JASC 5330
Service difficulty reports · 79,347
Reports filed under 5330 · Fuselage Main, Plate/Skin, 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 jasc_code = '5330' 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 jasc_code = '5330' 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 SWAA2018073123895Skin · corrodedAFT CARGO DOOR THRESHOLD EXTERIOR SKIN CORRODED. REPAIRED SKIN PER EA.SDR JJBA20180711007Skin · scratchedDURING A "C" CHECK AT MAINTENANCE FACILITY. THE FOLLOWING DISCREPANCY WAS NOTED. AIRCRAFT EXTERNAL SKIN HAS SCRATCH BETWEEN FRAME 27-28; AT STRINGER 21R-21L. BLENDED 2 EACH AREAS AREA A 5.200"L X 0.900"W, AREA B 0.740"L X 0.250"W, ORIGINAL SKIN THICKNESS CHEM SDR JJBA2018072311005Skin · damagedDAMAGED SKIN BETWEEN FR 59-60 AND BETWEEN STR 11-12L. REPAIRED DAMAGED SKIN BETWEEN FR 59-60 AND BETWEEN STR 11-12L BY CUT OUT, FILLER, DOUBLER FABRICATION AND INSTALLATION. RESTORED SURFACE PROTECTION.SDR DALA2018071204463Skin · corrodedDURING INSPECTION FOUND CORROSION ON FUSELAGE SKIN AREA UNDER DORSAL FIN AND VERTICAL STABILIZER FROM STA 1016 TO STA 1156. AREA WAS REPAIRED PER ETI-37-18-427 REV 2 AND ER/A 569932-14 REV ORIG.SDR SWAA2022022117836Skin · corrodedCORROSION ON FUSELAGE SKIN EXTERIOR SURFACE AROUND DRAIN AT STA. 970 BETWEEN STR. 26L AND 27L / FACT AS A RESULT OF POST REPAIR INSPECTION. CORROSION ON FUSELAGE SKIN EXTERIOR SURFACE AROUND DRAIN AT STA. 970, BETWEEN STRINGER 26L & 27L WAS REPAIRED IAW EA #1-SDR FDEA201807101658Skin · dentedDENT ON OUTER FUSELAGE SKIN BETWEEN STA 420 & STA 440 BETWEEN S-17L & S-18L. MEASURED, CUT OUT AND REPAIRED DENTED AREA ON FUSELAGE SKIN IAW SRM 5-40-02-0G, SRM 51-40-05-0G AND SRM 53-00-00-01-2R REPAIR 16.SDR A6WA2018071345930Landing · crackedLT TRU DOOR AFT LATCH CUTOUT CRACKED AT LANDING. FWD LWR CORNER. REPLACED.SDR DALA2018071104447Skin · corrodedON WALKAROUND FOUND AFT LAV PANEL SKIN CORRODED AND BULGING. REPAIRED ON N/R 1, REF ERA 569907-14.SDR ABXA2018072709077Skin · dentedTWO DENTS ON THE FUSELAGE SKIN AT STATION 632. THE SKIN WAS REPAIRED. THE AIRPLANE WAS GROUNDED.SDR FDEA201807091653Skin · corrodedAFT ACCESSORY COMPARTMENT RT FUSELAGE SKIN AT STA 2163.685 LONGERON 33R-35R, FOUND CORROSION. CARRIED OUT REPAIR AS PER SRM 53-70-01-2R FIGURE 201 REPAIR 3. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. RT FUSELAGE SKIN AT STA 2163.685 LONGERON 33R - LONGERON 35SDR IPXA2018070931528Doubler · gougedFUSELAGE TAIL BALL DOUBLER GOUGED FR 84-FR85, S-43L-S-43R. REPAIRED PER EO A300-5330-69043-B. THIS IS A MAJOR REPAIR.SDR IPXA2018070931527Doubler · gougedTAIL BALL DOUBLER GOUGED FR84-FR85 S-43L - S-43R. REPAIRED PER EO A3005330-69043-B.SDR HDNA2018070900817Skin Panel · corrodedCORROSION DETECTED BEYOND LIMITS PUBLISHED IN REPAIR MANUALS AROUND RIGHT AFT FOOT STEP ON SIDE OF FUSELAGE.SDR HDNA201807090817Skin Panel · corrodedCORROSION BEYOND LIMITS PUBLISHED IN REPAIR MANUALS AROUND LEFT AFT FOOT STEPS ON SIDE OF FUSELAGE.SDR UIEA2018070501340Skin · damagedATA 53-30, ALONG STA 740, ALONG S-3L, UPPER CROWN LT FX SKIN AREA FOUND WITH ONE RIVET HOLE ELONGATED. ELONGATED HOLE DAMAGE ON UPPER CROWN FX SKIN AREA AT STA 740 STR S-3L REPAIRED AS PER EN 1129-18 REV ' - '.SDR FDEA201807081648Skin · dentedCOMPLY WITH EA H-5330-T0340792-P1, FUSELAGE SKIN REPAIR AT STA 1430. REPAIRED FUSELAGE SKIN AT STA 1430 ABOVE STR 35L AND BELOW STR 39L IAW EA NR H-5330-T0340792A.SDR AALA2018071199058Skin · crackedAFT FUSELAGE SKIN CRACKED ON THE LEFT SIDE ABOVE THE AFT AIRSTAIRS, JUST FORWARD OF TAIL CONE EJECTION HANDLE COMPARTMENT. THE AIRCRAFT WAS GROUNDED. REPAIRED IAW 53-30-00-4 REPAIR 4.SDR SWAA2018071123381Skin · crackedFORWARD HINGE OF AUXILIARY POWER UNIT DOOR FUSELAGE SKIN CRACKED. REPAIRED SKIN PER EA.SDR SWAA2022022157919Scuff Plate · crackedFWD CARGO DOOR CUT OUT; FWD LOWER CORNER SCUFF PLATE CRACKED. / LOCATED AND DRILLED NEW FWD. LOWER CORNER SCUFF PLATE; FWD. CARGO DOOR CUT OUT; PART #143A8331-3; I.A.W. S.R.M. 51-40-05-0G-0 AND DRAWING #143A8331; WILL BE INSTALLED FROM ROUTINE CARD; CUSTOMER CSDR SWAA2022022117221Scuff Plate · crackedAFT PIT FWD DOOR SCUFF PLATE IS CRACKED / RECEIVED NEW AFT PIT; FWD CORNER DOOR SCUFF PLATE P/N: 654A004-97 SI#: 7530659 ATAG: WN1013 IAW B737-700 AIPC 53-13-00-05A. LOCATED AND DRILLED IAW B737-700 SRM 51-40-05-0G-0 AND COUNTERSUNK IAW B737-700 SRM 51-40-08-0SDR SWIA2018081445000Skin · dentedMULTIPLE DENTS TO THE RT FUSELAGE SKIN BETWEEN BS 605 AND 589, STRINGERS 21R - 24R. WORKED THE DENTS AND REPAIRED THE AREA IAW REO.SDR DALA2018071704532Skin · gougedWHILE ON THE LINE IN ATL, MTC FOUND GOUGE DAMAGE TO THE LT FUSELAGE SKIN AT STA 590 AND WL 208.1 BETWEEN STR 16L AND 18L AS SEEN IN FIGURE 1 OF THE INSTRUCTIONS. THE GOUGE DAMAGE HAS BEEN BLENDED OUT, MEASURES APPROX 2 UP/DOWN BY 2 FWD/AFT AND IS LOCATED 12.37SDR FDEA201807051635Skin · corrodedFABRICATE NEW DOUBLER AND ADD ADDITIONAL FASTENERS. REMOVED AND REPLACED DOUBLER PER EA 5330-T0340491 P1 AT STA 2020 RT SIDE BETWEEN L29 & L31. COMPLIED WITH WORK CARD EA T 8-5330-70340491 P1.SDR SWAA2022022156796Scuff Plate · brokenAFT CARGO DOOR SURROUND FWD CORNER SCUFF PLATE OB FLANGE HAS PIECE BROKEN OFF (MARKED) / PLATE REPAIRED ON REPAIR ORDER # 7530063-B5R. PLATE TO BE INSTALLED ON ROUTINE TASK CARD # 753-721-00-01.SDR SWAA2022022126649Scuff Plate · crackedCRACK INDICATION AT DENT ON LEADING EDGE OF AFT CARGO BIN DOOR SCUFF PLATE PER NDT MANUEL PART 6; 51-00-00 PRO.14 / REMOVED AND REPLACED AFT CARGO BIN DOOR SCUFF PLATE PER SRM 53-60-15SDR SWAA2018080824104Skin · corrodedFUSELAGE SKIN AT BUTT JOINT FORWARD SIDE CORRODED AT BS 1016, BETWEEN STR 20L TO STR 22L. REPAIRED SKIN IAW ER AND EA.SDR SWAA2018080824103Skin · corrodedFUSELAGE SKIN AT BUTT JOINT AFT SIDE SKIN CORRODED AT BS 1016, BETWEEN STR 20L TO STR 22L. REPAIRED SKIN PER EA.SDR FDEA201807041629Skin · corrodedEMPENNAGE RT AFT SKIN FOUND WITH CORROSION UNDERNEATH BODY FAIRING 347DF LOWER EDGE BETWEEN STA 2146 TO 2164. CORROSION BLENDED OUT AND FOUND EXCEEDED ALLOWABLE LIMITS AS PER SRM 53-70-01-2R FIG 201 REPAIR 3. ORIGINAL THK 0.095" THK REMOVED 0.080" THK REMAINEDSDR SWAA2022022156638Scuff Plate · crackedFWD CARGO BAY FWD CORNER SCUFF PLATE IS CRACKED / REPAIRED FWD CARGO BAY FWD CORNER SCUFF PLATE IAW SWA EA 1-A53-2076 REV 11SDR SWAA2022022156639Scuff Plate · crackedAFT CARGO BAY FWD CORNER SCUFF PLATE IS CRACKED / REPAIRED AFT CARGO BAY FWD CORNER SCUFF PLATE IAW SWA EA 1-A53-8076 REV 11SDR SWAA2022022156781Scuff Plate · crackedAFT CARGO DOOR AFT THRESHOLD CRACKED / PLATE REPAIRED ON REPAIR ORDER # 7530337-A2R. PLATE TO BE INSTALLED ON ROUTINE TASK CARD # 753-721-00-01.SDR K11A2018112124008Skin · crackedFUSELAGE SKIN, 1 INCH CRACK. UNDER ENGINE INLET FWD END OF CAVITY THROUGH ACCESS PANELS 9521 AND 9522, ON FUSELAGE.SDR SWAA2018080824102Bear Strap · corrodedFORWARD CARGO BAY DOOR CUTOUT BEAR STRAP CORRODED AT BS 490, RBL 39. REPAIRED STRAP IAW ER AND EA.SDR SWAA2018071023319Skin · damagedFUSELAGE SKIN CREASED AT BS 1007, BETWEEN STR 15R TO STR 16R. REPAIRED SKIN PER EA.SDR UIEA2018060201015Skin · dentedFOUND TWO DENTS ADJACENT TO EACH OTHER AT RIGHT UPPER HALF OF FUSELAGE APPROX AT STA 1197 BETWEEN STRINGER 3R-4R, BELOW JOINT LAP. REMOVED 3EA FASTENERS BETWEEN 1197+88 AND STA 1197+132 STR 2R AND 4R, HFEC AREA NO CRACKS NOTED, RE-INSTALLED 3EA FASTENERS AT ARSDR SWAA2022021818313Scuff Plate · crackedAFT CARGO BAY DOOR FWD SCUFF PLATE IS CRACKED AT FWD AND AFT RADIUS. / RECIEVED NEW PART; LOCATED DRILLED PER SRM 51-40-02-0G-0 & SRM 51-40-05-0G-0SDR SWAA2022021818314Scuff Plate · crackedAFT CARGO BAY DOOR AFT SCUFF PLATE IS CRACKED AT AFT RADIUS. / ACB AFT SCUFF PLATE TO BE REPLACED ON CUSTOMER CARD # T815241SDR K11A2018112124001Skin · crackedCRACK IN EXTERIOR SKIN ABOVE LEFT AFT EMERGENCY EXIT HATCH, ABOVE HANDLE.SDR IPXA2018072331912Skin · corrodedINSPECTION TYPE:4C, UPPER AFT NUT PLATE HAS EXFOLIATION CORROSION AROUND IT ON SKIN INSIDE ACCESS 316AB RT SIDE APPROX STA 2160. REPAIRED AFT FUSELAGE UPPER AFT SKIN AT APPROX STA Y=2160 BETWEEN LONGERON 12R AND LONGERON 13R IAW EA 011-5370-01-A7362 REV IR ANDSDR IPXA2018072031882Skin · dentedINSPECTION TYPE:4C, FUSELAGE EXTERIOR SKIN DENTED AT STA 5-46 BETWEN L46R AND L47R. DENT REPAIRED PER EO MD11-5330-69249-A AND EA 011-5300-01-A7349 REV IR (MINOR)SDR DALA2018070304374Access Panel · damagedDURING INSPECTION FOUND HOLGED HOLE ON ACCESS PANEL 193AL. ACCESS PANEL 193AL WAS REPAIRED PER SRM 53-40-70 REPAIR 1 PAR 4B (2). TABLE 202, SRM 51-70-05 REPAIR 8 PAR 4 F G AND SRM 51-70-05 REPAIR GENERAL PAR 4.SDR DALA2018070304372Access Panel · wornDURING INSPECTION FOUND WEAR IN COMPOSITE MATERIAL OF ACCESS PANEL 193D. ACCESS PANEL WAS REPAIRED PER SRM 51-70-05-2R-6 PAR 4 STEP E F AND G AND SRM 51-70-05-2R-0.SDR AALA20180702004Skin · crackedAIRCRAFT IN BASE MAINTENANCE. CRACK AT AFT RIGHT HAND NOSE GEAR DOOR, AFT HINGE CUTOUT. INSTALLED DOUBLER AND EDGE SEALED PER SRM 53-05-00-001, FIGURE 158 AND DRAWING SGO9530030.SDR FDEA201807021621Angle · crackedNR 3 ACM COMPT CEILING AT STA 595 AND LONGERON 29 AIR LEAK FOUND DURING PRESSURIZATION. INSTALLED REPAIRED ANGLE IN REF TO SRM 53-40-00,VOL1 FIG 28 AT NR 3 ACM COMPT CEILING STA 595 AND LONGERON 29.SDR MK1Y20180702005Skin · crackedFOUND A CRACK ON AN EXISTING BLENDOUT, EXTERNAL FUSELAGE SKIN, AFT OF THE CARGO DOOR CUTOUT, BS 1271, BETWEEN STRINGERS 29R AND 30R.SDR MK1Y20180702004Skin · crackedFOUND A CRACK ON THE EXTERNAL FUSELAGE SKIN, BS 1923, 10 INCHES BELOW STRINGER 25RSDR MK1Y20180702003Skin · dentedDEEP DENT FOUND ON THE EXTERNAL FUSELAGE SKIN BETWEEN BS 1562 - 1582, STRINGERS 24L - 26LSDR EBVR20180702001Skin · corrodedBLEND AND REMOVE CORROSION AND EVALUATE 1 EACH PIN HOLE ON THE R/H SIDE OF THE FUSELAGE, JUST AFT OF THE NOSE ACCESS DOOR. PERFORMED REPAIR TO RT NOSE SKIN AFT OF AVIONICS DOOR.SDR SWAA2022021819790Scuff Plate · crackedFWD CARGO DOOR SCUFF PLATE HAS CRACK. CRACK 3' AFT OF FORWARD EDGE OF SCUFF PLATE. MEASURES APPROXIMATELY 1' LONG. / REMOVED AND REPLACED FWD CARGO DOOR CENTER SCUFF PLATE REF AMM 53-11-02.SDR SWAA2022021856628Scuff Plate · crackedAFT CARGO BAY AFT CORNER SCUFF PLATE CRACKED / REPAIRED AFT CARGO BAY AFT CORNER SCUFF PLATE IAW SWA EA 1-A53-2075 REV 11
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