N8556Z
Service difficulty reports · 89
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 = 'N8556Z' 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 = 'N8556Z' 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 SWAA2023120718252Angle · corrodedAFT CARGO L/H TRANSITION ANGLE HAS CORROSION ON UPPER SURFACE STA 727J TO 727J+22 LBL 22. MRKD<[01] AFT CARGO COMPARTMENT DAMAGE ON LT SIDEPLATE CHANNEL UPPER SURFACE FORM STA 727J TO STA 727J + 22; LBL 22; WL 155 WAS FOUND TO BE OUT OF ALLOWABLE LIMITS IAW SRSDR SWAA2023120718253Angle · corrodedAFT CARGO R/H TRANSITION ANGLE HAS CORROSION ON UPPER SURFACE STA 727J TO 727J+22 RBL 22. MRKD<[01] AFT CARGO COMPARTMENT RT SIDEPLATE CHANNEL DAMAGE BETWEEN STA 727J TO STA 727J + 22 ; RBL 21; WL 155 WAS FOUND TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-53-1ASDR SWAA2023120718254Angle · corrodedAFT CARGO R/H TRANSITION ANGLE HAS CORROSION ON UPPER SURFACE STA 747 TO 765 RBL 22. MRKD<[01] AFT CARGO COMPARTMENT RT SIDEPLATE CHANNEL DAMAGE BETWEEN STA 747 TO STA 767; RBL 22; WL 155 WAS FOUND TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-53-1A-2. SIDEPLATESDR SWAA2023120718255Angle · corrodedAFT CARGO L/H TRANSITION ANGLE HAS CORROSION ON UPPER SURFACE STA 747 TO 767 LBL 22. MRKD<[01] AFT CARGO COMPARTMENT DAMAGE ON LT SIDEPLATE CHANNEL UPPER SURFACE FORM STA747 TO STA 767 ; LBL 22; WL 155 WAS FOUND TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-53-1SDR SWAA2023120718256Angle · corrodedAFT CARGO R/H TRANSITION ANGLE HAS CORROSION ON UPPER SURFACE STA 767 TO 787 RBL 22. MRKD<[01] AFT CARGO COMPARTMENT RT SIDEPLATE SHIELD ASSEMBLY DAMAGE BETWEEN STA 767 TO STA 792; RBL 21; WL 155 WAS FOUND TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-53-1A-2.;[SDR SWAA2023120718265Angle · corrodedAFT CARGO L/H TRANSITION ANGLE HAS CORROSION ON UPPER SURFACE STA 767 TO 787 LBL 22. MRKD<[01] AFT CARGO COMPARTMENT DAMAGE ON LT SIDEPLATE CHANNEL UPPER SURFACE FORM STA 767 TO STA 787 ; LBL 22; WL 155 WAS FOUND TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-53-SDR SWAA2023120718267Strap · corrodedAFT CARGO FLOOR PANEL SPLICE STRAP HAS CORROSION ON UPPER SURFACE AROUND SEVERAL N/P HOLES AT STA 772. MRKD<[01] AFT CARGO COMPARTMENT DAMAGE ON SPLICE TEE ASSEMBLY UPPER SURFACE IN STA 767 + 5 RBL 22; LBL 22; WL 155 WAS FOUND TO BE OUT OF ALLOWABLE LIMITS IAWSDR SWAA2023120817684Floor Support · elongatedFOUND HOLE NOT ROUND AT FLIGHT DECK FLOOR BS 255 RBL 5 FOUND HOLE NOT ROUND AT FLOOR DECK BS 255 RBL 5<[01] REPAIRED ON STEPS 24-29 ON EA M23-153-03295;[02] GREGORY BAXTER (TECHNICIAN); 27-NOV-2023 15:26 UTC<BR>REPAIRED ON STEPS 24-29 ON EA M23-153-03295;[03] SDR SWAA2023120717573Angle · corrodedCORROSION ON AFT SERVICE DOOR Z ANGLE AT STA 983 RBL 48. MARKED.<[01] REMOVED CORROSION (0.003) PER SRM 51-10-02;[02] INSPECTED DAMAGE REMOVAL AS REQUIRED. CORRECTIVE ACTION #1. PERFORMED HFEC INSPECTION OF DAMAGE REMOVAL AREA IAW 737 NDT PART 6; 51-00-00 PROCSDR SWAA2023120717711Floorbeam · corrodedTOP SURFACE OF FLOOR BEAM @STA 947; LBL 52 HAS CORROSION OUTBOARD SIDE OF LAV MOUNT TOP SURFACE OF FLOOR BEAM @STA 947 LBL 52 HAS CORROSION OUTBOARD SIDE OF LAV MOUNT<[01] REMOVED CORROSION PER SRM 51-10-02. FOUND AREA OUT OF LIMITS PER SRM 53-70-51-1A-1.;[02]SDR SWAA2023120717351Lens · damagedRIGHT OVERWING EMERGENCY EXIT DOORS EXTERIOR FUSELAGE EMERGENCY LIGHTS LENS FILLED WITH MOISTURE. 2EA.<[01] INSPECTED LENS PER AMM 33-51-04. NO MOISTURE NOTED ON OPAQUE LENS.SDR SWAA2023120517353Retainer · looseLEFT EMERGENCY EXIT HATCH ESCAPE STRAP RED VELCRO RETAINER NOT ATTACHED TO FUSELAGE WITH STRAP STOWED.<[01] REINSTALLED VELCRO RETAINER PER AMM 25-61-10.SDR SWAA2023120517352Retainer · looseRIGHT EMERGENCY EXIT HATCH ESCAPE STRAP RED VELCRO RETAINER NOT ATTACHED TO FUSELAGE WITH STRAP STOWED.<[01] REINSTALLED VELCRO RETAINER PER AMM 25-61-10.SDR SWAA2023121116614Web · crackedWEB IB OF RIGHT WING DEFLECTION ROLLER CRACKED AT UPPER OB RIVET; MARKED.<[01] REMOVED AND REPLACED WEB PER SRM 51-10-02.;[02] COMPLIED WITH INSPECTION; REMOVED AND REPLACED WEB PER SRM 51-10-02.SDR SWAA2023121116616Attach Bracket · crackedRIGHT WING DEFLECTION ROLLER SUPPORT BEAM ATTACH BRACKET IS CRACKED ON FWD SIDE; MARKED.<[01] REMOVED AND REPLACED ATTACH BRACKET PER SRM 51-10-02;[02] COMPLIED WITH INSPECTION; REMOVED AND REPLACED ATTACH BRACKET PER SRM 51-10-02.SDR SWAA2023120716617Plate · crackedRIGHT WING WIGGLE PLATE UNDER WING PANEL 651EB CRACKED AT RIVET; MARKED.<[01] REMOVED AND REPLACED THE WIGGLE PLATE UNDER RH WING PANEL 651EB PER SRM 51-40-02.SDR SWAA2023120716951Floor Support · crackedPASSENGER FLOOR SUPPORT ANGLE IS CRACKED; B.S.540 RBL 2<[01] REMOVED AND REPLACED FLOOR SUPPORT ANGLE PER SRM 51-40-02.;[02] REJECT: MEASUREMENT ITEM #10 SHOULD BE ANSWERED YES AS FAULT FAILURE TYPE IS LISTED AS 05 (DAMAGE). REFERENCE MPM 52.02.01.;[03] REJECTSDR SWAA2023120716934Attach Fitting · puncturedL-2 DOOR LINER TEDLAR PUNCTURED NEAR SLIDE AFT ATTACH POINT.<[01] REPAIRED AFT ENTRY DOOR LINER PER AMM 25-00-00.SDR SWAA2023120716950Floor Support · crackedPASSENGER FLOOR SUPPORT ANGLE IS CRACKED; B.S.540 LBL 2<[01] REMOVED AND REPLACED PASSENGER FLOOR SUPPORT ANGLE B.S.540 PER SRM 51-40-02;[02] C/W INSPECTION.SDR SWAA2023121122349Panel · looseLEFT WING UPPER TRAILING EDGE PANEL OUTBD OF NACELLE STRUT FAIRING ATTACH POINT TO DEFLECTION RIB HAS PLAY; LOOSE<[01] REMOVED INBOARD AND OUTBOARD SERRATED PLATES PER SRM 57-51-02.;[02] CUT OUT DAMAGED SECTION OF DEFLECTION RIB UPPER TAB PER SRM 57-51-02-2R-4SDR SWAA2023121116159Floor Panel · crackedAFT CARGO PANEL 142YDC CRACKED.<[01] REMOVED AND REPLACED PANEL PER AMM 21-32-05.SDR SWAA2023120716164Panel · crackedAFT CARGO PANEL142KW CRACKED.<SDR SWAA2023081689216Floor Panel · separatedAFT CARGO LH SIDE; SECOND PANEL AFT OF BULKHEAD SEPERATED FROM FLOOR<[01] OK TO CONTINUE PER MEL 25-16-01; SP1B;[02] R&R CARGO PANELS 141DW & 141FW IAW AMM 25-52-06SDR SWAA2023081690187Floor Panel · separatedAFT CARGO LH SIDE; SECOND PANEL AFT OF BULKHEAD SEPERATED FROM FLOOR<[01] OK TO CONTINUE PER MEL 25-16-01; SP1B;[02] R&R CARGO PANELS 141DW & 141FW IAW AMM 25-52-06SDR SWAA2023080986427Battery Pack · inoperativeEMERGENCY LIGHTS INOP AT FWD ENTRY DOOR<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK (M1675) IAW AMM 33-51-06. OPS CHECK GOOD.SDR SWAA2023041928272Light · inoperativeFWD EXTERIOR EMERGENCY LIGHT BY L1 DOOR INOP.<[01] RELAMPED FWD EXTERIOR EMERGENCY LIGHT BY L! DOOR IN REFERENCE WITH AMM 33-51-04. OPS CHECK GOOD AT THIS TIME.SDR SWAA2022121280548Overwing Exit · fault messageSUPPLEMENTAL INFORMATION: RH AFT OVERWING EXIT DOOR LIGHT IS ON WITH FAULT CODE 52-72022 R OW SW DISAGREE PRESENT ON PSEU BITE FC: 52-72022 R OW SW DISAGREE<[01] OK TO CONT PER MEL 52-3-03. SP1 COMPLIED WITH ;VERIFIED DOOR IS CLOSED<BR>AUTH # 108101;[02] PERFOSDR SWAA2022112171531Light · inoperativeSIDEWALL LIGHT ABOVE L/H FWD OVERWING EXIT INOP. / [01] OK TO CONTINUE PER MEL 33-2-04; SP1B.;[02] REMOVED AND REPLACED OVERWING EXIT LIGHT ASSEMBLY IAW AMM 33-21-00. OK FOR SERVICE.SDR SWAA2022101760161Battery · inoperativeFWD F/A JUMP SEAT FLASHLIGHT WONT TEST AND SEAL BROKEN / [01] R AND R?D FWD F/A FLASHLIGHT BATTERY IAW AMM 25-64-00SDR SWAA2022100554225Light · inoperativeLH FWD OVER-WING EXIT SIDEWALL LIGHT INOP / [01] R&R CABIN SIDEWALL LIGHTS AT 4;5;6;7;8;9;10;11;12 ABC PER AMM 33-21-00SDR SWAA2022042295549Indicator · faultyTRAILING EDGE FLAP DISAGREE. FLAPS WOULD NOT MOVE PAST 5 DEGREES USED ALTERNATE FLAP EXTENSION / [01] PERFORMED FSEU BITE PROCEDURE IAW FIM 27-51 TASK 801 NO DECEFTS NOTED. INSPECTED TRANSMISSION TORQUE TRIP INDICATORS IAW FIM 27-51 TASK 849 NO DEFECTS NOTED. SDR SWAA2022010356714Flashlight · inoperativeFWD GALLEY INBD FA FLASHLIGHT INOP ; FWD GALLEY IND FA FLASHLIGHT INOP / [01] R&R INBD F/A FLASHLIGHT BATTERY; OPS CHECK GOOD; IAW B737 AMM 25-64-00.SDR SWAA2021062586313Scuff Plate · damagedREFERENCE PREVIOUS LOGPAGE 1809366 WORKING EA 1-A53-32467. WITHIN 50 FLIGHT CYCLES REMOVE AND REPLACE AFT CARGO CENTER SCUFF PLATE PER AMM 53-11-02. IF THERE IS DAMAGE TO UNDERLYING STRUCTURE ADDRESS PER SRM OR CONTACT SERVICE ENGINEERING ( MX NOTE ) / R&R AFTSDR SWAA2020120934635Girt Bar · looseFWD ENTRY AFT GIRT BAR CLIP IS LOOSE. RESECURED GIRT BAR CLIP FWD ENTRY AFT GIRT BAR, IAW AMM 52-11-00.SDR SWAA2020102625145Motor · failedELECTRIC TRIM INOPERABLE WOULD NOT ENGAGE A OR B AUTO PILOT. R & R STAB TRIM MOTOR, PER MM 27-41-71. OPERATIONS CHECK GOOD ISSUE 3063169POS, TAG 654366 P/N OFF/ON 6355C0001-02 S/N OFF 5258 S/N ON 02232.SDR SWAA2020081708148Flashlight · inoperativeFWD OB FA FLASH LIGHT INOP ( CABIN EMERGENCY FLASHLIGHT HOLDERS/FLASHLIGHTS ) / REPLACED EMER FLASHLIGHT AS PER AMM 25-64-00 CL # 78987SDR SWAA2019020429128Sign · looseAFT EMERGENCY EXIT WALL SIGN LOOSE. REINSTALLED SIGN IAW AMM.SDR SWAA2019010928300Lens · missingRT OVERWING LOWER EMERGENCY EXIT SIGN MISSING. R&R LENS PER AMM.SDR SWAA2018082324520Battery · dischargedFORWARD GALLEY LT FLASHLIGHT INOP. R&R BATTERY PER MM.
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