N8673F
Service difficulty reports · 127
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 = 'N8673F' 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 = 'N8673F' 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 SWAA2023112014274Tail Cone · delaminatedTAIL CONE HAS MULTIPLE DELAMINATED DENTS BETWEEN MULTIPLE COMPOSITE REPAIRS ON UPPER ON L/H SURFACES<[01] REMOVED DAMAGE IN AREAS OF DENTS MARKED PER SRM 51-70-5-05. REPAIR 1;[02] INSPECTED WORK PERFORMED ON C/A #1;[03] POTTED CORE ON AFFECTED REPAIR AREAS PR SDR SWAA2023112013956Angle · corrodedON THE FWD ENTRY DOOR LOWER THRESHOLD STRUCTURE; THE INNER 'Z' ANGLE HAS AREAS OF CORROSION.<[01] REMOVED CORROSION; FOUND OUT OF LIMITS PER SRM 53-10-51-1A-1;[02] VERIFIED REMOVED CORROSION; FOUND OUT OF LIMITS PER SRM 53-10-51-1A-1.;[03] DRILLED NEW Z ANGLE SDR SWAA2023112014276Fitting · corrodedLAV FITTING AT STA 947: 52 RBL HAS CORROSION UNDER FITTING. (M)<[01] REMOVED DAMAGE I.A.W SRM 51-10-02. MEASURED DAMAGE DEPTH TO BE .062 INCHES. DAMAGE FOUND TO BE OUT OF ALLOWABLE LIMITS AS GIVEN IN SRM 53-70-51-1A-1.;[02] REMOVED GALLEY FITTING I.A.W SRM 51-SDR SWAA2023112014411Shield · corrodedAFT CARGO STA. 847-867; CORROSION AROUND NUT-PLATE HOLES ON RT TRANSITION ANGLE.<[01] REMOVED CORROSION PER SRM 53-60-15-1A-1.;[02] REMOVED CORROSION FROM AREA PER SRM 53-60-15-1A-1 (REMAINING THICKNESS 0.045'). SHIELD/TRANSITION ANGLE IS OUT OF LIMITS PER<BR>SDR SWAA2023112013816Plate · crackedAFT CARGO THRESHOLD AFT CORNER PLATE CRACKED.<[01] AFT CARGO THRESHOLD AFT CORNER PLATE WAS REMOVED AND REPLACED ON FAULT # TTG8Q00P8ZTG.;[02] AFT CARGO THRESHOLD AFT CORNER PLATE WAS REMOVED AND REPLACED ON FAULT # TTG8Q00P8ZTG. C/W INSPECTIONSDR SWAA2023112013478Door Latch · corrodedSTABILIZER TRIM ACCESS DOOR LATCH MECHANISM HARDWARE/COMPONENTS HAS CORROSION.<[01] REMOVED AND REPLACED STABILIZER TRIM ACCESS DOOR 311BL LATCH MECHANISM REF SRM 51-40-02; AND AMM 52-41-11.;[02] CORRECTION: REMOVED AND REPLACED STABILIZER TRIM ACCESS DOOR 311SDR SWAA2023112013134Access Door · delaminatedPANEL 333FB DOOR ASSY - LOWER T/E - LEFT HORIZONTAL STABILIZER - LH LOWER. IB END HAS FIBERGLASS DAMAGE AND DELAMINATION.<[01] REMOVED DAMAGE PER SRM 55-10-01-1A-3;[02] REPAIRED PER SRM 55-10-01. SRM 51-70-08.;[03] INSPECTED WORK PERFORMEDSDR SWAA2023112015757Flap · delaminatedR/H O/B AFT FLAP IS DELAMINATED ON I/B AFT CORNER<[01] REMOVED R/H O/B AFT FLAP PER AMM 27-51-21.;[02] OK TO INSTALL RH O/B AFT FLAP;[03] VERIFIED CORRECTIVE ACTION #2. RII INSPECTION C/W. OK TO INSTALL SERVICEABLE FLAP.;[04] INSTALLED R/H OTBD AFT FLAP IAW AMSDR SWAA2023090596329Fairing · crackedCRACK; #2 ENGINE PYLON AFT STRUT SUPPORT FAIRING ASSY<[01] REMOVED PYLON STRUT AFT FAIRING IAW SRM 51-40-02.;[02] INSTALLED NEW PYLON STRUT AFT FAIRING FITTING PER SRM 51-40-02 AND SRM 51-10-02SDR SWAA2023071879019Battery Pack · inoperativeLH OVERWING FWD EMERGENCY LIGHT AND RH OVERWING AFT EMERGENCY LIGHT INOP<[01] PART REMOVAL;[02] PART INSTALL;[03] R&R?D EMERGENCY LIGHT POWER SUPPLY BATTERY PACKS M2335 & M1671 IAW AMM 3-51-06. OPS CHECK GOOD @ THIS TIME.SDR SWAA2023071779067Cover · missingMID CABIN OVERWING EXIT PLACARD MISSING<[01] REINSTALLED OVERWING EXIT SIGN LENS COVER PER SIPSDR SWAA2023040723820Battery Pack · inoperativeTOTAL OF FIVE EMERGENCY LIGHTS INOP. TWO INTERNAL L2 DOOR LIGHTS AND THE L2 EXTERIOR. ONE CABIN IDENTIFIER AT 27ABC AND ONE ATTACHED TO THE AFT L/H WINDSCREEN BY LAVATORY DOOR.<[01] REPLACED THE AFT GALLEY L/H BATTERY PACK (M1673) PER <BR>AMM 33-51-06. ALL LIGSDR SWAA2023021000316Wedge · cracked#2 ENGINE AFT PYLON TE WEDGE CRACKED ON FWD WEB MEASURING 1 AND EXTENDING BEYOND RADIUS<[01] ACCOMPLISHED EA 23-154-00430.SDR SWAA2022122885305Slide · out of adjustFWD ENTRY SLIDE OUT OF ADJUSTMENT. ADJUSTED THE FWD ENTRY SLIDE IAW AMM 25-66-01SDR SWAA2022121582009Lens · missingAISLE EMERGENCY EXIT LIGHT COVER LENS MISSING MID CABIN. LIGHT CONSIDERED INOPER AISLE EMERGENCY EXIT LIGHT COVER LENS MISSING MID CABIN. LIGHT CONSIDERED INOPERATIVE. REPLACED MISSING EXIT SIGN LENS COVER IN REF TO AMM 33-51-01. EMERGENCY LIGHTS OPS TEST GOSDR SWAA2022071427581Flap · delaminatedDURING WAC FOUND DAMAGE ON INBOARD OF R/H OUTBOARD TRAILING EDGE FLAPS LOWER SKIN DELAMINATION AREA = L: 22.000' W: 10.000' FROM THE LOWER I/B CORNER.MISSING MATERIAL = L: 3.500' W: 2.000' FROM THE LOWER I/B CORNER. SEE ATTACHED IMAGES. / [01] MEASUREMENTS ADDSDR SWAA2022062420519Battery Pack · inoperativeFWD ENTRY DOOR EMERGENCY LIGHTS INOP / [01] REMOVED AND REPLACED POWER SUPPLY M1675 AND THE BATTERY PACK PER AMM 33-51-06 OPS CHECK GOODSDR SWAA2022060815008Light · inoperativeSLIDE / OVERWING EMERGENCY EXIT LIGHT AFT OF L2 DOOR INOP / [01] RELAMPED PER 737 AMM 33-51-04.SDR SWAA2021123055826Skin · crackedEXTERNAL POWER DOOR CUTOUT FRAME SKIN CRACKED AND BROKEN AT LOWER LATCH BLOCK ; / [01] VERIFIED MATERIAL; -2 DOUBLER 2024 T3 .050' ATAG A34144; -3 FILLER 2024-T3 .040' ATAG A12631 IAW SRM 53-10-15-2R-4 TABLE 201.; [02] VERIFIED STEP 1; [03] CUT AND REMOVED DAMSDR SWAA2021122253535Angle · crackedA-24-9 MID CABIN FLOOR PANEL SUPPORT ANGLE CRACKED AT STATION 540 LBL 2. ; / [01] RECEIVED NEW PART 143A5240-35 A-TAG WN11950; LOCATED AND DRILLED; DEBURRED HOLES IAW SRM 51-40-05-0G.; [02] VERIFIED STEP 1 AND OK TO INSTALL; [03] REMOVED AND REPLACED SUPPORT ASDR SWAA2021122253537Angle · crackedA-24-10 MID CABIN FLOOR PANEL SUPPORT ANGLE AT STATION 540 RBL 2 CRACKED. ; / [01] RECEIVED. NEW PART 143A5240-36; A-TAG WN11946; LOCATED AND DRILLED; DEBURRED HOLES IAW SRM 51-40-05-0G.; [02] VERIFIED STEP 1 AND OK TO INSTALL; [03] REMOVED AND REPLACED SUPPORSDR SWAA2021122252016Battery Pack · inoperativeEMERGENCY EXIT LIGHTS CONTROLLED BY BATTERY PACK M01672 ARE INOP ; / [01] REPLACED BATTERY PACK AT M1672 IAW AMM 33-51-06-960-805 OP TEST GOOD<BR>WORK PERFORMED BY EMP#18130; [02] VERIFIED STEP 1; [03] AUDITEDSDR SWAA2022010451815Skin · delaminatedL/H WING O/B AFT FLAP AREA OF DELAM ON UPPER SURFACE 78.5' O/B OF I/B EDGE AND 2' FWD OF AFT EDGE ; / [01] BOND TEST IAW B737 NDT PART 4; 51-00-05. DISBOND AREA MARKED IN BLACK. TOOL#40082; DUE 11OCT22; [02] EVALUATED AND FOUND DELAM 1/2 INCH DIAMETER AND REPASDR SWAA2021122251688Angle · out of toleranceFWD PIT LH ZEE ANGLE STA. 500H THRU 500I WAS FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 AND REQUIRES REPAIR. ; / [01] REF. FAULT TTG8Q009PLKJ STEP 3. ?UT IAW B737 NDT PART 4 51-00-00 PROCEDURE 2. ORIGINAL .040'; REMAINING AT STA 500H+17 IS .029'; .011' LOSDR SWAA2021122251447Support · corrodedAFT PIT CORROSION AT BS 947 ON AFT BULKHEAD FLOOR SUPPORT; RBL 17 WL179 DOT 45 ; / [01] BLENDED CORROSION BY HAND RUBBING IAW SRM 51-10-02; [02] VERIFIED STEP 1; [03] DUE TO NO TECH DATA FLOOR SUPPORT WAS FOUND TO BE OUT OF LIMITS; [04] VERIFIED STEP 3; [05] VSDR SWAA2022011451427Floor Panel · corrodedDOT#29-186 AFT PIT FLOOR PANEL 140DF CORRODED ; / [01] VERIFIED LIMITS ON AFT PIT FLOOR PANEL 140DF. CORROSION EXCEEDS 20' MAX ALLOWED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-1..; [02] VERIFIED MATERIAL FOR REPLACEMENT FLOOR PANEL TO BE .071; 2024-T3; ISDR SWAA2022010451098None · crackedA113-08 R/H A/C BAY CENTER TANK STA 663; RBL 33.8; LOWER CHORD IS CRACKED. ; / [01] REMOVED VERTICAL STIFFENER AT RBL 45 IAW SRM 51-40-02.; [02] REMOVED U CHANNEL BS 663 RBL 45 TO RBL 70 IAW SRM 51-40-02.; [03] STARTED REMOVING FASTENERS C/T FUEL TANK. IAW SRMSDR SWAA2022010450942Support Fitting · cracked#6 FLAP SUPPORT FITTING CRACKED. DOT#A193-1 ; / [01] REMOVED #6 I/B FLAP TRANSMISSION ATTACH FITTING IAW AMM 27-51-31-000-801 STEP 2.E.(5).(B) & AMM 27-51-15-000-801 STEP 2.F.(5).; [02] LINED REAMED #6 FLAP TRANSMISSION INBOARD SUPPORT FITTING IAW BOEING CMM 5SDR SWAA2021123051431Strip · corrodedDOT#40-186 AFT PIT R4 CAP STRIP CORRODED ; / [01] REMOVED CORROSION FROM CAPSTRIP R4.; [02] VERIFIED STEP 1; [03] MEASURED AND VERIFIED MATERIAL LOSS USING AAR TOOL # 1714 DUE 10/11/22 FOUND OUT OF LIMITS DUE NO LIMITS REFERENCE FOUND. ORIG. T OF CAPSTRIP 0.06SDR SWAA2021123051432Strip · corrodedDOT#41-186 AFT PIT R2 CAP STRIP CORRODED ; / [01] REMOVED CORROSION FROM CAPSTRIP R2; [02] VERIFIED STEP 1; [03] MEASURED AND VERIFIED MATERIAL LOSS USING AAR TOOL # 1714 DUE 10/11/22 FOUND OUT OF LIMITS DUE NO LIMITS REFERENCE FOUND. ORIG. T OF CAPSTRIP 0.063SDR SWAA2021123051433Strip · corrodedDOT#43-186 AFT PIT L4 CAP STRIP CORRODED ; / [01] REMOVED CORROSION FROM CAPSTRIP L4; [02] VERIFIED STEP 1; [03] MEASURED AND VERIFIED MATERIAL LOSS USING AAR TOOL # 1714 DUE 10/11/22 FOUND OUT OF LIMITS DUE NO LIMITS REFERENCE FOUND. ORIG. T OF CAPSTRIP 0.063SDR SWAA2021123051435Strip · corrodedDOT#42-186 AFT PIT R1 CAP STRIP CORRODED ; / [01] REMOVED CORROSION FROM CAPSTRIP R1.; [02] REMOVED CORROSION FROM CAPSTRIP R1; [03] VERIFIED STEP 1-2; [04] MEASURED AND VERIFIED MATERIAL LOSS USING AAR TOOL # 1714 DUE 10/11/22 FOUND OUT OF LIMITS DUE NO LIMITSDR SWAA2021123051436Strip · corrodedDOT#44-186 AFT PIT L3 CAP STRIP CORRODED ; / [01] REMOVED CORROSION FROM CAPSTRIP L3; [02] VERIFIED STEP 1; [03] MEASURED AND VERIFIED MATERIAL LOSS USING AAR TOOL # 1714 DUE 10/11/22 FOUND OUT OF LIMITS DUE NO LIMITS REFERENCE FOUND. ORIG. T OF CAPSTRIP 0.063SDR SWAA2021123051095Strip · corrodedDOT#19-186 FWD PIT LH-2 CAP STRIP CORRODED ; / [01] REMOVED CORROSION FROML/H CAP STRIP 2 IAW SRM 51-10-02-OG-0; [02] MEASURED AND VERIFIED MATERIAL LOSS USING AAR TOOL # 1714 DUE 10/11/22 FOUND OUT OF LIMITS DUE NO LIMITS REFERENCE FOUND. ORIG. T OF CAPSTRIP SDR SWAA2021123051094Strip · corrodedDOT#17-186 FWD PIT RH-2 CAP STRIP CORRODED ; / [01] REMOVED. CORROSION FROM R/H -2 CAP STRIP. IAW SRM 51-10-02-OG-0; [02] MEASURED AND VERIFIED MATERIAL LOSS USING AAR TOOL # 1714 DUE 10/11/22 FOUND OUT OF LIMITS DUE NO LIMITS REFERENCE FOUND. ORIG. T OF CAPSTSDR SWAA2021123051100Strip · corrodedDOT#18-186 FWD PIT RH-3 CAP STRIP CORRODED ; / [01] REMOVED. CORROSION FROM R/H-3 CAP STRIP IAW SRM 51-10-02-OG-0; [02] MEASURED AND VERIFIED MATERIAL LOSS USING AAR TOOL # 1714 DUE 10/11/22 FOUND OUT OF LIMITS DUE NO LIMITS REFERENCE FOUND. ORIG. T OF CAPSTRISDR SWAA2021123051101Strip · corrodedDOT#20-186 FWD PIT LH-3 CAP STRIP CORRODED ; / [01] REMOVED CORROSION FROM L/H-3 CAP STRIP IAW SRM 51-10-02-OG-0; [02] MEASURED AND VERIFIED MATERIAL LOSS USING AAR TOOL # 1714 DUE 10/11/22 FOUND OUT OF LIMITS DUE NO LIMITS REFERENCE FOUND. ORIG. T OF CAPSTRIPSDR SWAA2021123051102Strip · corrodedDOT#21-186 FWD PIT LH-4 CAP STRIP CORRODED ; / [01] REMOVED CORROSION FROM L/H-4 IAW SRM 51-10-02-OG-0; [02] MEASURED AND VERIFIED MATERIAL LOSS USING AAR TOOL # 1714 DUE 10/11/22 FOUND OUT OF LIMITS DUE NO LIMITS REFERENCE FOUND. ORIG. T OF CAPSTRIP 0.063 ; LSDR SWAA2021122251434Strip · corrodedDOT#45-186 AFT PIT L2 CAP STRIP CORRODED ; / [01] REMOVED CORROSION FROM CAPSTRIP L2; [02] VERIFIED STEP 1; [03] MEASURED AND VERIFIED MATERIAL LOSS USING AAR TOOL # 1714 DUE 10/11/22 FOUND OUT OF LIMITS DUE NO LIMITS REFERENCE FOUND. ORIG. T OF CAPSTRIP 0.063SDR SWAA2021122251423Floor Panel · corrodedDOT#31-186 AFT PIT FLOOR PANEL 140CF CORRODED ; / [01] EVALUATED FLOOR PANEL 140CF AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-1 EXCEEDS THE 20' MAXIMUM FOR CORROSION; [02] VERIFIED CORRECT MATERIAL 2024-T3 .071' CLAD IAW AMM 25-52-01-201-801 A-TAG #A104SDR SWAA2021122251426Floor Panel · corrodedDOT#28-186 AFT PIT FLOOR PANEL 140AF CORRODED ; / [01] VERIFIED MATERIAL ID FOR FLOOR PANEL 140AF 2024 T3 .071 TAG# A03994 IAW AMM 25-52-01-201-801; [02] VERIFIED STEP 1; [03] VERIFIED ITEMS 1 AND 2; [04] OUT OF SEQUENCE: EVALUATED CORROSION AND IS MORE 20' FOSDR SWAA2021122251421Floor Panel · corrodedDOT#30-186 AFT PIT FLOOR PANEL 140EF CORRODED ; / [01] EVALUATED DAMAGE; FOUND TO EXCEED LIMITS PROVIDED IN SRM 53-00-53-1A-1 FIG.102; [02] VERIFIED MATERIAL FOR NEW FLOOR PANEL AS 2024-T3 .071' A TAG A104326 IAW AMM 25-52-01-201-801; [03] VERIFIED STEPS 1 & 2SDR SWAA2021122251090Strap · corrodedPANEL 192CR; R/H A/C BAY ACCESS DOOR; DOOR FWD I/B HINGE FITTING GROUND STRAP HAS CORROSION AT HINGE ATTACH BOLT ON DOOR. DOT: 148-006 ; / [01] REMOVED HINGE FROM PANEL#194CR A/C BAY ACCESS DOOR FORWARD INBD HINGE I/A/W SRM 51-40-02-0G-0. VERIFIED NEW PART # 1SDR SWAA2021122251089Angle · corrodedA-061 DOT 021 FWD CARGO PIT CORROSION ON R/H Z ANGLE FROM STA 500A TO STA 500H +15' RBL 23 W/L 155 ; / [01] REMOVED CORROSION FROM FWD CARGO RH ZEE ANGLE BS 500A -500I AND VERIFIED WITH 10X MAG GLASS. ORIGINAL T= .040' LOSS OF .18' REMAINING .022' FOUND TO BE SDR SWAA2021122251424Floor Panel · corrodedDOT#33-186 AFT PIT PANEL BREAK ATTACHED TO FLOOR PANEL 140BF CORRODED ; / [01] VERIFIED AND REPLACED AFT CARGO FLOOR PANEL SPLICE STRAP ON PANEL 140BF ON PARTS RACK IAW BOEING DWG# 146A7500 ID:0233 REV:- P/N 146A9401-8 ATAG A105405; [02] VERIFIED STEP 1<BR>INSSDR SWAA2021122251429Floor Panel · corrodedDOT#32-186 AFT PIT FLOOR PANEL 140BF CORRODED ; / [01] VERIFIED LIMITS. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-1. EXCEEDS 20' MAX ALLOWED.; [02] VERIFIED MATERIAL FOR AFT PIT REPLACEMENT FLOOR PANEL 140BF AS .071; 2024 T-3. IAW AMM 25-52-01-201-801.; [0SDR SWAA2021122251087Attach Angle · corrodedA-061 DOT 020 FWD CARGO PIT CORROSION ON FLOOR SUPPORT ATTACH ANGLE STA 500I RBL 23 TO LBL 23 W/L 155 ; / [01] REMOVED CORROSIONFROM AFT BULKHEAD LOWER SUPPORT RAIL AT BS 500I. ORIGINAL T= .071' LOSS OF .027' REMAINING .044' FOUND TO BE OUT OF LIMITS IAW SRM53SDR SWAA2021122252603Tie Down · corrodedDOT#38-186 AFT PIT AFT TIE DOWN CORRODED ; / [01] VERIFIED AND REPLACED AFT CARGO COMPARTMENT AFT TIEDOWN PLATE ON PARTS RACK IAW BOEING DWG#453A2600 ID:0093 REV:A <BR>P/N 453A2611-2 ATAG A85405; [02] VERIFIED STEP 1<BR>INSP C/W<BR>AUDIT C/WSDR SWAA2021122252604Tie Down · corrodedDOT#39-186 AFT PIT FWD TIE DOWN CORRODED ; / [01] VERIFIED AND REPLACED AFT CARGO COMPARTMENT FWD TIEDOWN PLATE ON PARTS RACK IAW BOEING DWG#453A2600 ID:0093 REV:A <BR>P/N 453A2611-1 ATAG E72774; [02] VERIFIED STEP 1<BR>INSP C/W<BR>AUDISDR SWAA2021122251093Structure · crackedLT A/C BAY, BS 663, LBL 9.5; LOWER CHORD IS CRACKED. REMOVED DAMAGED SECTION IAW SRM 57-10-10-2R-5. REPLACEMENT ANGLE FABRICATED & -2 SPLICE ANGLE FABRICATED IAW SRM 57-10-10-2R-5. PERFORMED DETAILED INSP OF REPAIR AREA AND UNDERLYING STRUCTURE, NO DEFECTS
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