKED INTERCOSTAL UPPER ATTACH ANGLE AT STA 380-400; LBL 13; WL 208.<[01] UPDATED TABLE AND PART BLOCK;[02] REMOVED DAMAGED INTERCOSTAL UPPER ATTACH ANGLE AT STA 380-400; LBL 13; WL 208 PER SRM 51-40-02-0G-0.;[03] LOCATED AND DRILLED AND DEBURRED AND INSTALLMar 27, 2023 · N8529Z · Boeing 7378H4 · Fuselage Main, Plate/SkinSDR SWAA2023042521215Angle · corrodedCORROSION ON 'Z' ANGLE STA 992 2 EA AREAS ; LBL 37; LBL 43; WL 208 UPPER SURFACE.<[01] UPDATED MEASUREMENTS. UPON FURTHER INVESTIGATION; THERE'S NO ALLOWABLE DAMAGE AND PART WILL BE REPLACE IAW SRM 51-10-02 STEP 9. REMOVED Z ANGLE AT STA 992.2 LBL37; LBL43; ANMar 27, 2023 · N8529Z · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2023042521225Angle · corrodedCORROSION ON 'Z' ANGLE STA 992; RBL 37; WL 208 UPPER SURFACE.<[01] UPDATED MEASUREMENTS. UPON FURTHER INVESTIGATION; THERE'S NO ALLOWABLE DAMAGE AND PART WILL BE REPLACE IAW SRM 51-10-02 STEP 9. REMOVED Z ANGLE AT STA 992; RBL37; AND WL208 IAW SRM 51-40-02.;[0Mar 27, 2023 · N8529Z · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2023042521291Shield · corrodedCORROSION AFT CARGO BAY SHIELD FWD OF CARGO DOOR AROUND MULTIPLE NUT PLATE HOLES BS767 TO BS794 RBL22 WL156<[01] CORROSION ON SHIELD WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM.;[02] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT TABLE;[0Mar 27, 2023 · N8529Z · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2023042521286Web · corrodedCORROSION AFT CARGO BAY SUB THRESHOLD WEB MULTIPLE AREAS AROUND NUT PLATE HOLES BS794 TO BS847 RBL 26.5 WL156<[01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 794.5+8' REMOVED 0.020' IN A AREA OF 1'X1' ORIGINAL THICKNESS 0.045' FOUMar 27, 2023 · N8529Z · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2023042721042Floorbeam · corrodedCORROSION ON BS 986 FLOOR BEAM; LBL 44; WL 208; AROUND NUTPLATE HOLE.<REMOVED CORROSION ON BS986 LBL44 WL 208 AROUND THE NUTPLATE HOLE ORIGINAL MATERIAL THICKNESS IS 0.150' REMAINING MATERIAL THICKNESS IS 0.120' DAMAGE TO BE FOUND OUT LIMITS I.A.W SRM 53-70-51Mar 26, 2023 · N8529Z · Boeing 7378H4 · Fuselage Main, Floor BeamSDR SWAA2023042521041Floorbeam · corrodedCORROSION FOUND ON BS 947 FLOOR BEAM; LBL 24; WL 208; AFT EDGE OF THE UPPER CHORD.<[01] CORROSION ON BS 947 FLOOR BEAM; LBL 24; WL 208; AFT EDGE OF THE UPPER CHORD ORIGINAL MATERIAL THICKNESS IS .180' LOWEST MATERIAL REMAINING IS 0.140' FOUND TO BE OUT OF LIMIMar 26, 2023 · N8529Z · Boeing 7378H4 · Fuselage Main, Floor BeamSDR SWAA2023042619412Panel · damagedPANEL 521KB DISBONDED AT FWD I/B CORNER.<OUT OF ALLOWABLE LIMITS IAW SRM 57-41-01-1A-1 PARA 4.A.(5).REMOVED DAMAGED PLIES. CLEANED AND PREPARED PANEL IAW SRM 51-70-05-2R-6 PARA 4.A-D.;[02] MEASUREMENT TABLE UPDATED. FABRICATED REPAIR PLIES USING BMS 5-129 TY2 Mar 22, 2023 · N8529Z · Boeing 7378H4 · Wing Miscellaneous StructureSDR SWAA2023042619264Attach Angle · crackedL/H BS663 UPPER ATTACH ANGLE IS CRACKED ON VAPOR BARRIER LBL8 WL167.68<REMOVED DAMAGED SECTION OF LH BS663 VAPOR BARRIER UPPER ATTACH ANGLE LBL8-LBL20 WL167.68 IAW SRM 57-10-10-2R-5. RECEIVED REPAIR PARTS FOR BS663 LH VAPOR BARRIER UPPER ATTACH ANGLE LBL8-LBL2Mar 21, 2023 · N8529Z · Boeing 7378H4 · Fuselage Main, FrameSDR SWAA2023042619266Attach Angle · crackedR/H BS663 UPPER ATTACH ANGLE IS CRACKED ON VAPOR BARRIER RBL8 WL167.68<REMOVED DAMAGED SECTION OF RH BS663 VAPOR BARRIER UPPER ATTACH ANGLE RBL8-RBL20 WL167.68 IAW SRM 57-10-10-2R-5.RECEIVED REPAIR PARTS FOR BS663 RH VAPOR BARRIER UPPER ATTACH ANGLE RBL8-RBL20Mar 21, 2023 · N8529Z · Boeing 7378H4 · Fuselage Main, FrameSDR SWAA2023042519405Cover · missingL/H EMEREGENCY EXIT HATCH ESCAPE STRAP RETAINER COVER ASSY IS MISSING.<[01] REPLACED EMERGENCY EXIT HATCH ESCAPE STRAP RETAINER COVER IAW SIP AMM SWA D633A101 STEP 2. A-C;[02] VERIFIED CORRECTIVE ACTION STEP 1.;[03] VERIFIED CORRECTIVE ACTION 1.Mar 21, 2023 · N8529Z · Boeing 7378H4 · Emergency EquipmentSDR SWAA2023042718902Light · inoperativeRIGHT EMERGENCY GROUND ILLUMINATION LIGHT IS INOP<[01] RELAMPED RIGHT EMERGENCY GROUND ILLUMINATION LIGHT PER AMM 33-51-04-960-801;[02] RELAMPED RIGHT EMERGENCY GROUND ILLUMINATION LIGHT PER AMM 33-51-04-960-801 STEP 2. F. (1);[03] TEST STILL REQUIRED;[04] PERMar 20, 2023 · N8529Z · Boeing 7378H4 · Emergency LightingSDR SWAA2023042618918Door · out of adjustFWD SERVICE DOOR REQUIRES ADJUSTMENT.<[01] BEGAN ADJUSTING FSD PER AMM 52-41-00-820-801 STEPS 2.I; L; K; N; Q AND R;[02] ADJUSTED FWD SERVICE DOOR PER AMM AMM 52-41-00-820-801 STEPS 2.I; L; K; N; Q AND R AND PERFORMED FWD SERVICE DOOR SYSTEM TEST PER AMM 52-41Mar 20, 2023 · N8529Z · Boeing 7378H4 · Service DoorsSDR SWAA2022120678524Transmitter · stuckHAD A LE FLAPS TRANSIT LIGHT ILLUMINATED ON FINAL AT 200 FEET WITH WITH FLAPS IN 30 POSITION. ON G0 AROUND THE LE FLAPS TRANSIT LIGHT EXTINGUISH WITH GO AROUND PROCEDURE AND SELECTIING FLAP HANDLE TO POSITION 15 AND GEAR GEAR UP. CALLED FOR FLAPS 5 AND HEARD GDec 4, 2022 · N8529Z · Boeing 7378H4 · Trailing Flap Position Indicating SystemSDR SWAA2022100351829Megaphone · inoperativeF/A MEGAPHONE INOP / [01] R&R AFT MEGAPHONE PER MM 25-64-00Oct 1, 2022 · N8529Z · Boeing 7378H4 · Emergency EquipmentSDR SWAA2021022249969Cover · out of positionAFT/FO SIE/DOOR PULL TO INFLATE VELCRO COVER STUCK / REPOSITIONED VELCRO/FLAP COVER WITHOUT REMOVING SLIDE PACK; NO DEFECTSNOTED. S.I.P.Feb 18, 2021 · N8529Z · Boeing 7378H4 · Emergency EquipmentSDR SWAA2019123140039Flashlight · inoperativeAFT CAPTAIN`S SIDE CABIN FLASHLIGHT WOULD NOT TEST. REPAIRED FLASHLIGHT IAW AMM.Dec 30, 2019 · N8529Z · Boeing 7378H4 · Emergency Equipment
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