N8554X
Service difficulty reports · 57
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 = 'N8554X' 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 = 'N8554X' 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 SWAA2026092179944Bolt · looseFUEL LEAK REPORTED FROM REFUELING PANEL. RETORQUED MOUNTING BOLTS ON THE CENTER TANK FUELING SHUTOFF VALVE IAW AMM 28-21-51. NO LEAKS NOTED.SDR SWAA2026062515351Light · cracked2ABC FLOOR PHOTOLUMINESCENCE STRIP IS CRACKED; DAMAGED AND HAS MOISTURE BUILD UP. REMOVED AND REPLACED FLOOR PHOTOLUMINESCENCE STRIP AT 2ABC IAW AMM 35-51-015.SDR SWAA2026062515350Light · cracked3DEF FLOOR PHOTOLUMINESCENCE STRIP IS CRACKED, DAMAGED AND HAS MOISTURE BUILD UP. REMOVED AND REPLACED FLOOR PHOTOLUMINESCENCE STRIP AT 3DEF IAW AMM 33-51-15.SDR SWAA2026042793295Hmu · leakingNUMBER 2 ENG FAILED ON TAKEOFF; REJECT AT APPROX 100 KIAS BRK ENERGY 21.1M FT-LB. INSPECTION REQUIRED ABOVE 30.0M FT-LM. DURING INITIAL EVALUTATION FAULT CODE 73-31552 IS PRESENT IN EEC IAW FIM 73-31, TASK 803. PERFORMED GVI OF NR 2 ENGINE AND DISCOVERED HSDR SWAA2026042793346Pump · failedNUMBER 2 ENGINE FAILED ON TAKEOFF, REJECT AT APPROX 100 KIAS BRK ENERGY 21.1M FT-LB; INSPECTION REQUIRED ABOVE 30.0M FT-LM. DURING INITIAL EVALUTATION FAULT CODE 73-31552 IS PRESENT IN EEC REF FIM 73-31 TASK 803. PERFORMED GVI OF NR 2 ENGINE AND DISCOVERED SDR SWAA2026042792200Cover · looseL1 DOOR SLIDE COVER 2EA CLIPS ARE LOOSE. RESECURED L1 DOOR SLIDE COVER 2EA CLIPS IAW SRM 51-40-02.SDR SWAA2026040785437Flashlight · failedLEFT OTBD AFT FLASHLIGHT HAS RED LIGHT. R & R FLASHLIGHT ASSY IAW AMM 25-64-00 IN L/H AFT OTBD POSITION.SDR SWAA2025103029303Megaphone · inoperativeAFT MEGAPHONE INOPERATIVE. REMOVED AND REPLACED IAW AMM 25-64-00-SWA-804-NG-01.SDR SWAA2025021496140Flashlight · no testAFT R/H F/A FLASHLIGHT NOT TESTING<[01] REPLACED AFT F/A FLASHLIGHT PER AMM 25-64-00.SDR SWAA20250131001Lens · missingEMERGENCY EXIT LIGHT LENS MISSING<[01] REPLACED MISSING CENTER AISLE CEILING EMERGENCY EXIT LIGHT LENS PER AMM 33-51-01. OSD: 1/31/2025SDR SWAA2024092742731Girt Bar · out of adjustPLASTIC PIECE FELL OFF DOOR R1 GIRT BAR.<[01] REPLACED R1 DOOR GIRT BAR EVAC RELEASE STOP PER AMM 25-66-00.SDR SWAA2024080722163Light · inoperativeLEFT SIDE ROW 15CB OVER WING EXIT DOOR LIGHT INOPERATIVE<[01] OK TO CONT. PER MEL 33-2-04 SP#1 AUTH.#207613;[02] R&RD WINDOW LIGHT ASSEMBLY AT ROW 15CB IAW AMM 33-21-00; LOADED SOFTWARE AS REQUIRED AND OPS CHECK GOODSDR SWAA2024072516170Flashlight · inoperative1 AFT EMERGENCY FLASHLIGHT INOP<[01] REPLACED AFT EMERGENCY FLASHLIGHT AND BATTERY. OPS NORMAL. REF AMM 25-64-00SDR SWAA2024072516811Battery · inoperative1 AFT EMERGENCY FLASHLIGHT INOP<[01] REPLACED AFT EMERGENCY FLASHLIGHT AND BATTERY. OPS NORMAL. REF AMM 25-64-00SDR SWAA2024050281409Light · inoperativeRH SIDE SERVICE DOOR EMERGENCY LIGHT INOP<[01] R/R RH SLIDE SERVICE DOOR EMERGENCY LIGHT PER AMM 33-51-04SDR SWAA2024010437127Flashlight · inoperativeAFT CABIN F/OS SIDE FLASHLIGHT DOES NOT TEST<[01] SECURED AFT F/O FLASHLIGHT TO MOUNT PER SIP. NO DEFECTS NOTED.SDR SWAA2023122735337Cover · looseOVERHEAD EMERGENCY EXIT SIGN MID CABIN CAME LOOSE<[01] RE-ATTACHED OVERHEAD EMERGENCY EXIT SIGN PLASTIC COVER REF 33-51-03SDR SWAA2023121331100Battery · inoperativeAFT CABIN FLASHLIGHT INOP<[01] R/R AFT CABIN FLASHLIGHT ASSY AND BATTERY IAW AMM 25-64-00 OPS CHECK GOODSDR SWAA2023121329560Flashlight · inoperativeAFT CABIN FLASHLIGHT INOP<[01] R/R AFT CABIN FLASHLIGHT ASSY AND BATTERY IAW AMM 25-64-00 OPS CHECK GOODSDR SWAA2023120526716Skirt · out of adjustFWD ENTRY DOOR ESCAPE SLIDE; LOWER SKIRT MAKES HARD CONTACT WITH THE SCUFF PLATE WHEN OPENING AND CLOSING DOOR.<[01] ADJUSTED ESCAPE SLIDE ON FWD ENTRY DOOR PER AMM INTRODUCTION 2. STANDARD INDUSTRY PRACTICES STEP B AND AMM 25-66-01-400-801.;[02] VERIFIED CORRSDR SWAA2023120526713Lens · damagedFWD LAV EMERGENCY EXIT LIGHT LENS DAMAGED<[01] REMOVED AND REPLACED FWD LAV EMERGENCY EXIT LIGHT LENS PER AMM 33-51-01-960-802. OPS CHECK WAS GOOD.;[02] VERIFIED.<BR>VERIFIED MEASUREMENTS.SDR SWAA2023120523637Shield · cracked#2 ENGINE O/B FAN COWL OIL ACCESS DOOR SHEILD IS CRACKED<[01] REMOVED AND REPLACED #2 ENGINE O/B FAN COWL OIL ACCESS DOOR SHEILD PER SRM 51-40-02-0G-0 AND CMM 71-13-30;[02] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.SDR SWAA2023120518665Attach Angle · crackedR/H BS663 UPPER ATTACH ANGLE IS CRACKED ON VAPOR BARRIER RBL8 WL167.68<[01] R/H BS663 UPPER ATTACH ANGLE IS ON VAPOR BARRIER RBL8 WL167.68 REPAIRED BY REMOVED DAMAGE AREA; FABRICATED; LOCATED; DRILLED AND INSTALLED REPAIR PARTS IAW SRM 57-10-10-2R-5 PAR 4 A-P.SDR SWAA2023120518045Floor Panel · pulledPANEL 221AF UPPER SURFACE HAS PULLED STRANDS OF FIBERGLASS<[01] UPPER SURFACE REPAIR ON PANEL 221AF COMPLETED IAW SRM 53-00-50-2R-1;[02] VERIFIED RII INSPECTION REQUIREMENTS ARE MET.;[03] VERIFIED UPPER SURFACE REPAIR ON PANEL 221AF COMPLETED IAW SRM 53-00-50-SDR SWAA2023120518782Floor Panel · delaminatedPANEL 221BF UPPER PLY IS DALAMINATED<[01] PANEL 221BF UPPER PLY DELAMINATION WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] FINAL INSPECTION. JOB COMPLETE.<BR><BR>VERIFIED MEASUREMENTS.SDR SWAA2023120518039Floor Support · crackedFLOOR SUPPORT CRACKED AT BS 380-400 LBL13 WL208.<[01] ALL STEPS COMPLETE REMOVED CRACKED FLOOR SUPPORT AT BS 380-400 LBL13 WL208 PER SRM 51-40-02 COMPLETED MEASUREMENT TABLE.<BR>LOCATED AND DRILLED NEW FLOOR SUPPORT AT BS 380-400 LBL13 WL208 PER SRM 51-40-04 BSDR SWAA2023120518040Floor Support · crackedFLOOR SUPPORT CRACKED AT BS 390 LBL51 WL208.<[01] REMOVED FLOOR SUPPORT ON BS 390 LBL 51 WL208 PER SRM 51-40-02 AND ENGINEER DWG: 143A5400 ID: 0183 (AND 0182).;[02] COMPLETED ALL STEPS REMOVED CRACKED FLOOR SUPPORT AT BS 390 LBL51 WL208 PER SRM 51-40-02 COMPLESDR SWAA2023120518037Channel · crackedFWD ENTRY DOOR MOPSILL CRACKED AT BS 303.9 LBL60 WL208<[01] INSTALLED FWD ENTRY DOOR MOPSILL IAW SRM 51-40-02-0G-0; BOEING DWG 140A9810 ID:71 REV:-; BOEING DWG 141A8110 ID:0022 REV:A AND BOEING DWG 141A8110 ID:0023 REV:-.;[02] CARD COMPLETESDR SWAA2023120518783Floor Panel · exposedPANEL 241AF FORWARD RIGHT CORNER HAS EXPOSED CORE<[01] DUE TO EXTENT OF DAMAGE ON UPPER SURFACE OF PANEL FABRICATED NEW 241AF FLOOR PANEL FROM BMS4-17 TYPE 6 LOT#1534398-1. INSTALLED INSERTS USING BMS5-107 LOT#AK3BA2380A/A; INSERTS CURED USING HEAT LAMP AND THSDR SWAA2023120517643Floor Support · crackedWING CENTER SECTION - CRACKED SUPPORT FLOOR AT BS 540 RBL 2 WL 208 (MARKED)<[01] REMOVED AND REPLACED FLOOR SUPPORT @ BS540 BL0-RBL25 WL208 PER SRM 51-40-02 AND DWG:143A0060 REV:ASDR SWAA2023120517645Floor Support · crackedWING CENTER SECTION - CRACKED SUPPORT FLOOR AT BS 540 LBL 2 WL 208 (MARKED)<[01] REMOVED AND REPLACED CRACKED FLOOR SUPPORT AT BS 540 BL0-LBL25 WL 208 PER SRM 51-40-02; DWG#143A0060.;[02] VERIFIED COMPLETION OF CORRECTIVE ACTIONS 1 AND MEASUREMENT TABLE.SDR SWAA2023120517549Floorbeam · corrodedAFT PASSENGER COMPARTMENT FLOOR STRUCTURE - WET AREAS - CORROSION ON FLOOR BEAM BS 947 LBL 23.5 WL 208 (MARKED)<[01] VERIFIED MEASUREMENT TABLE.;[02] REMOVED AND REPAIRED DAMAGES FLANGE OF THE FLOOR BEAM BS947 LBL9-LBL36 WL208 I.A.W SRM 53-70-51-2R-5 REPAIR 5 SDR SWAA2023120517555Floorbeam · corrodedAFT PASSENGER COMPARTMENT FLOOR STRUCTURE - WET AREAS - CORROSION ON FLOOR BEAM BS 947 LBL 15.75 WL 208 (MARKED)<[01] FAULT RESOLVED ON OTHER FAULT<BR>DAMAGE TO BE REPAIRED ON FAULT TTG8Q00PEN6P DUE TO EXCEED LIMITS GIVEN PER SRM 53-70-51-1A-1 AND REQUIRED A RSDR SWAA2023120517171Web · corrodedCORROSION FWD CARGO BAY SUB THRESHOLD WEB MULTIPLE AREAS AROUND NUT PLATE HOLES BS440+10' TO BS490' RBL 26.5 WL156<[01] VERIFIED STEPS 1;2 COMPLETE AND MEASUREMENT TABLE.;[02] REMOVED AND REPLACED FWD CARGO BAY SUB THRESHOLD WEB BS 440-492 RBL 26.5 WL 156 PER SDR SWAA2023120517172Shield · corrodedCORROSION FWD CARGO BAY AFT SHIELD BS500+3 TO BS500+17 RBL22 WL156 HAS MULTIPLE AREAS AROUND NUT PLATE HOLES<[01] VERIFIED STEP 1;2 COMPLETE.;[02] DAMAGED SHIELD REPLACED DUE NO DATA FOUND ON SRM NEW SHIELD LOCATED; DRILLED AND INSTALLED IAW SRM 51-40-02-0G-0 SDR SWAA2023120517173Support · corrodedCORROSION FWD CARGO BAY AFT LOWER BULKHEAD SUPPORT HAS MULTIPLE AREAS AROUND FASTENER HOLES BS500I LBL21 TO RBL21<[01] VERIFIED STEPS 1;2 COMPLETE AND MEASUREMENT TABLE.;[02] CORROSION ON LOWER BULKHEAD SUPPORT WAS FOUND TO BE OUT OF LIMITS. REMOVED; REPLACED SDR SWAA2023120517174Support Plate · corrodedCORROSION FWD CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS500A TO BS500I RBL22 WL156<[01] VERIFIED STEPS 1;2 COMPLETE AND MEASUREMENT TABLE.;[02] CUSTOMER CARD COMPLETE AND VERIFIED MEASUREMENT TABLE.;[03] CORROSION ONSDR SWAA2023120517178Shield · corrodedCORROSION AFT CARGO BAY SHIELD FWD OF CARGO DOOR AROUND MULTIPLE NUT PLATE HOLES BS767+3 TO BS794 RBL22 WL156<[01] VERIFIED STEPS 1;2 COMPLETE.;[02] CORROSION ON SHIELD FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM. PART REPLACEMENT REQUIRED SDR SWAA2023120517175Web · corrodedCORROSION AFT CARGO BAY SUB THRESHOLD WEB MULTIPLE AREAS AROUND NUT PLATE HOLES BS787+18' TO BS827+10' RBL 26 WL156<[01] VERIFIED STEPS 1;2 COMPLETE AND MEASUREMENT TABLE.;[02] CORROSION ON AFT CARGO BAY SUB THRESHOLD WEB WAS FOUND TO BE OUT OF LIMITS. REMOVEDSDR SWAA2023120517176Support Plate · corrodedCORROSION AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE HAS MULTIPLE AREAS AROUND NUT PLATE HOLES BS727E+19' TO BS767 RBL22 WL156<[01] VERIFIED STEPS 1;2 COMPLETE AND MEASUREMENT TABLE.;[02] VERIFIED STEPS 1-6;[03] MADE CORRECTIONS AND CHANGED STEP STATUS SDR SWAA2023120517177Support Plate · corrodedCORROSION AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS727G+19' TO BS787+1' LBL22 WL156<[01] VERIFIED STEPS 1;2 COMPLETE AND MEASUREMENT TABLE.;[02] VERIFIED STEPS 1-6;[03] MADE CORRECTIONS AND CHANGED STEP STATUS TSDR SWAA2023120517180Strap · corrodedCORROSION AFT CARGO BAY FLOOR SPLICE STRAP AROUND NUT PLATE HOLE BS767+6 RBL11 WL156<[01] UPDATED MEASUREMENT TABLE. CORROSION ON STRAP 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] VERIFISDR SWAA2023120517181Strap · corrodedCORROSION AFT CARGO BAY FLOOR SPLICE STRAP AROUND NUT PLATE HOLE BS727D+6 RBL6 WL156<[01] UPDATE MEASUREMENT TABLE. CORROSION ON STRAP 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 SWAA2023120517182Strap · corrodedCORROSION AFT CARGO BAY FLOOR SPLICE STRAP AROUND NUT PLATE HOLE BS727I+6 RBL10 WL156<[01] UPDATE MEASUREMENT TABLE. CORROSION ON STRAP 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] VERIFISDR SWAA2023120517183Strap · corrodedCORROSION AFT CARGO BAY FLOOR SPLICE STRAP AROUND NUT PLATE HOLE BS887 RBL11.5 WL168<[01] UPDATE MEASUREMENT TABLE. CORROSION ON STRAP 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 SWAA2023120517302Web · crackedRIGHT WING DEFLECTION CONTROL RIB WEB IS CRACKED AT THE O/B UPPER FASTENER CORNER (MARKED)<[01] UPDATED MEASUREMENTS; AND STEPS 1 & 2.;[02] REMOVED; REPLACED; AND INSTALLED A NEW R/W; T/E DEFLECTION CONTROL RIB WEB IAW SRM 51-40-02 AND BOEING DWG 115A2512. ALSSDR SWAA2023120516251Skin · debondedPANEL 194CL OUTER SKIN IS DISBONDED NEAR CENTER OF PANEL. (MARKED)<[01] PANEL 194CL WITH OUTER SKIN IS DISBONDED NEAR CENTER OF PANEL WAS REPAIRED IAW SRM 51-70-05-2R-2.;[02] VERIFIED CORRECTIVE ACTION ITEM 1 AND MEASUREMENTS TABLE. JOB COMPLETE.SDR SWAA2023100909080Fseu · faultyFLAP MALFUNCTION AT FLAPS 5. NO ASYMMETRY NOTED. T/EDGE FLAPS DISAGREE QRH RUN. C/W ALTN FLAPS DUTY CYCLE<[01] REMOVED AND REPLACED T/E FLAP POSITION INDICATOR PER M/M OPS CHECKED GOOD PER M/M 27-58-02; ALSO R AND R FSEU BOX PER M/M 27-58-02 OPS CHECKED GOOD- SDR SWAA2023100908968Indicator · faultyFLAP MALFUNCTION AT FLAPS 5. NO ASYMMETRY NOTED. T/EDGE FLAPS DISAGREE QRH RUN. C/W ALTN FLAPS DUTY CYCLE<[01] REMOVED AND REPLACED T/E FLAP POSITION INDICATOR PER M/M OPS CHECKED GOOD PER M/M 27-58-02; ALSO R AND R FSEU BOX PER M/M 27-58-02 OPS CHECKED GOOD- SDR SWAA2023072481288Slide · out of positionFWD SVC DOOR SLIDE GIRYT BAR HARD TO INSTALL/REMOVE<[01] REPOSITION FWD SVC DOOR ESCAPE SLIDE IN CONTAINER PER AMM 25-66-01
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