N8553W
Service difficulty reports · 78
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 = 'N8553W' 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 = 'N8553W' 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 SWAA2023112813658Angle · corrodedSURFACE CORROSION ON R/H TRANSITION ANGLE STA. 727I - 727J RBL 21 (MARKED)<[01] REMOVED CORROSION ON RH TRANSITION ANGLE STA 727I - 727J. REMAINING THICKNESS IS 0.034. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2;[02] C/W INSP. CORROSION ON RH TRANSITION ANSDR SWAA2023112813657Angle · corrodedSURFACE CORROSION ON R/H TRANSITION ANGLE STA. 727J - 747 RBL 21 (MARKED)<[01] REMOVED CORROSION ON RH TRANSITION ANGLE STA 727J- 747. REMAINING THICKNESS IS 0.035. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2;[02] C/W INSP. CORROSION ON RH TRANSITION ANGLESDR SWAA2023112813659Angle · corrodedSURFACE CORROSION ON R/H TRANSITION ANGLE STA. 747 - 767 RBL 21 (MARKED)<[01] REMOVED SURFACE CORROSION IN AFT CARGO R/H TRANSITION ANGLE AT STA. 747-767 RBL 21 PER SRM 51-10-02.;[02] REMOVED CORROSION ON RH TRANSITION ANGLE STA 747 - 767. REMAINING THICKNESS SDR SWAA2023112813660Angle · corrodedSURFACE CORROSION ON R/H TRANSITION ANGLE STA. 727D - 727E RBL 21 (MARKED)<[01] REMOVED CORROSION ON RH TRANSITION ANGLE STA 727D- 727E. REMAINING THICKNESS IS 0.035. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2;[02] C/W INSP .REMOVED CORROSION ON RH TRANSISDR SWAA2023113013610Floor Support · corrodedCORROSION ON FLOOR SUPPORT AT SEVERAL FASTENER HOLES BS947+3 LBL15 -LBL48<[01] REMOVED FLOOR SUPPORT BS 947 +3 LBL 16 TO LBL 24 IAW SRM 51-40-02.;[02] REMOVED INTERCOSTAL BS947 TO BS967 LBL 24 IAW SRM 51-40-02.;[03] REMOVED FLOOR SUPPORT ANGLE BS947 +3 LBL24 TSDR SWAA2023113013592Floor Support · corrodedCORROSION ON FLOOR SUPPORT AT MULTIPLE FASTENER HOLES BS947+3 RBL39 -RBL46<[01] REMOVED CORROSION ON FLOOR SUPPORT AT BS947+3 RBL39- RBL46 IN BORE HOLES AND SURROUNDING AREAS; DAMAGE FOUND TO BE OUT OF LIMITS (REMOVED 0.009? OF 0.070?) IAW SRM 53-70-51-1A-1.;[SDR SWAA2023113013591Floorbeam · corrodedCORROSION ON FLOOR BEAM AT FASTENER HOLE 986.5 LBL 43<[01] BLENDED CORROSION ON UPPER FLANGE OF FLOOR BEAM 986.5 AT LBL 43? PER SRM 51-10-02. REMOVED .016? OF MATERIAL. REMAINING THICKNESS IS .134?. DAMAGE REMOVAL IS OUT OF LIMITS PER SRM 53-70-51-1A-1.;[02] VSDR SWAA2023112813604Floor Panel · corrodedAFT CARGO FLOOR PANEL 140EF HAS CORROSION ALONG I/B AND O/B EDGES.<[01] R & R FLOOR PANEL 140EF IAW AMM 25-52-10. SEE N/R TTG8Q00P27UE FOR P/N INFO;[02] INSPECTION COMPLETE ON CORRECTIVE ACTION #1 FOR PANEL REPLACEMENT. SEE TTG8Q00NE6LA FOR OK TO CLOSE PANEL.SDR SWAA2023112813605Floor Panel · corrodedAFT CARGO FLOOR PANEL 140BF HAS CORROSION ALONG I/B AND O/B EDGES.<[01] R & R CARGO FLOOR PANEL 140BF IAW AMM 25-52-10. SEE N/R CARD TTG8Q00P28PM FOR PART INFORMATION.;[02] INSPECTION COMPLETE ON CORRECTIVE ACTION #1 FOR PANEL REPLACEMENT. SEE TTG8Q00NE6LG FORSDR SWAA2023112813606Floor Panel · corrodedAFT CARGO FLOOR PANEL 140AF HAS CORROSION ALONG I/B AND O/B EDGES.<[01] R & R FLOOR PANEL 140AF IAW AMM 25-52-10. SEE N/R TTG8Q00P27TY FOR P/N INFO;[02] INSPECTION COMPLETE ON CORRECTIVE ACTION #1 FOR PANEL REPLACEMENT. SEE TTG8Q00NE6LJ FOR OK TO CLOSE PANEL.SDR SWAA2023112813589Floor Panel · corrodedAFT CARGO FLOOR PANEL 140DF HAS CORROSION ALONG I/B AND O/B EDGES.<[01] R & R CARGO FLOOR PANEL 140DF IAW AMM 25-52-10. SEE N/R CARD TTG8Q00P630D FOR PART INFORMATION.;[02] INSPECTION COMPLETE ON CORRECTIVE ACTION #1 FOR PANEL REPLACEMENT. SEE TTG8Q00NE6LC FORSDR SWAA2023112813588Floor Panel · corrodedAFT CARGO FLOOR PANEL 140CF HAS CORROSION ALONG I/B AND O/B EDGES.<[01] R & R CARGO FLOOR PANEL 140CF IAW AMM 25-52-10. SEE N/R CARD TTG8Q00P27Z1 FOR PART INFORMATION.;[02] INSPECTION COMPLETE ON CORRECTIVE ACTION #1 FOR PANEL REPLACEMENT. SEE TTG8Q00NE6LE FORSDR SWAA2023112813599Floor Support · crackedPASSENGER CABIN STA 540; BL - 0 TO RBL 23 FLOOR SUPPORT IS CRACKED.<[01] REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-40-02.;[02] C/W INSPECTIONSDR SWAA2023112813600Floor Support · crackedPASSENGER CABIN STA 540; BL - 0 TO LBL 23 FLOOR SUPPORT IS CRACKED.<[01] REMOVED AND REPLACED PASSENGER CABIN FLOOR SUPPORT AT STA 540 BL-0 TO LBL 23 IAW SRM 51-40-02.;[02] VERIFIED CA 1. LONNIE HERMANN (TECHNICIAN); 25-OCT-2023 05:16 UTC<BR>REMOVED AND REPLACSDR SWAA2023112812513Handle · damagedFORWARD ENTRY DOOR LINER 831AW CREASED AT ASSIST HANDLE WITH THE ALUMINUM REINFORCING ANGLE CRACKED. AREA MARKED.<[01] REMOVED AND REPLACED LINER PER M/M REF 52-11-31;[02] REMOVED AND REPLACED LINER PER M/M REF 52-11-31. LINER WILL BE INSTALLED ON CARD TTG8Q00SDR SWAA2023113012479Plate · crackedRH WING LOWER T/E WAFFLE PLATE BROKEN (JUST INBD OF #7 FLAP TRANSMISSION)<[01] R/R WAFFLE PLATE IAW SRM 51-40-02.;[02] C/W INSPECTION.SDR SWAA2023113018756Panel · corrodedFUELING PANEL HAS LIGHT CORROSION AROUND INDICATOR HOLES.<[01] R&R FUELING PANEL AND OPS CHECK GOOD PER AMM 28-41-61.SDR SWAA2023112812491Attach Bracket · crackedLEFT WING DEFLECTION RIB COVE WEB OUTBOARD ATTACH BRACKET IS CRACKED. (MARKED)<[01] REMOVED DAMAGED BRACKET PER SRM 51-40-02;[02] INSTALLED NEW BRACKET ON L/H WING DEFLECTION RIB COVE WEB PER SRM 51-40-02.;[03] C/W INSP .INSTALLED NEW BRACKET ON L/H WING DEFLESDR SWAA2023112812355Slat · delaminated#8 SLAT LOWER SURFACE HAS A DELAMINATED AREA 3.5'X3' ON O/B END.<[01] REMOVED #8 SLAT.;[02] ACCOMPLISHED VISUAL INSP. OF #8 INBD SLAT CAN. OK TO INSTALL #8 SLAT PER MM 27-81-21;[03] R&R #8 SLAT PER AMM 27-81-21.;[04] C/W RII INSPECTION;[05] R&R #8 SLAT PER AMMSDR SWAA2023070574440Slide · looseFWD ENTRY DOOR GRIT BAR PLASTIC SLEEVE LOOSE<[01] ADJUSTED GRIT BAR LOCKING SLEEVE ON FWD ENTRY DOOR PER SIP.SDR SWAA2023061458177Slide · out of positionFLIGHT ATTENDATS REPORT L1 DOOR GIRT BAR DIFICULT TO STOW<[01] REPOSITIONED FWD ENTRY DOOR SCAPE SLIDE PER AMM 25-66-01SDR SWAA2023061257694Girt Bar · out of adjustCREW REPORTS L1 DOOR GIRT BAR DIFFICULT TO STOW AND UNSTOW<[01] ADJUSTED INNER LATCH BRACKET FOR GIRT BAR ON L1 DOOR PER AMM 25-66-01-200-802SDR SWAA2023031617044Flashlight · inoperativeFWD LEFT FA FLASHLIGHT INOP. REFITTED EMERGENCY FLASHLIGHT AND TEST OK PER AMM 25-64-00SDR SWAA2022112174047Flashlight · no testFWD FA FLASHLIGHT WILL NOT TEST / [01] RESEATED FWD FLIGHT ATTENDANT EMERGENCY FLASHLIGHT. TESTS OK PER MM 25-64-00SDR SWAA2022101057511Flashlight · failedLH AFT F/A FLASHLIGHT IS BLINKING RED / [01] REMOVED AND REPLACED L/H AFT F/A FLASHLIGHT BATTERY PER SIPSDR SWAA2020090814086Battery · inoperativeAFT FLIGHT ATTENDANT A/C RIGHT OUTBOARD FLASHLIGHT TESTS RED (FLASHING), OK TO CONTINUE PER MEL 25-12-01 SP#1B TRACKING # 98373 ( CABIN EMERGENCY FLASHLIGHT HOLDERS/FLASHLIGHTS ). REPLACED BATTERY PER CMM 25-60-13.SDR SWAA2020052078636Battery · dischargedCREW REPORTED AFT FLASHLIGHT FLASHING RED / REMOVED AND REPLACED AFT FLASHLIGHT'S BATTERY AS REQUIRED PER B737 MM 25-64-00SDR SWAA2019121039438Indicator · detachedEMERGENCY LIGHT ANNUNCIATOR LIGHT IN OVERHEAD PANEL FELL OUT WHILE IN FLIGHT COULD NOT LOCATE LAMP. / INSTALLED MISSING P5 PANEL EMERGENCY LT PB SWITCH IAW SWPM.
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