N7858A
Service difficulty reports · 221
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 = 'N7858A' 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 = 'N7858A' 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 SWAA2026092967279Lamp · inoperativePASSENGER CABIN EMERGENCY LIGHT OVER SEAT 6ABC WAS INOPERATIVE. R & R THE LAMP IAW AMM 33-51-03-960-801. TEST PASSED.SDR SWAA2026060208076Megaphone · damagedAFT MEGAPHONE IS DAMAGE. REMOVED AND REPLACED AFT MEGAPHONE IAW AMM 25-64-00. INSTALLED INSPECTION DECAL. OP CHECKED GOOD.SDR SWAA2026021269550Battery Pack · no testTHE LEFT EMERGENCY LIGHTING BATTERY PACK AT ROW 20 FAILED A CAPACITY CHECK. REMOVED & REPLACED THE BATTERY PACK IAW MM 33-51-06.SDR SWAA2026021269549Battery Pack · no testFWD LEFT EMERGENCY LIGHTING BATTERY PACK FAILED A CAPACITY CHECK. REMOVED & REPLACED THE BATTERY PACK IAW MM 33-51-06.SDR SWAA2025102126549Trim Motor · inoperativeELECTRIC STABILIZER TRIM INOPERATIVE. R & R STAB TRIM MOTOR PER AMM 27-41-71 OPS CHECK NORMALSDR SWAA2025060275623Skirt · damagedAFT GALLEY SERVICE DOOR ESCAPE SLIDE SKIRT FRAYED AND RUBBER WORN <[01]. AS DOOR SLIDE REMOVED AND REPLACED ON CARD #TTG8Q011E6QR; [02] REMOVED AND REPLACED AS SLIDE PER AMM 25-66-01.; [03] INSPECTION C/W REMOVED AND REPLACED AS SLIDE PER AMM 25-66-01. AS DOOSDR SWAA2025051968500Wedge · delaminatedRT. I/B MAIN FLAP T/E WEDGE DELAMINATED.<[01] VERIFIED ACTION ITEMS.;[02] ALL ACTIONS FOR REMOVAL AND INSTALLATION COMPLETED;[03] VERIFIED ACTION ITEMS.SDR SWAA2025051956598Stringer Clip · crackedCRACKED STR CLIP AT PAX CABIN BS727C S-5L CRACKED STR CLIP AT PAX CABIN BS727C S-5L. MARKED<[01] REMOVED AND REPLACED WITH NEW CRACKED STR CLIP AT PAX CABIN BS727C S-5L. REMOVED STR CLIP AT PAX CABIN BS727C S-5L IAW SRM 51-40-02. <BR>INSTALLED NEW STR CLIP AT SDR SWAA2025051956585Support Bracket · crackedAFT CARGO BAY WATER TANK SUPPORT BRACKET BS 947 LBL 10 WL 179 IS CRACKED<[01] REMOVED AND REPLACED NEW SUPPORT BRACKET IAW SRM 51-40-02-0G-0 AND DWG 149A8103 REV:A.;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.SDR SWAA2025051956572Attach Angle · crackedCRACKED ATTACH ANGLE AT MIN CABIN BS 691; RBL 1; WL 207<[01] REMOVED AND REPLACED ATTACH ANGLE AT BS 691; RBL 1; WL 207 I.A.W SRM 51-40-02-0G-0 AND BOEING DWGS 111A6002 REV: -; 273A9111 REV: -;[02] CORRECTIVE ACTION ITEM 1 VERIFIED; CARD COMPLETE.SDR SWAA2025051956575Skin · delaminatedLEFT WING O/B AFT FLAP HAS DELAMINATION ON I/B UPPER SIDE<[01] REPAIRED DELAMINATION DAMAGE ON I/B UPPER SIDE OF LEFT WING O/B AFT FLAP IAW SRM 51-70-10-2R-4.;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.SDR SWAA2025051956581Skin · crackedRIGHT WING #6 SLAT NOSE SKIN HAS A CRACK AT ACTUATOR FITTING RIBS<[01] REPAIRED NO.6 SLAT NOSE SKIN AT ACTUATOR FITING RIB IAW SRM 57-42-01-2R-8.;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.SDR SWAA2025051956571Attach Angle · crackedCRACKED ATTACH ANGLE AT MIN CABIN BS 691; LBL 1; WL 207<[01] REMOVED AND REPLACED ATTACH ANGLE AT MIN CABIN BS691 LBL 1; WL207 I.A.W SRM 51-40-02-0G-0 AND BOEING DWGS 111A6002 REV: -; 273A9111 REV: -;[02] CORRECTIVE ACTION ITEM 1 VERIFIED; CARD COMPLETE.SDR SWAA2025051956543Seat Track · corrodedCORROSION ON LBL 24 SEAT TRACK WELL AT STA 727C+13 TO 727C+15; 727E+4 TO 727E+6; 807+17 TO 807+19; 827+13 TO 847; 847+7 TO 847+9; 867+9 TO 867+11; WL 208.3<[01] DISCREPANCIES FOUND ON THIS FAULT BEING VOID DUE TO MECHANICAL DAMAGE REPORTED ON TTG8Q00ZWAQK EXCESDR SWAA2025051956536Panel · debondedPANEL 191CL OUTER SKIN IS DISBONDED NEAR CENTER OF PANEL. (MARKED)<[01] PANEL 191CL WITH OUTER SKIN DISBONDED NEAR CENTER OF PANEL WAS REPAIRED IAW SRM 51-70-05-2R-2.SDR SWAA2025051656558Cargo Track · crackedAFT CARGO BAY CARGO TRACK IS CRACKED BS767 RBL13 WL156<[01] REPAIRED AS PER SRM 53-00-53-2R-3 AND EA 25-153-01016.;[02] VERIFIED CORRECTIVE ACTIONSDR SWAA2025051956490Attach Angle · crackedCRACKED ATTACH ANGLE AT MID CABIN BS691 RBL1 WL206. MARKED<[01] REMOVED AND REPLACED ATTACH ANGLE AT MID CABIN BS691 RBL1 WL206 I.A.W SRM 51-40-02-0G-0 AND BOEING DWGS 111A6002 REV: -; 273A9111 REV: -;[02] CORRECTIVE ACTION ITEM 1 VERIFIED; CARD COMPLETE.SDR SWAA2025051956491Attach Angle · crackedCRACKED ATTACH ANGLE AT MID CABIN BS692 RBL24 WL204. MARKED<[01] REMOVED AND REPLACED ATTACH ANGLE AT MID CABIN BS692 RBL24 WL204 I.A.W SRM 51-40-02-0G-0 AND BOEING DWGS 111A6002 REV: -; 273A9111 REV: -;[02] CORRECTIVE ACTION ITEM 1 VERIFIED; CARD COMPLETE.SDR SWAA2025051956495Floorbeam · crackedCRACKED PANEL BREAK AT MID CABIN BS540 LBL1 WL208.<[01] REMOVED AND REPLACED PANEL BREAK AT MID CABIN BS540 LBL1 WL208 IAW SRM 51-40-02-0G-0 AND DWG 143A0060;[02] VERIFIEDSDR SWAA2025051956496Floorbeam · crackedCRACKED PANEL BREAK AT MID CABIN BS540 RBL1 WL208. MARKED<[01] REMOVED AND REPLACED PANEL BREAK AT MID CABIN BS540 RBL1 WL208 IAW SRM 51-40-02-0G-0 AND DWG 143A0060;[02] COMPLETESDR SWAA2025051956464Doubler · crackedEGPR SURROUND DOUBLER IS CRACKED BS233 WL175 8' ABOVE S-24R MARKED<[01] TRIMMED OUT THE DAMAGED AREA OF THE EGPR SURROUND DOUBLER IAW SRM 53-10-15-2R-4 REPAIR 4 PARG 4(C); FABRICATED -2 DOUBLER; MADE FROM 2024T3#0.050 LOT# 1558343-1 AND -3 FILLER; MADE FROM 20SDR SWAA2025051956409Wire · damagedG4 GALLEY EMERGENCY EXIT LIGHT QUICK DISCONNECT WIRE DAMAGED<[01] REMOVED & REPLACED G4 EMERGENCY EXIT LIGHT IAW AMM 33-51-01-960-802 3.C.(5)(6);[02] VERIFIED CORRECTIVE ACTION #1SDR SWAA2025020391914Handle · looseFORWARD ENTRY L1 DOOR HANDLE LOOSE<[01] ADJUSTED FORWARD ENTRY L1 DOOR HANDLE PER AMM 52-11-00.SDR SWAA2024111960211Battery Pack · inoperativeAFT EMERGENCY LIGHTS ASSOCIATED WITH PACK M1672 INOP.<[01] REMOVED AND REPLACED THE M1672 EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-06. OPS CHECK GOOD.SDR SWAA2024072918565Lamp · inoperativeR/H AFT EXTERIOR EMERGENCY LIGHT INOP<[01] RELAMPED THE R/H AFT EXTERIOR EMERGENCY LIGHT REF AMM 33-51-04. OPS CHECK GOOD AT THIS TIME.SDR SWAA2024020246489Lamp · inoperativeEMERGENCY LIGHT BY AFT SERVICE DOOR ON THE OUTSIDE IS INOP<[01] RELAMPED RH AFT EMERGENCY LIGHT PER AMM 33-51-04. OPS CHECK GOOD.SDR SWAA2023101109072Retainer · looseGIRT BAR RETAINER ON FORWARD SERVICE DOOR DOES NOT SECURELY HOLD GIRT BAR.<[01] STRAIGHTENED FWD SERVICE DOOR GIRT BAR RETAINER CLIPS IAW AMM 25-66-01. GIRT BAR RETENTION IS NORMAL. A/C OK FOR SERVICE.SDR SWAA2023092503079Clamp · did not stowFWD ENTRY DOOR SLIDE IS DIFFICULT TO ARM<[01] REPLACED SLIDE CLAMP ASSY PER AMM 25-66-00SDR SWAA2023042841334Slide · out of adjustCABIN PASSENGER L2 DOOR SLIDE SKIRT TOUCHING LOWER FRAME STRUCTURE<[01] ACCOMPLISHED REPOSITION OF AFT ENTRY ESCAPE SLIDE REF; SOUTHWEST MT CARD 725-61-06 STEPS 3A;3B;3C;3G AND 3K.;[02] VERIFIED WORK PERFORMED;[03] STEP 1 SHOULD READ: ACCOMPLISHED REPOSITION OSDR SWAA2023042841335Skirt · out of adjustCABIN PASSENGER R2 DOOR SLIDE SKIRT TOUCHING LOWER FRAME STRUCTURE<[01] ACCOMPLISHED REPOSITION OF AFT GALLEY SERVICE DOOR ESCAPE SLIDE REF; SOUTHWEST MT CARD 725-61-06 STEPS 3A;3B;3C;3G AND 3K.;[02] VERIFIED WORK PERFORMED;[03] STEP 1 SHOULD READ: ACCOMPLISHESDR SWAA2023050129554Panel · crackedPANEL 193D SEVERAL ATTACHMENT HOLES CRACKED<[01] FAULT RAISED IN ERROR; PANEL WAS REPLACED ON T/C TTG8Q00JRU9QSDR SWAA2023050128220Scuff Plate · crackedFOUND AFT CARGO FWD SCUFF PLATE CRACKED<[01] RECIEVED FWD SCUFF PLATE P/N 146A8341-7; PO# 2012626 AND REF. TTG8Q00JZ1G7 FOR SCUFF PLATE INSTALLATION.;[02] RECIEVED FWD SCUFF PLATE P/N 146A8341-7; PO# 2012626 AND REF. TTG8Q00JZ1G7 FOR SCUFF PLATE INSTALLATION.SDR SWAA2023050128221Scuff Plate · crackedFOUND AFT CARGO AFT SCUFF PLATE CRACKED<[01] RECIEVED AFT SCUFF PLATE P/N 146A8341-9; PO# 1772343 AND REF. TTG8Q00JZ1G7 FOR SCUFF PLATE INSTALLATION.;[02] RECIEVED AFT SCUFF PLATE P/N 146A8341-9; PO# 1772343 AND REF. TTG8Q00JZ1G7 FOR SCUFF PLATE INSTALLATION.SDR SWAA2023050124699Strap · elongatedAFT CARGO COMPARTMENT AT STA 727D; RBL 21; WL 156 FRAME HAS ELONGATED HOLE.<[01] REAMED UP ELONGATED HOLES ON DAMAGED FRAME AT STA. 727D PER REF. SRM 51-10-02-0G-0 AND SRM 53-60-07-2R-2; FINAL HOLE DIAMETER ON UPPER HOLE 0.247'; VENIER CALIPER USED B/C 174952;SDR SWAA2023050124701Strap · elongatedAFT CARGO COMPARTMENT FLOOR AT STA 747; RBL 21; WL 156 FRAME HAS ELONGATED HOLE.<[01] REAMED UP ELONGATED HOLES ON DAMAGED FRAME AT STA. 747 PER REF. SRM 53-60-07-2R-2; FINAL HOLE DIAMETER ON UPPER HOLE 0.247' AND ON LOWER HOLE 0.247'; VENIER CALIPER USED B/C SDR SWAA2023050124704Strap · elongatedAFT CARGO COMPARTMENT FLOOR AT STA 767; RBL 21; WL 156 FRAME HAS ELONGATED FASTENER HOLE.<[01] REAMED UP ELONGATED HOLES ON DAMAGED FRAME AT STA. 767 PER REF. SRM 53-60-07-2R-2; FINAL HOLE DIAMETER ON UPPER HOLE 0.247'AND ON LOWER HOLE 0.247'; VENIER CALIPER USDR SWAA2023050124114Channel · elongatedR/H AFT CARGO COMPARTMENT Z CHANNEL AT STA727D - STA727E HAS ELONGATED HOLES.<[01] REF TASK 'TTG8Q00JZGZA' FOR PARTS INSTALLATION;[02] CORRECTION TO STEP 1: REF TASK TTG8Q00JZGZA FOR ZEE CHANNEL REPLACMENT;[03] VERIFIED Z CHANNEL WILL BE REPLACED ON T/C TTG8Q0SDR SWAA2023050124116Channel · elongatedR/H AFT CARGO COMPARTMENT Z CHANNEL AT STA747 - STA767 HAS ELONGATED HOLES.<[01] RECIEVED NEW PART# 146A7502-51 PO# 2012626; REF TASK 'TTG8Q00JZGZA' FOR PARTS INSTALLATION;[02] VERIFIED STEP 1.SDR SWAA2023050124115Channel · corrodedREJECT....CORROSION AFT CARGO COMPARTMENT Z - CHANNEL LOWER SURFACE AT STA 727D - STA727E RBL 21 WL 156 HAS CORROSION<[01] REMOVED CORROSION AT AFT CARGO COMPARTMENT Z CHANNEL LOWER SURFACE AT STA 727D-STA 727E RBL21 WL 156 PER REF SRM 51-10-02-0G-0;[02] STEP SDR SWAA2023050123239Panel · elongatedACCESS PANEL 561BB SEVERAL FASTENER HOLES ENLONGATED<[01] ACCOMPLISHED REPAIR AT ACCESS PANEL 561BB PER SRM 51-70-04-2R-9;[02] VERIFIED REPAIRSDR SWAA2023050122725Channel · elongatedL/H AFT CARGO COMPARTMENT FLOOR Z-CHANNEL AT STA 727B - STA 727C LBL 21 HAS ELONGATED HOLE.<[01] RECIEVED NEW Z-CHANNEL PART# 146A7502-27 PO# 2012626; REF TASK CARD TTG8Q00JZHM2 FOR PARTS INSTALLATION;[02] VERIFIED RECIEVING Z CHANNEL TO BE INSTALLED ON T/C TTSDR SWAA2023050122726Channel · elongatedL/H AFT CARGO COMPARTMENT FLOOR Z-CHANNEL AT STA 727D - STA 747 LBL 21 HAS ELONGATED HOLES.<[01] REF TASK CARD TTG8Q00JZHM2 FOR PARTS INSTALLATION.;[02] CORRECTION TO STEP 1: REF TASK CARD TTG8Q00JZHM2 FOR ZEE CHANNEL REPLACEMENT;[03] VERIFIED STEP 2.SDR SWAA2023050122727Channel · elongatedL/H AFT CARGO COMPARTMENT FLOOR Z-CHANNEL AT STA 787 - STA 807 LBL 21 HAS ELONGATED HOLES.<[01] REF TASK CARD TTG8Q00JZHM2 FOR PARTS INSTALLATION.;[02] CORRECTION TO STEP 1: REF TASK CARD TTG8Q00JZHM2 FOR ZEE CHANNEL REPLACEMENT;[03] VERIFIED Z CHANNEL WILL BESDR SWAA2023050122728Channel · elongatedL/H AFT CARGO COMPARTMENT FLOOR Z-CHANNEL AT STA 747 - STA 787 LBL 21 HAS ELONGATED HOLES.<[01] REF TASK CARD TTG8Q00JZHM2 FOR PARTS INSTALLATION.;[02] CORRECTION TO STEP 1: REF TASK CARD TTG8Q00JZHM2 FOR ZEE CHANNEL REPLACEMENT;[03] VERIFIED Z CHANNEL WILL BESDR SWAA2023050121521Bracket · elongatedFLIGHT DECK DOOR UPPER I/B CORNER BRACKET HOLES ENLONGATED<[01] REMOVED AND REPLACED WEB AND BRACKET AT STA 277 FLIGHT DECK DOOR UPPER I/B CORNER STR 2R AS PER SRM 51-40-02-0G-0 AND DRAWING 141A9402.;[02] VERIFIED REMOVE AND REPLACE WEB AND BRACKET;[03] VERIFISDR SWAA2023050120035Panel · crackedAFT CARGO COMPARTMENT BULKHEAD ACCESS PANEL EXTERNAL SURFACE CRACKED. AFT CARGO COMPARTMENT AFT BULKHEAD ACCESS PANEL EXTERNAL SURFACE CRACKED.<[01] REMOVED DAMAGE AREA AND APPLIED THE GLASS FABRIC REPAIR PLIES AT DAMAGED AREA ON AFT CARGO COMPARTMENT BULKHEADSDR SWAA2023050119834Support Angle · elongatedFWD CARGO COMPARTMENT R/H SIDE WALL SUPPORT ANGLE LOWER FASTENER HOLE ELONGATED @ S-25R STA 500D WL 156 MKD DOT<[01] REMOVED AND REPLACED RAIL FROM FWD CARGO COMPARTMENT R/H SIDE AFT B/H WALL AS PER SRM 51-40-02-0G-0 AND DWG 143A9481.;[02] VERIFIED STEP 1SDR SWAA2023050119835Channel · corrodedCORROSION FWD CARGO COMPARTMENT L/H FLOOR SUPPORT Z CHANNEL AROUND FASTENER HOLE @ S-25L STA 500A+7' WL 156 MKD DOT<[01] VERIFIED STEP 5SDR SWAA2023050119832Shield · corrodedCORROSION AT FWD CARGO COMPARTMENT. TRANSITION SHIELD FLOOR SUPPORT PANEL @ S-25R BETWEEN STA 500 & 500A WL156<[01] REMOVED AND REPALCE SHIELD AT FWD CARGO COMPARTMENT FLOOR SUPPORT PANEL @ S-25R BETWEEN STA 500 & 500A WL156 AS PER SRM 51-40-02-0G-0 AND DWG 14SDR SWAA2023050119593Stiffener · crackedRIGHT HORIZONTAL STABILIZER RIB #5 STIFFENER #3 CRACK AT LOWER SECTION<[01] INSTALLED REPAIR PARTS AT R/H HORIZONTAL STABILIZER RIB #5; STIFFENER #3 REF SRM 55-10-09-2R-4 AND APPLIED FILET SEAL REF SRM 51-20-05-0G-0.<BR>SEALANT APPLICATION. MIXED TIME 22:00 PM
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