N8543Z
Service difficulty reports · 64
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 = 'N8543Z' 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 = 'N8543Z' 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 SWAA2026090700173Cover · detachedEMERGENCY EXIT SIGN FELL OFF. SECURED THE CEILING EMERGENCY EXIT LIGHT COVER IAW SIP.SDR SWAA2026082712675Wire · damagedDURNING APPROACH WHEN SELECTING FLAPS 15 LE FLAPS IN TRANSIT ILLUMINATED DURNING APPROACH WHEN SELECTING FLAPS 15 LE FLAPS IN TRANSIT ILLUMINATED REPAIRED WIRE W6588-2202B-20 APPROX 6 FROM D39939 PER SWPM 20-10-13 AND WDM 27-81-21. OPS CHECK GOOD PER AMM 27-81SDR SWAA2026072045980Slide · unpackedAFT ENTRY DOOR, DOOR SLIDE REQUIRES CURTAIN RE-PACK DUE TO HITTING DOOR THRESHOLD. RE-PACKED AFT ENTRY DOOR SLIDE IAW AMM 25-66-01.SDR SWAA2026072034129Slide · unraveledAFT SERVICE DOOR, SLIDE REQUIRES CURTAIN REPACK DUE TO HITTING DOOR THRESHOLD. REPACKED AFT SERVICE DOOR SLIDE IAW AMM 25-66-01.SDR SWAA2026062305973Seal · crackedRIGHT HORIZONTAL STAB FWD UPPER SLIDER SEAL WAS CRACKED. REMOVED AND REPLACED SLIDER SEAL IAW SRM 51-40-02.SDR SWAA2026062305975Seal · crackedLEFT HORIZONTAL STAB FWD UPPER SLIDER SEAL IS CRACKED. REMOVED AND REPLACED SLIDER SEAL IAW SRM 51-40-02.SDR SWAA2026062305969Panel · crackedSTABILIZER REMOVABLE LE PANEL 341A INTERNAL FIBERGLASS WEB HAS A CRACK AT A FWD RIVET. REMOVED NUT PLATES; FOR FURTHER INSPECTION IAW SRM 51-40-02. REMOVED PAINT IN SUPPOSED DAMAGED AREA. NO DEFECTS NOTED TO PLY'S ON FWD AND AFT SIDE. CRACK ARE LINES IN THESDR SWAA2026062304897Vapor Barrier · crackedLEFT A/C BAY, BS 663 LBL 35, VAPOR BARRIER ANGLE WAS CRACKED. CUT AND REMOVED DAMAGED SECTION OF BS 663 VAPOR BARRIER ATTACH ANGLE FROM APPROX LBL35 TO LBL65 IAW SRM 57-10-10-2R-5. LOCATED HOLES ON VAPOR BARRIER REPLACEMENT ANGLE IAW SRM 57-10-10-2R-5. LOSDR SWAA2026012664010Floor Panel · crackedAFT CARGO BAY FLOOR PANEL 141FW HAD TWO CRACKS WITHIN TWO INCHES OF LOWER EDGE. REPAIRED IAW EA M-21-125-00669.SDR SWAA2025121853605Door · out of adjustFORWARD SERVICE DOOR CATCHING ON GALLEY CABINET WHEN OPENING AND CLOSING. REPAIRED IAW AMM 52-41-00-820-801-NG.SDR SWAA2025072494940Sensor · faultyLE FLAPS TRANSIT LIGHT CAME ON AT 170KTS AND FLAPS 5; THEN BECAME INTERMITTENT WITH GEAR DOWN AND FLAPS 15<[01] T/S FAULT COULD 27-81222 IN REF TO FIM 27-88 TASK 805. LEADING EDGE FLAP F4 OUTBOARD SENSOR FAULTY. REMOVED AND REPLACED IN REF TO AMM 27-88-11. OPSSDR SWAA2024071211875Megaphone · inoperativeAFT MEGAPHONE SIREN INOP.<[01] 01 - REMOVED AND REPLACED AFT GALLEY MEGAPHONE PER [AMM 25-64-00-201-NG (DETACHABLE EMERGENCY EQUIPMENT - MAINTENANCE PRACTICES - PERMANENT)]SDR SWAA2024061300549Angle · crackedATTACH ANGLE CRACKED ; STA 420 ; AFT SIDE OF FRAME 2 ABOVE STR 26LT. ATTACH ANGLE CRACKED STA 420 AFT SIDE OF FRAME 2 ABOVE STR 26LT.<[01] REMOVED AND REPLACED ASSY CLIP <BR>REF SRM 51-40-02SDR SWAA2024061300151Bulb · inoperativeLEFT SLIDE/OVER WING EMERGENCY LIGHT IS OUT<[01] REMOVED AND REPLACED LEFT SLIDE /OVER WING EMERGENCY LIGHT BULB IAW AMM 33-51-04-960-801-NG OPS CHECKS GOODSDR SWAA2024041876488Girt Bar · out of adjustFWD SERVICE DOOR SLIDE PACK AFT GIRT BAR STOW CLIP FWD RIVIT IS SHEARED. THE CLIP IS LOOSE. FWD SERVICE DOOR SLIDE PACK AFT GIRT BAR STOW CLIP FWD RIVIT IS SHEARED. THE CLIP IS LOOSE.<[01] 01 - REMOVED AND REPLACED PER [AMM 25-66-01-801-NG (DOOR-MOUNTED ESCAPESDR SWAA2024041876487Girt Bar · out of adjustFWD ENTRY DOOR SLIDE PACK COVER FWD GIRT BAR STOW CLIP AFT RIVIT HOLE HAS A SCREW AND NUT INSTALLED AND REQUIRES A RIVIT.<[01] 01 - REPAIRED PER [AMM 25-66-01-801-NG (DOOR-MOUNTED ESCAPE SYSTEM - REPAIR - PERMANENT)];[02] SECONDARY REFERENCE SRM 51-40-12 FOR HSDR SWAA2024022655277Battery · inoperativeAFT FA FLASHLIGHT INOP<[01] REMOVED AND REPLACED BATTERY ON AFT FLASHLIGHT IAW AMM 25-64-00SDR SWAA2023121330946Girt Bar · out of adjustFWD SERVICE DOOR GIRT BAR FWD CLIP WILL NOT SECURE GIRT BAR IN STOWED POSITION<[01] ADJUSTED GIRT BAR RETENTION CLIP AND OPS CKS NORMAL REF AMM 25-66-01.SDR SWAA2023072080762Battery · inoperativeFLASHLIGHT AFT CA SIDE DOES NOT TEST<[01] REPLACED FLASHLIGHT BATTERY REFERENCE B737AMM CH 25-64-00. OPS CK GOOD.SDR SWAA2023071979562Bulb · inoperativeTHE FLOOR PROXIMITY EXIT SIGNS BY THE L/H AND R/H AFT OEW DOORS EACH HAVE AN UNLIT BULB.<[01] RELAMPED AND PERFORMED GOOD TEST OF FLOOR PROXIMITY EXIT SIGNS BY THE L/H AND R/H AFT OEW DOORS EACH HAVE 1EA UNLIT BULBS; PER AMM 33-51-01-960-801.;[02] VERIFIED CORSDR SWAA2023071978542Handle · looseCABIN DOOR ASSIST HANDLES LOOSE AT THE FWD ENTRY DOORWAY FWD SIDE; L2 DOOR LINER AND THE R2 DOOR LINER<[01] TIGHTENED CABIN DOOR ASSIST HANDLES AT FWD ENTRY DOORWAY SIDE; L2 LINER AND R2 LINER PER AMM 52-41-31-400-802 STEP 3.F.(2); SOPM 20-50-01;;[02] VERIFIEDSDR SWAA2023071877813Light · inoperativeEMERGENCY EXIT LIGHT ON THE R/H FWD OVERWING EXIT SIGN INOP<[01] IT FOUND D14840 DISCONNECTED. RECONNECTED D14840 AND PERFORMED GOOD OPERATIONAL TEST OF EMERGENCY EXIT LIGHT ON THE R/H FWD OVERWING PER WDM 33-51-13; WDM 33-21-12 AND AMM 33-51-00-710-801.;[02] SDR SWAA2023071177032Flashlight · intermittentL/H AFT ATTENDANT SEAT; INBOARD EMERGENCY FLASHLIGHT INTERMITTENT. INSTALLED NEW L/H AFT ATTENDANT SEAT INBOARD EMERGENCY FLASHLIGHT IAW AMM 25-64-00-200-802.SDR SWAA2023071875485Seal · crackedRT HORIZ STAB FRONT SPAR UPPER SLIDE SEAL CRACKED.<[01] DISCONNECTED RT HORIZ STAB F/S UPPER SLIDE SEAL LINKS FROM SLIDE SEAL PER SOPM 20-50-01.;[02] REMOVED AND REPLACED RT HORIZ STAB FRONT SPAR UPPER SLIDE SEAL IAW MM 53-31-31-000-802 AND MM 53-31-31-400-802SDR SWAA2023071874658Scuff Plate · crackedAFT CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED<[01] WELDED CRACK ON AFT CARGO BAY AFT CORNER SCUFF PLATE USING ER4043 ALUMINUM FILLER ROD LOT NUMBER 1131216 PER SRM 53-60-15-2R-1 PARAGRAPH 4. B. (2) AND (4). REPAIR AREA STILL REQUIRES A DYE PENETRANT INSPECTISDR SWAA2023071971219Floor Support · corrodedCORROSION ON FLOOR SUPPORT BS 949 RBL 51 WL 208<[01] VERIFIED APPLICABILITY PER SRM 53-70-51-1A-1 ALLOWABLE DAMAGE 1;[02] EVALUATED CORROSION ON FLOOR SUPPORT STA 949; RBL 51; WL 208 1'X0.600' INCH LOWEST MATERIAL REMOVED IS 0.040' ADJACENT TO ORIGINAL MATERIASDR SWAA2023071870756Frame · crackedBS 328 FRAME CRACKED AT LOWER END JUST ABOVE FWD ENTRY DOOR UPPER SILL WEB LBL 40 WL 284.<[01] NO ALLOWABLE DAMAGE PERMITTED PER SRM 53-00-07-1A-1 ALLOWABLE DAMAGE 1 PAR 4.A <BR>DISCREPANCY TO BE CONFIRMED BY HFEC;REMOVE I.A.W SRM 51-10-02-0G-0 AND CONTACT ENGSDR SWAA2023071170754Intercostal · crackedCRACKED INTERCOSTAL UPPER FLANGE BS 380-400 LBL 14 WL 208.<[01] NO ENTRIES FOUND ON SRM FOR PASSENGER CABIN FLOOR SUPPORT BS 380-400; LBL 14; WL 208 PART TO BE REMOVED AND REPLACED PER SRM 51-10-02-0G-0 PAR 9.C;[02] REMOVED PASSENGER CABIN FLOOR SUPPORT BS 380SDR SWAA2023071970379Floorbeam · corrodedCORROSION ON FLOOR BEAM UPPER FLANGE BS 947 LBL 25 AND LBL 50 WL 208.<[01] VERIFIED APPLICABILITY OF SRM 53-70-51-1A-1 ALLOWABLE DAMAGE [12] CORRECTION ACTION: FABRICATED REPAIR PARTS ITEM(1) T-CHORD 2EA FROM BAC1505-101045 7075T6 LOT #1522472-1; ITEM(2) ANGLESDR SWAA2023071970381Floorbeam · corrodedCORROSION ON FLOOR BEAM BS 947 RBL 50 WL 208.<[01] VERIFIED APPLICABILITY OF SRM 53-70-51-1A-1 ALLOWABLE DAMAGE 1;[02] EVALUATED CORROSION ON BS 947 FLOORBEAM UPPER FLANGE AT RBL 50 WL 208 IN AN AREA OF .8' X .6' LOWEST REMAINING MATERIAL THICKNESS .125; CORROSDR SWAA2023071961109Support · corrodedCORROSION FWD CARGO BAY AFT LOWER BULKHEAD SUPPORT HAS MULTIPLE AREAS AROUND FASTENER HOLES BS500I LBL21 TO RBL21<[01] EVALUATED CORROSION AT ALL LOCATION OF BULKHEAD SUPPORT; FOUND DEEPEST LOCATION TO BE AT BS 500I LBL 21 WL 156; FOUND 0.020 REMOVED FROM ORIGSDR SWAA2023071961110Support · corrodedCORROSION FWD CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS500A TO BS500I RBL22 WL156<[01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 500D+10' REMOVED 0.015' IN AN AREA OF 1'X1' ORIGINAL THSDR SWAA2023071961115Web · corrodedCORROSION FWD CARGO BAY SUB THRESHOLD WEB MULTIPLE AREAS AROUND NUT PLATE HOLES BS440+5' TO BS490' RBL 26 WL156<[01] EVALUATED CORROSION AT ALL LOCATION OF SUB THRESHOLD WEB; FOUND DEEPEST LOCATION TO BE AT BS 440+13 RBL 26 WL 156; FOUND 0.020 REMOVED FROM ORISDR SWAA2023071961112Shield · corrodedCORROSION FWD CARGO BAY AFT SHIELD BS500+1 TO BS500+19 RBL22 WL156 HAS MULTIPLE AREAS AROUND NUT PLATE HOLES<[01] EVALUATED CORROSION ON SHIELD BS 500+1 TO 500+19 RBL 22 WL 156; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PERSDR SWAA2023071961113Web · corrodedCORROSION AFT CARGO BAY SUB THRESHOLD WEB MULTIPLE AREAS AROUND NUT PLATE HOLES BS794 TO BS847 RBL 26 WL156<[01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 800 REMOVED 0.015' IN A AREA OF 1'X1' ORIGINAL THICKNESS 0.045' FOUND TO BSDR SWAA2023071961117Shield · corrodedCORROSION AFT CARGO BAY SHIELD AFT OF CARGO DOOR HAS MULTIPLE AREAS AROUND NUT PLATE HOLES BS847 TO BS867 RBL22 WL163.5<[01] CORROSION ON SHIELD WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM. PART REPLACEMENT REQUIRED PER SRM 51-10-02.;[0SDR SWAA2023071961118Shield · corrodedCORROSION AFT CARGO BAY SHIELD FWD OF CARGO DOOR AROUND MULTIPLE NUT PLATE HOLES BS767+3 TO BS794 RBL22 WL156<[01] CORROSION ON SHIELD WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM. PART REPLACEMENT REQUIRED PER SRM 51-10-02.;[02] VERIFIESDR SWAA2023071961119Attach Angle · corrodedCORROSION AFT CARGO BAY ATTACH ANGLE UNDER SHIELD HAS MULTIPLE AREAS UNDER NUT PLATES BS767 TO BS787 RBL21 WL156<[01] CORROSION ON ANGLE WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM. PART REPLACEMENT REQUIRED PER SRM 51-10-02.;[02] VERIFSDR SWAA2023071961121Support · corrodedCORROSION AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS727I+18' TO BS827 LBL22 WL156<[01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 767+9' REMOVED 0.020' IN A AREA OF 1'X1' ORIGINAL THSDR SWAA2023071961122Plate · corrodedCORROSION AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE HAS MULTIPLE AREAS AROUND NUT PLATE HOLES BS727H+16' TO BS767 RBL22 WL156<[01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 727J+5' REMOVED 0.015' IN A AREA OF 1'X1' ORIGINSDR SWAA2023071961114Strap · corrodedCORROSION AFT CARGO BAY FLOOR SPLICE STRAP AROUND NUT PLATE HOLE BS767+6 RBL11 WL156<[01] EVALUATED CORROSION ON FLOOR SPLICE STRAP BS 767+6 RBL 11 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 SWAA2023071961123Strap · corrodedCORROSION AFT CARGO BAY FLOOR SPLICE STRAP AROUND NUT PLATE HOLE BS727I+6 RBL11.5 WL156<[01] EVALUATED CORROSION ON FLOOR SPLICE STRAP BS 727I+6 RBL 11.5 WL 156; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0GSDR SWAA2023071966147Plate · corrodedCORROSION AFT CARGO BAY SPLICE PLATE BS767 RBL24 WL157<[01] CORROSION ON PLATE WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM. PART REPLACEMENT REQUIRED PER SRM 51-10-02.;[02] VERIFIED CORRECTIVE ACTION 1.;[03] REMOVED DAMAGED AFT CARGO BASDR SWAA2023071960699Angle · crackedRT WING TE TRANSVERSE WEB; OB ATTACH ANGLE CRACKED; AT THE DEFLECTION CONTROL RIB.<[01] VERIFIED APPLICABILITY FOR ALLOWABLE DAMAGE LIMITS RT WING TE TRANSVERSE WEB;ATTACH ANGLE IAW SRM 51-10-02;[02] NO ALLOWABLE DAMAGE LIMITS RT WING TE TRANSVERSE WEB ;OB ATTSDR SWAA2023071860877Panel · crackedCRACKED BREAK PANEL STA 540; LBL 1; WL 208.<[01] REMOVED CRACK DAMAGED BREAK PANEL AT BS 540 LBL 1 TO LBL 24 WL 208 IAW SRM 51-40-02-0G-0 LOCATED AND DRILLED NEW BREAK PANEL IAW SRM 51-40-05-0G-0 AND INSTALLED IAW SRM 51-40-02-0G-0 AND BOEING DWG 143A5240;[02]SDR SWAA2023071860878Panel · crackedCRACKED BREAK PANEL STA 540; RBL 1; WL 208.<[01] REMOVED AND REPLACED BREAK PANEL AT BS 540; BL0-RBL25; WL 208 IAW SRM 51-40-02-0G-0 AND IPC 53-42-11-66;[02] VERIFIED CORRECTIVE ACTION #1 AND MEASUREMENT TABLE;[03] TASK COMPLETESDR SWAA2023071160092Handle · brokenFED ASSIST HANDLE IS BROKEN.<[01] REPLACED BROKEN FED ASSIST HANDLE PER AMM 52-11-31-400-802;[02] VERIFIED COMPLETION OF CORRECTIVE ACTIONS 1.SDR SWAA2023071959467Attach Angle · crackedR/H BS663 UPPER ATTACH ANGLE IS CRACKED ON VAPOR BARRIER RBL8 WL167.68<[01] INSTALLED EWIS PROTECTION ON REPAIR AREA BS 663 RBL 6 TO 35 WL 155 TO 167 IAW AMM 20-60-07.;[02] R/H BS663 UPPER ATTACH ANGLE CRACKED ON VAPOR BARRIER RBL8 WL167.68 WAS FOUND CRACKED OSDR SWAA2023071959468Attach Angle · crackedL/H BS663 UPPER ATTACH ANGLE IS CRACKED ON VAPOR BARRIER LBL8 WL167.68<[01] VERIFIED APPLICABILITY OF SRM 57-10-10-2R-5.;[07] REQUIRED NDI HFEC FOR OPEN HOLES AND CRACK FREE CUT OUT ON REPAIR AREA L/H BS663 UPPER ATTACH ANGLE ON VAPOR BARRIER LBL6-22 WL167.68 SDR SWAA2023060253906Flashlight · inoperativeAFT EMERGENCY FLASHLIGHT NOT TESTING<[01] OK TO CONTINUE PER MEL 25-12-01. SP-1B;[02] REPLACED AFT EMERGENCY FLASHLIGHT PER 33-55-00 AND GOOD OPS CHECK PER AMM 25-64-00
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