N8629A
Service difficulty reports · 174
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 = 'N8629A' 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 = 'N8629A' 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 SWAA2022052606751Skin · crackedFWD SERVICE DOOR INBOARD UPPER SKIN FWD UPPER ACCESS HOLE SKIN CRACKED. / [01] REPAIRED IAW EA 22-152-01431; REFER TO EACH STEP'S FOR WORK PERFORMED.;[02] INSPECTED WORK PERFORMEDSDR SWAA2022052603001Scuff Plate · crackedFWD CARGO AFT THRESHOLD CORNER CRACKED. / [01] INSTALLED NEW AFT SCUFF PLATE FOR THE FWD CARGO PER AMM 53-11-02SDR SWAA2022052603000Threshold · crackedAFT CARGO FWD THRESHOLD CORNER CRACKED. / [01] OK TO INSTALL PART;[02] REMOVED AND REPLACED PER SRM 51-10-02 AND AMM 53-11-02;[03] INSPECTED WORK PERFORMEDSDR SWAA2022052600839Angle · crackedAFT CARGO STA. 867; LAV. TANK POST HAS CRACKED ANGLE ON INSIDE STRUCTURE. / [01] REMOVED AND REPLACED ANGLE PER SRM 51-40-02 AND 51-10-02.;[02] C/W INSPECTIONSDR SWAA2022052600830Support · corrodedFLOOR SUPPORT HAS CORROSION AT STA. 946 LBL. 24.0 AFT WET AREA. / [01] FLOOR SUPPORT ANGLE IS OUT OF LIMITS PER SRM 53-70-51-1A-1.;[02] REMOVED AND REPLACED FLOOR SUPPORT ANGLE PER SRM 51-40-02. PART NUMBER OF NEW ANGLE IS 147A5430-7;[03] VERIFIED REPLACEMENT SDR SWAA2022052600598Angle · corrodedCORROSION ON R/H TRANSITION ANGLE UPPER SURFACE AROUND NUT PLATE HOLES BS 500A TO BS 500D. / [01] REMOVED DAMAGE I.A.W SRM 51-10-02. MEASURED DAMAGE DEPTH TO BE .008 INCHES. DAMAGE FOUND TO BE BEYOND ALLOWABLE DAMAGE LIMITS AS GIVEN IN SRM 53-00-53-1A-2.;[09] SDR SWAA2022052600599Angle · corrodedCORROSION ON L/H TRANSITION ANGLE UPPER SURFACE AROUND NUT PLATE HOLES BS 500A TO BS 500F.REMOVED DAMAGE I.A.W SRM 51-10-02. MEASURED DAMAGE DEPTH TO BE .014 INCHES. DAMAGE FOUND TO BE BEYOND ALLOWABLE DAMAGE LIMITS AS GIVEN IN SRM 53-00-53-1A-2.CUT AND REMOVESDR SWAA2022052600833Track · corrodedAFT CARGO STA. 792 RBL 14 CORROSION AROUND FLOOR CHANNEL NUT-PLATE HOLE. AFT CARGO FLOOR CHANNEL (TRACK) IS OUT OF LIMITS PER SRM 53-00-53-1A-2. REMOVED FASTENERS FROM FLOOR CHANNEL FROM B.S 767-887 I.A.W SRM 51-40-02. CUT FLOOR CHANNEL AT B.S 747+8 I.A.W SRM SDR SWAA2022052600836Web · corrodedAFT CARGO THRESHOLD WEB STA. 792-847; CORROSION AROUND NUT-PLATE HOLES. / [01] COMPLIED WITH MEASUREMENTS.;[02] THRESHOLD CARGO WEB IS OUT OF LIMITS PER SRM 53-60-15-1A-1.;[03] REMOVED WEB PER SRM 51-40-02.;[04] INSPECTED WORK PERFORMED ON C/A #2;[05] DRILLED SDR SWAA2022052600834Angle · corrodedAFT SERVICE DOOR FLOOR DRAIN SUPPORT ANGLE HAS CORROSION F.S. 947 TO 967. / [01] SUPPORT ANGLE (MACHINED INTERCOSTAL) IS OUT OF LIMITS PER SRM 53-70-51-1A-1.;[02] REMOVED SUPPORT ANGLE AND DRILLED NEW SUPPORT ANGLE 147A5660U22 PER SRM 51-40-02 AND 51-10-02. OKSDR SWAA2022052600844Beam · corrodedAFT ENTRY DOOR FLOOR SUPPORT BEAM HAS CORROSION AT F.S. 947 LBL 50.0 AT THE FORWARD FLOOR DRAIN SUPPORT BEAM. / [01] SUPPORT BEAM (MACHINED INTERCOSTAL) IS OUT OF LIMITS PER SRM 53-70-51-1A-1.;[02] REMOVED OLD SUPPORT BEAM FROM STA 947-967 AT LBL 50 AND DRILLESDR SWAA2022052600605Skin · crackedHFEC INDICATION OF A CRACK IN R/H WING LEADING SKIN FASTENER COUNTERSINK AT THE 11TH HOLE INBOARD OF THE ENGINE PYLON. CRACK INDICATION REMAINED AFTER OVERSIZING HOLE TO .247 INCHES. / [01] ATTACHED PHOTO OF HOLE;[02] REPAIR ACCOMPLISHED PER EA 22-157-01278-WISDR SWAA2022052600245Threshold · crackedAFT CARGO AFT THRESHOLD CORNER CRACKED. / [01] OK TO INSTALL PART;[02] REMOVED AND REPLACED PER SRM 51-10-02 AND AMM 53-11-02;[03] INSPECTED WORK PERFORMEDSDR SWAA2022052600261Scuff Plate · crackedFWD CARGO FWD THRESHOLD CRACKED / [01] INSTALLED NEW FWD SCUFF PLATE PER AMM 53-11-02SDR SWAA2022052400254Floor Panel · corrodedFWD GALLEY FLOOR PANEL 221BF HAS CORRODED INSERTS. / [01] REMOVED AND REPLACED FWD GALLEY FLOOR PANEL 221BF PER AMM 53-21-00.;[02] VERIFIEDSDR SWAA2022031883467Light · inoperativeEMERGENCY LIGHT AFT OF RH WING INOP / [01] RELAMPED EMERGENCY LIGHT AFT OF RH WING PER AMM 33-51-04. OPS CHECK GOOD.SDR SWAA2021112947921Light · inoperativeAFT L/H AISLE EMERGENCY LIGHTS ABOVE AISLE INOP ; / [01] REMOVED AND REPLACED BATTERY PACK @ ROW 20ABC IAW AMM 33-51-06; OPS CHECK GOOD. MEL CLEARED; PLACARDS REMOVED.SDR SWAA2021111542301Sign · inoperativeAFT GALLEY EMERGENCY EXIT SIGN INOP. R&R AFT BATTERY PACK PER AMM 33-51-06-960-805.SDR SWAA2021111542300Light · inoperativeFWD GALLEY EMERGENCY EXIT SIGN INOP. R&R AFT BATTERY PACK PER AMM 33-51-06-960-805.SDR SWAA2021111542299Light · inoperativeAFT PAX INTERIOR EMERGENCY SIGN INOP. R&R AFT BATTERY PACK PER AMM 33-51-06-960-805.SDR SWAA2021111542298Light · inoperativeFWD PAX DOOR INTERIOR EMERGENCY EXIT SIGN INOP. R&R AFT BATTERY PACK PER AMM 33-51-06-960-805.SDR SWAA2021051773133Lamp · inoperativeDURING ACCOMPLISHMENT OF MT 733-010-00-01 OPS EMERG LIGHTS FOUND L/H AFT OF FLAPS AND AFT ENTRY DOOR EXTERNAL EMERG LIGHTS INOP / RELAMPED L/H AFT OF FLAPS AND AFT ENTRY DOOR EXT. EMERG LIGHTS PER AMM 33-51-04SDR SWAA2021040159440Light · inoperative*** DELAY ONLY ***WORKING ON CENTER AISLE EXIT ON ON MX NOTE / NEW LIGHT ASSYSDR SWAA2020081107352Megaphone · brokenAFT MEGAPHONE WAS BROKEN. R & R THE AFT MEGAPHONE IAW AMM 25-64-00SDR SWAA2021082745022Bracket · crackedRH WING; LWR INBOARD FIXED TRAILING EDGE PANEL 651FB FWD SEAL RETAINER HAS CRACKED ANGLE BRACKET / REMOVED AND REPLACED ANGLE BRACKET P/N 287A9152-24; ON FWD SEAL RETAINER OF RH WING PANEL 651FB IAW SRM 51-40-02-0G-0 AND BOEING DWG. 115A2710 REV. -. A-TAG # DFSDR SWAA2020050545018Intercostal · corrodedAFT CARGO COMPARTMENT STA 747 TO STA 767 RBL 20 WL 156 INTERCOSTAL HAS AREA OF CORROSION / REMOVED INTERCOSTAL AT AFT CARGO COMPARTMENT STA 727-767 RBL 20 WL 156 REMOVED CORROSION; CORROSION LOSS FOUND OUT OF LIMITS; VERIFIED NEW MATERIALS; FABRICATED NEW INTESDR SWAA2021082544283Floor Support · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTUR RBL 24; WL 156; STA 767 CLIP COMMON TO SHIELD AND FRAME HAS CORROSION ON LOWER SURFACE; MARKED. / REMOVED DAMAGE CLIP COMMON TO SHIELD AND FLAME DUE NO ALLOWABLE DAMAGE LIMITS FOUND IN THE SRM IDENTIFIED LOCATED INSTALLED NSDR SWAA2021081744258Angle · crackedLH WING AFT T/E PANEL INBD 551 FB HAS CRACKED L BRACKET 26' INBD FROM OTBD END FWD SIDE. / REMOVED AND REPLACED L BRACKET 26' INBD FROM OTBD AND FWD SIDE ON PANEL 551FB IAW SRM 51-40-02-0G-0 AND BOEING DWG 115A2710 ATAG A50875 P/N 287A9152-23SDR SWAA2021080544250Floor Panel · corrodedAFT PIT FLOOR PANEL 140 DF HAS CORROSION AT PERIMETER EDGES. / AFT PIT FLOOR PANEL 140DF HAS CORROSION AT PREMETER GOUGES. FABRICATED NEW FLOOR PANEL 140DF IAW B737 AMM 25-52-01-201-801. AND BOEING DWG 453A2610 REV B P/N 2024-T3-071 ATAG A48963SDR SWAA2021080544248Floor Panel · corrodedAFT PIT FLOOR PANEL 140 EF HAS CORROSION AT PERIMETER EDGES. / FABRICATED & PRIMED AFT PIT FLOOR PANEL 140 EF IAW AMM 25-52-01-201-801 & AMM 51-21-72-370-804. A48964.SDR SWAA2021080544249Floor Panel · corrodedAFT PIT FLOOR PANEL 140 AF HAS CORROSION AT PERIMETER EDGES. / EVALUATED CORROSION ON R/H SIDE OF AFT CARGO PANEL 140AF FOUND 50' BY 1' OF CORROSION ALLOWED 20' OUT OF LIMITS PER 737-800 SRM 53-00-53-1A-1 FIG 102 FABRICATED PANEL 140AF I/A/W 737 AMM 25-52-01-2SDR SWAA2021080544247Floor Panel · corrodedAFT PIT FLOOR PANEL 140 BF HAS CORROSION AT PERIMETER EDGES. / FABRICATED & RPIMED PANEL 140 BF IAW AMM 25-52-01-201-801 AND AMM 51-21-72-370-804. A48959.SDR SWAA2021080544246Floor Panel · corrodedAFT PIT FLOOR PANEL 140 CF HAS CORROSION AT PERIMETER EDGES. / AFT PIT FLOOR PANEL 140CF HAS CORROSION AT PEREMETER EDGES. FABRICATED NEW FLOOR PANEL 140CF IAW B737 AMM 25-52-01-201-801 AND B737 DWG 453A2610 REV C. ATAG A48967SDR SWAA2021072744369Angle · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE FLOOR PANEL TRANSITION STRIP AT LBL 6; WL 166; STA 887 HAS CORROSION ON UPPER SURFACE; MARKED. / EVALUATED AND REPLACED AFT CARGO FLOOR STRUCTURE FLOOR PNL TRANSITION STRIP AT LBL6 AND WL166 STA 887 IAW BOEING DWG 147A7500SDR SWAA2021060844281Shield · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE SHIELD RBL 20; WL 156; STA 767 TO 787 HAS CORROSION ON UPPER AND LOWER SURFACES; MARKED. / REMOVED CORROSION FROM AFT CARGO COMPARTMENT FLOOR STRUC FLOOR SHIELD. VERIFIED MATERIAL LOSS: ORIG 'T' 0.050' LOSS 0.021' REMAIN 0SDR SWAA2020050544375Floor Panel · damagedPASSENGER CABIN FLOOR PANEL 241FF; UPPER SURFACE; AFT AREA; SURFACE HAS FRAYING FIBERS. / REPAIRED PASSENGER CABIN FLOOR PANEL 241FF UPPER SURFACE AFT AREA FRAYING FIBERS I/A/W SRM 53-00-50-2R-0 AND SRM 53-00-50-2R-1 REV 70SDR SWAA2020050544280Angle · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE Z-ANGLE LBL 20; WL 156; STA 727D TO 807 HAS MULTIPLE AREAS OF CORROSION ON UPPER AND LOWER SURFACES; MARKED. / AFT CARGO COMPARTMENT FLOOR STRUCTURE Z ANGLE LBL 20; WL156; STATION 727D TO 807 HAS MULTIPLE AREAS OF CORROSIOSDR SWAA2020050544278Angle · corrodedAFT CARGO COMPARTMENT Z-ANGLE RBL 20; WL 156; STA 727D TO STA 767 HAS MULTIPLE AREAS OF CORROSION ON UPPER AND LOWER SURFACES; MARKED. / REMOVED CORROSION FROM AFT CARGO COMPARTMENT 'Z' ANGLE RBL 20; STA 727D-767 VERIFIED MATERIAL LOSS: ORIG. 'T' 0.040'; LOSS:SDR SWAA2020050544553Floorboard · damagedCABIN FLOOR BOARD 242DF UPPER SURFACE PLY IS DAMAGED AT O/B AFT EDGE; 2' FROM O/B EDGE. / REPAIRED CABIN FLOOR BOARD 242DF UPPER SURFACE PLY DAMAGE AT O/B AFT EDGE; 2' FROM O/B EDGE IAW SRM 53-00-50-2R-0. IAW SRM 53-00-50-2R-1 AND SRM 53-00-50-1A-1.SDR SWAA2020050544552Floor Panel · delaminatedPASSENGER FLOOR PANEL 242CF UPPER SURFACE HAS 3 LARGE DENTS WITH DELAMINATION AT FWD RH CORNER AREA. / REPAIRED UPPER SURFACE PLY AT FWD R/H CORNER OF FLOORBOARD PANEL 242 CF IAW SRM 53-00-50-2R-1; PG'S 1;2; STEPS - 3 (A-N).SDR SWAA2020050544377Floor Panel · damagedPASSENGER CABIN FLOOR PANEL 242AF; UPPER SURFACE; FWD AREA; SURFACE HAS FRAYING FIBERS. / REPAIRED PASSENGER CABIN FLOOR PANEL 242 AF UPPER SURFACE FWD AREA FRAYING FIBERS I/A/W SRM 53-00-50-2R-0 AND SRM 53-00-30-2R-1 REV 70SDR SWAA2021080544090Floor Panel · corrodedFWD CARGO COMPARTMENT; FLOOR PANEL 120BF; AREA OF CORROSION ON EDGE OF PANEL; AREA MARKED IN BLUE / ALL WORK WAS ACCOMPLISHED ON JOB CARD 40685-1400-0005 COPY ATTACHEDSDR SWAA2021080544088Floor Panel · crackedFWD CARGO COMPARTMENT FLOOR PANEL 120BF; PANEL HAS CRACK WITH PRIOR STOP DRILL REPAIR INSTALLED / REPLACED FLOOR PANEL 120BF IN FWD CARGO COMPARTMENT IAW B737 AMM 25-52-01-201-801 (FLOOR PANEL WAS OUT OF LIMITS DUE TO EXCESSED 20')SDR SWAA2021070786132Skin · debondedLEFT WING #6 SPOILER HAS A SPOT OF DISBOND ON LOWER SURFACE 9.5' FROM I/B EDGE AND 6.5' FROM AFT EDGE. / REPAIRED LEFT WING #6 SPOILER LOWER SURFACE 9.5' FROM I/B EDGE AND 6.5' FROM AFT EDGE. IAW 737-800 SRM 51-70-10-2R-0 REV 69. 737-800 SRM 51-70-10-2R-2 REV SDR SWAA2020050544230Attach Angle · corrodedFWD PIT; RH LOWER BULKHEAD ATTACH ANGLE HAS CORROSION; BS:500I; RBL:25; WL:155. / VERIFIED PART OUT OF LIMITS DUE TO NO PUBLISHED LIMITS REMOVED OLD PART LOCATED AND DRILLED UP NEW BULKHEAD ATTACH ANGLE AND INSTALLED IAW SRM 51-40-05 AND DRAWING 143A9481 APPLISDR SWAA2020050544229Attach Angle · corrodedFWD PIT; AFT CENTER LOWER BULKHEAD ATTACH ANGLE HAS CORROSION; BS:500I; LBL:24 TO RBL:24; WL:155. / VERIFIED CORROSION ON FWD PIT AFT CENTER LOWER BULK HEAD ATTACH ANGLE AT STA 500I; LBL24 TO RBL24 WL 155 OUT OF LIMITS DUE TO NO PUBLISHED LIMITS REMOVED AND RESDR SWAA2021080543924Floor Panel · corrodedFWD CARGO COMPARTMENT FLOOR PANEL 120AF; CORROSION ON UPPER FWD EDGE OF PANEL; MARKED IN BLUE / EVALUATED CORROSION ON FWD CARGO PANEL 120AF IAW B737 SRM 53-00-53-1A-1. FOUND OUT OF LIMITS DAMAGE EXTENDS BEYOND 20'. REPLACED PANEL IAW B737 AMM 25-01-201-801SDR SWAA2021080543927Floor Panel · corrodedFWD CARGO COMPARTMENT FLOOR PANEL 120DF; AREAS OF CORROSION ON EDGES OF PANEL ON UPPER SIDE OF PANEL; AREAS MARKED IN BLUE / EVALUATED CORROSION FOUND TO BE OUT OF LIMITS EXCEEDS 20' OF CORROSION IAW B737 SRM 53-00-53-1A-1. FABRICATED NEW FLOOR PANEL P/N 453A2SDR SWAA2021072043929Attach Angle · crackedLH WING INBD SIDE OF DEFLECTOR RIB PANEL ATTACH ANGLE CRACKED AT BOOTOM FASTENER. / REMOVED AND REPLACED L/H WING I/B SIDE OF DEFLECTOR RIB; PANEL ATTACH ANGLE P/N 115A6260-1 TAG# A50600 IAW AMM 54-42-51-03 AND SRM 51-40-02-0G-0.SDR SWAA2020050543660Skin · canningRAMP REPORTED SMALL DENT UNDER APU INLET STA 1052 BETWEEN STRINGER 20R AND 21R / FUSELAGE SKIN REPAIRED DUE TO OIL CANNING CONDITION AT DENT LOCATION STA 1052 BETWEEN S-20R AND S-21R IAW SRM 53-80-01-2R-5 REPAIR 5.
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