N8626B
Service difficulty reports · 238
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 = 'N8626B' 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 = 'N8626B' 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 SWAA2026021862665Nut Plate · corrodedCORRODED RAIL NUT PLATE LOCATED INTERNAL CAVITY LEADING EDGE OFSS 308, LT WING. REPLACED RAIL NUT PLATE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 112A4402, SHEET 40, REV A.SDR SWAA2026021862657Plate · corrodedCORRODED RAIL PLATE, INTERNAL CAVITY OFSS 549, LT WING LE. REPLACED RAIL PLATE IAW SRM 51-10-02, ITEM 9, & SRM 51-40-02.SDR SWAA2026021862494Web · crackedCRACKED WEB, BS 344 - 360, LBL 11 IN THE FWD GALLEY AND LAVATORY. REPLACED THE WEB INTERCOSTAL, & FASTENERS IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 141A5400, SHEET, 46, REV A.SDR SWAA2026021862660Plate · corrodedCORROSION RAIL PLATE ON INTERNAL CAVITY OFSS 426, LT WING LE. REPLACED RAIL PLATE IAW SRM 51-10-02, ITEM 9, & SRM 51-40-02.SDR SWAA2026021862663Tie Clip · crackedCRACKED TIE CLIP, BS 277, S10R IN THE PAX CABIN. REPLACED THE TIE CLIP IAW SRM 51-10-02-0G-0, ITEM 9, DWG 141A1110, SHEET 18, REV -, & DWG 141A8380, SHEET 33, REV -.SDR SWAA2026021862658Plate · corrodedCORROSION RAIL PLATE LOC ON INTERNAL CAVITY OFSS 540, LT WING LE. REPLACED THE RAIL PLATE IAW SRW 51-40-02, SRM 51-10-02-0G-0, ITEM 9, & DWG 112A4402, SHEET 40, REV A. PERFORMED VISUAL INSPECTION ON AFFECTED AREA AND NO FOUND DAMAGE.SDR SWAA2026021862661Plate · corrodedCORROSION RAIL PLATE ON INTERNAL CAVITY OFSS 421, LT WING LE. REPLACED THE RAIL PLATE IAW SRM 51-10-02, ITEM 9 DUE TO NO FOUND ALLOWABLE DAMAGE IAW SRM AND INSTALLED FASTENERS IAW SRM 51-40-02.SDR SWAA2026021862662Plate · corrodedCORROSION RAIL PLATE ON INTERNAL CAVITY OFSS 409, LT WING LE. REPLACED RAIL PLATE IAW SRM 51-40-02, & SRM 51-10-02, ITEM 9.SDR SWAA2026021862656Plate · corrodedCORROSION RAIL PLATE, ON INTERNAL CAVITY LEADING EDGE OFSS 573, LT WING. REPLACED THE RAIL PLATE IAW SRM 51-10-02, ITEM 9, & SRM 51-40-02.SDR SWAA2026021862667Nut Plate · corrodedCORROSION RAIL NUT PLATE LOCATED ON INTERNAL CAVITY LEADING EDGE OFSS334 AT LT WING. REPLACED RAIL PLATE LOC INTERNAL CAVITY LEADING EDGE OFSS334 AT LT WING IAW SRM 51-10-02, ITEM 9, DUE TO NOT FOUND ALLOWABLE DAMAGE ON SRM AND INSTALLED FASTENERS IAW SRM 51-SDR SWAA2026021862377Support · corrodedCORRODED SUPPORT ZEE, BS 500C - 500I, LBL 22, WL 156. PERFORMED A PERMANENT REPAIR ON THE SUPPORT ZEE IAW SRM 53-00-53-2R-5, REPAIR 5, & EA M-22-153-01550.SDR SWAA2026021862335Plate · crackedCRACKED SEAL PLATE ACCESS PANEL 431AT ON LT PYLON (1 EA). MEASUREMENT OF CRACK: L: 0.988 INCH. REPLACED THE SEAL PLATE ON ACCESS PANEL 431AT LT PYLON IAW SRM 51-40-02, AND SRM 51-10-02, STEP 9, NO ADDITIONAL DAMAGE.SDR SWAA2026021862336Access Panel · crackedCRACK BLADE ACCESS PANEL 333AT AT LT HORIZONTAL STAB. REPLACED BLADE ACCESS PANEL 333AT AT LT HORIZONTAL STAB IAW SRM 51-10-02, PARAGRAPH 9, SRM 51-40-02. EASUREMENT OF CRACKS: L:0.295 INCHES.SDR SWAA2026021862168Floorbeam · corrodedCORRODED FLOORBEAM, BS 986.5, LBL 44, WL 208.1. PERFORMED A REPAIR ON THE FLOORBEAM IAW SRM 53-70-51-2R-6, REPAIR 6.SDR SWAA2026021862169Floorbeam · corrodedCORRODED FLOORBEAM BS 986.5, RBL 44, WL 208.1. PERFORMED A REPAIR ON THE FLOORBEAM IAW SRM 53-70-51-2R-6, REPAIR 6.SDR SWAA2026021862072Rib · crackedCRACK LEADING EDGE RIB LOCATED LE HSS 105.26, LT HORIZONTAL STAB. REPLACED RIB IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 186A1001, SHEET 19, REV -.SDR SWAA2026021862073Rib · crackedCRACKED ACCESS PANEL 331B RIB LOCATED LE HSS 114.55 AT LT HORIZONTAL STAB. REPLACED THE RIB IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 186A1001, SHEET 19, REV -.SDR SWAA2026021861865Nut · deterioratedDETERIORATED NUT ON THE ASSIST HANDLE LINING, ENTRY DOOR. REPLACED THE NUT IAW AMM 52-11-31-400-802, STEP 3.G (2).SDR SWAA2026021861332Angle · crackedCRACKED ANGLE, BS 500H, S26R. REPLACED THE ANGLE IAW SRM 51-10-02-0G-0, ITEM 9, & DWG 143A7505, SHEET 137, & 138, REV-.SDR SWAA2026021861333Angle · crackedCRACKED ANGLE, BS 500H, S26R. REPLACED THE ANGLE IAW SRM 51-10-02-0G-0, ITEM 9, & DWG 143A7505, SHEET 137, & 138, REV-.SDR SWAA2026021861331Angle · crackedCRACKED GUSSET ANGLE, BS 500I, S21L, IN THE FWD CARGO BAY. REPLACED THE GUSSET ANGLE & FASTENERS IAW SRM 51-40-02-0G, & DWG-143A7902, SHEET 256, REV B.SDR SWAA2026021861448Angle · crackedCRACKED GUSSET ANGLE, 500I, S19R, IN THE FWD CARGO BAY. REPLACED THE GUSSET ANGLE & FASTENERS IAW SRM 51-40-02-0G, & DWG-143A7902, SHEET 256, REV B.SDR SWAA2026021861334Scuff Plate · crackedCRACKED SCUFF PLATE AFT CORNER, IN THE AFT CARGO BAY. REPAIRED THE SCUFF PLATE IAW SRM 53-60-15-2R-1, REPAIR 1; & BAC 5975.SDR SWAA2026021861449Flashlight · inoperativeLAVATORY D FLASHLIGHT INBD INOPERATIVE. REPLACED THE FLASHLIGHT IAW CMM 25-60-02, REV 10, FIGURE 1, ITEM 17, PAGE 10006, & PAGE 10007.SDR SWAA2026021861447Access Panel · crackedCRACKED ACCESS PANEL 191D, LOWER FUSELAGE. REPAIRED THE ACCESS PANEL PANEL 191D IAW SRM 51-70-05-2R-2, REPAIR 2.SDR SWAA2026021860763Light · burned outBURNED OUT OVERWING EXIT LIGHT, ROW 14 RIGHT. REPLACED THE LIGHT IAW AMM 33-21-00-960-805, STEP 10.A. - 10.C.(11), EXCEPT 10.C.(4)(D) AND 10.C.(5)(D). TESTED OK.SDR SWAA2026021860771Light · burned outBURNED OUT OVERWING EXIT LIGHT ROW 14 LEFT. REPLACED THE LIGHT IAW AMM 33-21-00-960-805, STEP 10.A. - 10.C.(11) EXCEPT 10.C.(4)(D) AND 10.C.(5)(D). PERFORMED A TEST, TESTED OK.SDR SWAA2026021860967Lens · brokenBROKEN EMERGENCY LIGHT LENS. REPLACED THE LENS IAW AMM 33-51-03-960-803, STEP 4.D.(1)(2).SDR SWAA2026021860244Nut · deterioratedDETERIORATED NUT ON THE ASSIST HANDLE OF THE AFT SERVICE DOORWAY LINING. REPLACED THE NUT IAW AMM 25-21-25-420-801, STEP 3.B.(5), & SOPM 20-50-01, REV 39.SDR SWAA2025121551189Girt Bar · looseR1 DOOR GIRT BAR FITTINGS LOOSE. TORQUED THE R1 DOOR GIRT BAR FITTINGS IAW AMM 25-66-02-400-801.SDR SWAA2025121249360Battery Pack · inoperativeRIGHT OVERWING LIGHTS INOPERATIVE. R & R IAW AMM 33-51-06-960-805-NG POWER SUPPLY - BATTERY PACK.SDR SWAA2025121244221Battery Pack · inoperativeRIGHT OVERWING LIGHTS INOPERATIVE. R & R IAW AMM 33-51-06-960-805-NG POWER SUPPLY BATTERY PACK.SDR SWAA2025110430668Battery Pack · inoperativeBOTH L/H INTERIOR OVER WING EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK IAW AMM 33-51-06. OPS CHECK GOOD.SDR SWAA2025081100382Transmitter · faultedON APPROACH SELECTED FLAPS 30; FLAP DISPLAYED 15 & 25. WENT AROUND AND SELECTED FLAPS 15; FLAPS DISPLAYED BOTH AT 25 AND STAYED THERE FOR THE REMAINDER OF THE FLIGHT. OVERSPEED FLAPS 25 TO SPEED 193KT MOMENTARILY. LANDED NORMALLY AND ONCE AT THE GATE WITH FLAPSDR SWAA2025032608818Lens · wrong partEMERGENCY EXIT SIGN ARE POINTING IN THE WRONG DIRECTION<[01] RETURNED OVER-WING EMERGENCY EXIT LIGHT LENSES AT LEFT SIDE TO CORRECT POSITION PER SIPSDR SWAA2025022598283Lamp · inoperativeLH OVERWING EXITS; FORWARD AND AFT; EMERGENCY LIGHTS AT DOOR FRAMES HAS SEVERAL BULBS INOP. <[01] RELAMPED L/H OVERWING EXITS; FORWARD AND AFT; EMERGENCY LIGHTS AND PERFORMED A SATISFACTORY TEST OF THE NEW LAMPS IAW AMM 33-51-01-960-801; [02] VERIFIED CORRECTISDR SWAA2025021294858Spring · failedTRAYTABLE ARM STOP FAILED 14D<[01] REPLACED TRAY TABLE ARM PIVOT SPRING AT 14D PER CMM 25-22-46.SDR SWAA2024120273235Handle · brokenFORWARD SERVICE DOOR PLASTIC HANDLE BROKEN.<[01] R+R FWD SERVICE DOOR ASSIST HANDLE PER AMM 52-41-31.SDR SWAA2024061199730Connector · dirtyON APPROACH; WITH FLAPS 30 SELECTED; FLAPS WOULD ONLY GO TO FLAPS 15<[01] CLEANED LEFT FLAP TRANSMITTER ELECTRICAL CONNECTOR AND PERFORMED OPS TEST IAW AMM 27-58-01. OPS TEST GOOD. A/C OK FOR SERVICESDR SWAA2024040369460Battery Pack · inoperativeL/H AFT OVERWING ESCAPE LIGHT AND ESCAPE GROUND LIGHT INOP EMERGENCY BATTERY M1670 LOCATED IN CABIN BEHIND AIR RETURN AT FWD SIDE OF 21ABC<[01] REMOVED AND REPLACED EMERGENCY BATTERY PACK M1670 WITH NEW FROM STOCK. OPS CHECK GOOD.;[02] REMOVED AND REPLACED EMESDR SWAA2024040369461Battery Pack · inoperativeL/H FWD OVERWING ESCAPE LIGHT INOP BATTERY PACK M2335 LOCATED IN CABIN BEHIND AIR RETURN AT 8ABC<[01] REMOVED AND REPLACED EMERGENCY BATTERY PACK M2335 WITH NEW FROM STOCK IAW AMM 33-51-06. OPS CHECK GOOD.;[02] IAW AMM 33-51-06SDR SWAA2024040369458Battery Pack · inoperativeR/H AFT OVERWING ESCAPE LIGHT INOP BATTERY PACK M1671 LOCATED IN CABIN BEHIND AIR RETURN AT 21DEF<[01] REMOVED AND REPLACED EMERGENCY BATTERY PACK M1671 WITH NEW FROM STOCK IAW AMM 33-51-06. OPS CHECK GOOD.;[02] IAW AMM 33-51-06SDR SWAA2024040369459Battery Pack · inoperativeRIGHT FWD OVERWING ESCAPE LIGHT INOP BATTERY PACK M1676 LOCATED IN CABIN BEHIND AIR RETURN AT 8DEF<[01] REMOVED AND REPLACED EMERGENCY BATTERY PACK M1676 WITH NEW FROM STOCK IAW AMM 33-51-06. OPS CHECK GOOD.SDR SWAA2024040368345Angle · crackedLWR ANGLE BEHIND PANEL 141PW CRACKED.<[01] REMOVED AND REPLACED LWR ANGLE BEHIND PANEL 141PW IAW SRM 51-40-02.SDR SWAA2024040366344Strip · corroded4 EA. FWD CARGO CAP STRIPS HAVE MULTIPLE AREAS OF CORROSION ON LOWER SURFACE (MARKED)<[01] PARTS DATA UPDATE ONLY;[02] INSTALLED NEW FWD CARGO CAP STRIPS PER AMM 25-52-06;[03] REMOVED AND REPLACED 4 EA. FWD CARGO CAP STRIPS IAW AMM 25-52-10.;[04] VERIFIED REMOSDR SWAA2024040365610Skin · delaminatedRH OTBD AFT FLAP INBD LOWER SURFACE HAS DELAMINATION.<[01] REMOVED RIGHT WING O/B T/E FLAP ASSY PER AMM 27-51-22;[02] OK TO INSTALL AFT FLAP.;[03] INSTALLED NEW AFT FLAP IN REF TO AMM 27-51-22;[04] INSPECTION C/W FOR CA #3;[05] DUE TO FAILED RIG CHECK REMOVED SDR SWAA2024040364051Web · cracked#1ENG. INBD.COWL;PNL. 414; WEB SUPPORT ATTACHMENT AT OIL SERV. DOOR OPENING CRACKED.<[01] REMOVED AND REPLACED WEB PER CMM 71-13-30.;[02] INSPECTED CA #1SDR SWAA2024040363648Panel · deformedFLIGHT DECK PANEL 211AF DEFORMED<[01] LOCATED; DRILLED AND DEBURRED REPLACEMENT PANEL PER SRM 51-40-05.;[02] LOCATED; DRILLED AND DEBURRED REPLACEMENT PANEL PER SRM 51-40-05.;[03] REPAIR COMPLETED AND PANEL INSTALLED ON NON ROUTINE TTG8Q00S4P95 AND EA M21-153-SDR SWAA2024040363100Angle · crackedL/H WING OUTBD UPPER FIXED T/E PANEL BULB SEAL WEB CLIP THAT ATTACHES TO DEFLECTION CONTROL RIB CRACKED AT LOWER FASTENER ( PHOTO ATTACHED )<[01] INSTALLED NEW CLIP ANGLE WITH FASTENERS PER SRM 51-40-02.;[02] INSTALLED NEW CLIP ANGLE WITH FASTENERS PER SRM 51-SDR SWAA2023091198275Flap · delaminatedLEFT HAND OUTBOARD AFT FLAP UPPER SURFACE INBOARD END DELAMINATED<[01] C/W;[02] REMOVED AND REPLACED AFT O/B L/H AFT FLAP. PER AMM 27-51-22;[03] COMPLIED WITH REMOVAL AND REPLACEMENT OF AFT O/B L/H AFT FLAP. PER AMM 27-51-22
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