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.

SDR DALA2017030902000Skin · crackedFUSELAGE SKIN CRACKED BS 1531 BETWEEN LONGERONS 22 TO 25L. AREA WAS REPAIRED IAW SRM 53-00-01.Mar 8, 2017 · N924DN · Doug MD9030SDR N6WA2017030803Skin · corrodedLEVEL 2 CORROSION AT BS 333 CIRCULAR JOINT SPLICE AT STRINGER 26R. REMOVED AND REPLACED JOINT SPLICE IAW SRM 51-42-06.Mar 8, 2017 · N167GJ · Cndair CL6002C10SDR 7C7A2017030800287Skin Panel · dentedDENT DAMAGE TO FUSELAGE SKIN PANEL 85310533 STA X123 STR 24S AND 25S. REPAIRED IAW ECO 008.53-17-05.Mar 8, 2017 · N883EA · Dhav DHC8106SDR DALA2019070704066Skin · not reportedFUSELAGE SKIN AT GOGO WI-FI FWD ATG4 ANTENNA, FR 25 TO FR 26, S-43L TO S-42R; SECTION II PERMANENT REPAIR II PER ER/A 539169-14AD REV.B.Mar 7, 2017 · N322US · Airbus A320211SDR DALA2018082805315Skin · dentedDENT FOUND ON THE EXTERNAL SKIN, DURING A WALK AROUND, UNDER AND JUST FWD OF L1 DOOR ON LOWER FUSELAGE, PERFORMED PERMANENT REPAIR BETWEEN FRAMES 12+3 AND 16 ABOVE THE LT UPPER STRINGER ON FUSELAGE IAW SRM 53-11-11-300-006, ITEM 2. A STEPS 1A TO R, FIGURE 2010Mar 7, 2017 · N373NW · Airbus A320212SDR V0XD20170308014Skin · damagedDAMAGE TO FUSELAGE SKIN INTERIOR SURFACE BETWEEN FS517-FS533 AND STR 20-21L. BLENDED DAMAGE AND RESTORED FINISH IAW REO 670-53-31-407, DATED 2017-03-07, SRM 51-25-16, 51-21-11, AND 51-25-06. NDT PERFORMED.Mar 7, 2017 · N369CA · Cndair CL6002C10SDR DALA2017030801895Skin · dentedUPON REMOVAL OF LT FRACTAL DOUBLER, A DENT WAS FOUND. BETWEEN FR 59 AND FR 60 BETWEEN STR. 19L AND 20L. WIDTH 3.2 ( FORE AND AFT) HEIGHT 2 ( UP & DOWN ) APP DEPTH .031 6 EXISTING FAST. HOLES ARE LOCATED INSIDE OF THIS AREA CTR IS 5.0 FROM AFT EDGE OF ORIG. DOUMar 7, 2017 · N365NB · Airbus A319114SDR 7C7A2017030700286Skin · dentedDENT DAMAGE TO THE FUSELAGE SKIN PANEL BETWEEN BS 291.4 AND 312.35, STRINGER 1-2R. REPAIRED IAW RD 8-53-15073 WC 53-123.Mar 7, 2017 · N883EA · Dhav DHC8106SDR SWAA2017032912837Skin · crackedSKIN CRACKED AT BS 540R. R & R THE SKIN IAW EA .Mar 6, 2017 · N217JC · Boeing 7377H4SDR SWAA2017032912836Skin · crackedSKIN CRACKED AT BS 540. R & R THE SKIN IAW EA.Mar 6, 2017 · N217JC · Boeing 7377H4SDR DALA2017030801995Skin · damagedFUSELAGE PREVIOUS BLEND OUT ON EXTERNAL SKIN, BS 70, LONGERON 24L. REPAIRED IAW ERA 511165.Mar 6, 2017 · N923DN · Doug MD9030SDR DALA2017030801994Skin · crackedCRACKED FUSELAGE SKIN, BS 1522 BETWEEN LONGERONS 1 TO 2R. REPAIRED THE SKIN IAW SRM 53-00-01.Mar 6, 2017 · N924DN · Doug MD9030SDR DALA2017030701860Doubler · corrodedFUSELAGE, CABIN, RT STA 889 TO 908 R56.0, SPLICE DOUBLER, UNDERSIDE, CORROSION. REPLACED LOWER SKIN SPLICE DOUBLER AT STA 889-908 IAW SRM 51-41-05.Mar 6, 2017 · N972AT · Boeing 717200SDR SWAA2017072415181Skin · crackedAFT ENTRY DOOR FUSELAGE SKIN CRACKED AT FORWARD LOWER CORNER. REPAIRED THE SKIN IAW EA.Mar 5, 2017 · N613SW · Boeing 7373H4SDR DALA2017030601823Skin · dentedLEFT LOWER FUSELAGE HAS TWO DENTS 1 AT BS 620 STRINGER 17L THE SECOND AT BS 628 STRINER 17L. REPAIRED IAW ER/A 554321-14 REV ORIG.Mar 5, 2017 · N704X · Boeing 7572Q8SDR SWAA2017030812398Skin · crackedFUSELAGE SKIN PANEL CRACKED BETWEEN BS 827+5. TO 827+5.5, STRINGER 17L. REPAIRED SKIN IAW SRM.Mar 4, 2017 · N363SW · Boeing 7373H4SDR DALA2017030601847Skin · corrodedCORROSION ON EXTERNAL FUSELAGE SKIN BETWEEN BS 520 AND 540, STRINGER 28L AND 28R. REWORKED AREA ON THE SKIN AND FOUND WITHIN LIMITS IAW SRM 53-00-01, ALLOWABLE DAMAGE 1, DETAIL II, FIG 101, SHEET 4 OF 6.Mar 4, 2017 · N660DL · Boeing 757232SDR DALA2017030601829Skin · corrodedCORROSION ON EXTERNAL FUSELAGE SKIN BETWEEN BS 640 AND 660, STRINGERS 28L - 28R. REWORKED AREA AND FOUND WITHIN LIMITS IAW SRM 53-00-01, ALLOWABLE DAMAGE 1, DETAIL II, FIG 101, SHEET 4 OF 6.Mar 4, 2017 · N660DL · Boeing 757232SDR DALA2017030601828Skin · corrodedCORROSION ON EXTERNAL FUSELAGE SKIN BETWEEN. BS 720 AND 740, STRINGER 28L AND 28R. REWORKED THE AREA AND IS WITHIN LIMITS IAW SRM 53-00-01, ALLOWABLE DAMAGE 1, DETAIL II, FIG 101, SHEET 4 OF 6.Mar 4, 2017 · N660DL · Boeing 757232SDR SWAA2017031712517Skin · crackedFUSELAGE SKIN CRACKED AT L2 DOOR FWD LOWER CORNER CUTOUT. REPAIRED THE SKIN IAW EA.Mar 3, 2017 · N613SW · Boeing 7373H4SDR DALA2017033102582Skin · damagedFUSELAGE SKIN STA 235, ABOVE L-18L "FOUR CORNERS" AREA DENT AND GOUGE. PERMANENT REPAIR RESTRICTION. ER/A 539814-14 REV B IS CURRENT. REMOVED TIME LIMITED REPAIR AT STA 235 LONGERON 18LT AND ACCOMPLISHED A CLASS 1 PERMANENT REPAIR IAW SRM 53-10-01 REPAIR 10 FIMar 2, 2017 · N996AT · Boeing 717200SDR ASOA201703023032Skin · corrodedREAR FUSELAGE SKIN UNDER FORWARD NR 2 RADIO ALTIMETER CORRODED. SKIN AREA REPAIRED IAW SRM 53-00-23, ITEM 3.Mar 2, 2017 · N11544 · Emb EMB145LRSDR ASOA201703023027Doubler · corrodedWATER SERVICING POINT DOUBLER CORRODED. DOUBLER REPLACED IAW SRM 51-40-02.Mar 2, 2017 · N11544 · Emb EMB145LRSDR AALA20170302012Skin · crackedA CRACK WAS FOUND IN THE SKIN AT PULLED FASTENER BETWEEN BS 360 - 380 WITH CORROSION ON STRINGER SPLICE AT STRINGER 26L. REPAIRED STRINGER SPLICE PER EA #267695.Mar 2, 2017 · N904AN · Boeing 737823SDR DALA2017030301754Skin · dentedLEFT UPPER FUSELAGE HAS ONE DENT AT BS 416 ABOVE STRINGER 13L. REPAIRED IAW ER/A 554322-14, REV ORIG.Mar 2, 2017 · N704X · Boeing 7572Q8SDR DALA2017030201714Skin · damagedEXISTING BLENDOUT AT STA 1990 , S-28L TO S-29L MEASURED AND FOUND OUT OF LIMIT: ORG THK 0.075", MATERIAL REMAINED 0.056" (L=1.4' X 1.2") AS PER SRM 53-00-01 FIG 102. DAMAGED AREA TRIMMED OUT (L=2" X 1") AND REPAIR CARRIED OUT AS PER SRM 53-00-010 REPAIR 7 FIG Mar 2, 2017 · N705DN · Boeing 777232LRSDR DALA2018030801488Doubler · damagedOVERSIZED FASTENER HOLES IN THE CHEM MILL FWD RT SIDE OF DOUBLER, REPAIRED IAW ER/A 555976-14AD.Mar 1, 2017 · N329NB · Airbus A319114SDR AALA201703039013Skin · corrodedCORROSION ON FUSELAGE SKIN UNDER AFT DRAIN MAST BETWEEN STRINGERS 25 - 26R. REPAIRED THE SKIN IAW SRM 53-00-01 AND SRM 51-40-02.Mar 1, 2017 · N938UW · Boeing 7572B7SDR DALA2017030201711Skin · crackedDURING INSPECTION, FOUND A CRACK ON CUTOUT ON EXTERNAL GROUND ELECTRICAL POWER AFT EDGE ON LOWER FUSELAGE. REPAIRED IAW SRM 53-10-15, REPAIR 4.Mar 1, 2017 · N303DQ · Boeing 737732SDR DALA2017030201687Skin · corrodedCORROSION ON FUSELAGE SKIN AREA BELOW FILLET PANEL RUBSTRIP UPPER SECTION BETWEEN BS 760 - 800. CORROSION REMOVED IAW SRM 51-10-04 0G PAR. 26, 21, AND 15. UT WAS ACCOMPLISHED IAW NDT SPM 04-00-07 PAR 5 FIG 3 SHEET 1 AND 2.Mar 1, 2017 · N929AT · Boeing 717200SDR SWAA2017030312305Doubler · crackedELECTRICAL GROUND POWER RECEPTACLE SURROUND DOUBLER CRACKED ON AFT SIDE. REPAIRED DOUBLER IAW SRM.Feb 28, 2017 · N909WN · Boeing 7377H4SDR VNAA2017022800035Doubler · corrodedANTENNA DOUBLER AT STRINGER 27 BETWEEN BS 295 AND 310 IS CORRODED. REMOVED AND REPLACED ANTENNA DOUBLER.Feb 28, 2017 · N544EA · Cndair CL6002C10SDR ASOA201702281276Skin Panel · corrodedCORROSION FOUND ON THE EXTERNAL SKIN UNDER THE TCAS ANTENNA. BLENDED SKIN UNDER LOWER TCAS ANTENNA, NDT FOUND .001' MATERIAL REMOVED, NO DAMAGE ALLOWED IN THIS AREA IAW SRM 53-21-01-101-002 A01. SUBMITTED TO STS ENGINEERING. COMPLIED WITH EA 43-2017-019 AND ECFeb 28, 2017 · N748EV · Cndair CL6002C10SDR DALA2017030101710Skin · corrodedDURING INSPECTION, FOUND EXTERNAL FUSELAGE SKIN HAS PULLED RIVETS AND BULGING SKIN AT BS 360+8 TO +13 STRINGER 26L. MAINTENANCE REPAIRED THE SKIN IAW ERA 553117-14 REV O.Feb 28, 2017 · N377DA · Boeing 737832SDR IPXA2017030114550Skin · damagedFUSELAGE SKIN DAMAGED AT BS 132.5 BETWEEN STRINGERS 24 - 30R. DAMAGE MEASURES 12 INCHES CIRCUMFERENTIAL BY 2.25 INCHES FORE & AFT AND 1.5 INCHES OUTWARD DEFLECCTION, DAMAGE IS APPOX 6 INCHES FROM LOWER EDGE OF SKIN AND AT L/E. REPAIRED IAW EO B767-5330-63407Feb 28, 2017 · N340UP · Boeing 76734AFSDR IPXA2017032515480Skin · corrodedINSPECTION TYPE: 3C, AFT FUSELAGE RIGHT SIDE EXTERIOR SKIN HAS CORROSION BETWEEN BS 2129 - 2163.685, LONGERON 32 - 35R. REPAIRED THE SKIN IAW EA 011-5330-01-A6699-IR, AND EO MD11-5330-63701-AFeb 27, 2017 · N287UP · Doug MD11FSDR IPXA2017032315441Skin · corrodedINSPECTION TYPE: 3C, EXTERIOR AFT FUSELAGE SKIN AT BS 2140 TO 2163.685, LONG. 12 - 13R. REPAIRED THE SKIN IAW EA 011-5330-01-A6705, REV I/R, AND EO MD11-5330-63687-A. (MAJOR)Feb 27, 2017 · N287UP · Doug MD11FSDR IPXA2017031915296Skin · corrodedINSPECTION TYPE: 3C, LEFT HORIZONTAL LOWER FAIRING ATTACH SKIN HAS CORROSION AT BS 2160 AND LONGERON 35L. REPAIRED THE SKIN IAW SRM 57-70-01, REPAIR 3, FIG 201. MAJOR REPAIR.Feb 27, 2017 · N287UP · Doug MD11FSDR SWAA2017030612339Skin · damagedFUSELAGE SKIN CREASED BETWEEN BS 500+4 TO BS 500+7, STR 17L. REPAIRED SKIN PER ER & EA.Feb 27, 2017 · N429WN · Boeing 7377H4SDR UIEA2017030300275Doubler · corrodedBS 994 STRINGERS 45 - 46R, EXTERNAL DOUBLER FOUND CORRODED. REPLACED THE DOUBLER IAW SRM 51-10-02, AND SRM 51-40-02.Feb 27, 2017 · N492MC · Boeing 74747UFSDR UIEA2017030300274Skin · crackedBS 983, STRINGER 38R AT DRAG SPLICE FT AREA FOUND CRACK IN SKIN LAYER. THE SKIN WAS REPAIRED IAW SRM 53-20-R2, REPAIR 2, FIG 201.Feb 27, 2017 · N492MC · Boeing 74747UFSDR UIEA2017030300273Skin · crackedBS 983, STRINGER 38L AT DRAG SPLICE FITTING AREA FOUND CRACKED AT SKIN LAYER. THE SKIN WAS REPAIRED IAW SRM 53-20-2R2, REPAIR 2, FIG 201.Feb 27, 2017 · N492MC · Boeing 74747UFSDR UIEA2017030300272Skin · crackedLEFT NLG AFT WW CORNER AT BS 400 FOUND CRACKED. THE SKIN WAS REPAIRED IAW EO 4453A516 PART 3 AND RI-53-10-11743.Feb 27, 2017 · N492MC · Boeing 74747UFSDR IPXA2017022714462Skin · damagedFUSELAGE SKIN DAMAGED AT FR 20A. REMOVED DAMAGE AND REPAIRED THE SKIN IAW EO A300-5330-63377-B.Feb 27, 2017 · N157UP · Airbus A300F4622RSDR IPXA2017031415116Skin · chafedINSPECTION TYPE: 3C, EXTERIOR FUSELAGE SKIN UNDER WING TO BODY FAIRINGS AT BS 1159, LONGERON 44R HAS DEEP WEAR FROM PANEL CONTACT. REPAIRED THE SKIN IAW SRM 53-40-01, REPAIR 3, FIG 201. MAJORFeb 26, 2017 · N287UP · Doug MD11FSDR NACA2017022700021Skin · crackedTHE FUSELAGE SKIN, FOUND A 3 INCH CRACK, 2 INCHES AFT OF BS 727E DIRECTLY ABOVE STRINGER 23R. THE SKIN WAS REPAIRED IAW SRM 53-00-01, REPAIR 31.Feb 26, 2017 · N360WA · Boeing 737301SDR DALA2017022701672Doubler · dentedDENT ON EXTERNAL SKIN REPAIR DOUBLER LOCATED BETWEEN S-15L TO S-18L AND BS 620+5 INCH AT UPPER FUSELAGE. THE DENTS ON EXTERNAL REPAIR DOUBLER LOCATED BETWEEN S15L TO S18L AND BS 620+5 INCH AT UPPER FUSELAGE ARE ASSESSED WITH ER/A NR 477155-14 REVISION "C" AND Feb 25, 2017 · N660DL · Boeing 757232SDR DALA2017022501650Vent · corrodedDURING INSPECTION, FOUND CORROSION AROUND TOILET VACUUM EXHAUST VENT. MAINTENANCE REPAIRED IAW ERA 555619-14 REV. 0.Feb 25, 2017 · N3771K · Boeing 737832SDR NACA2017022700020Skin · crackedSKIN HAD A 2 1/2 INCH CRACK 6 INCHES AFT OF BS 727E DIRECTLY ABOVE STRINGER 21R. FUSELAGE SKIN REPAIRED IAW SRM 53-00-01, REPAIR 31.Feb 25, 2017 · N360WA · Boeing 737301SDR DALA2017081806305Skin · dentedDENTS AND PULL IN RIVETS FOUND ON EXTERNAL SKIN BETWEEN FRAMES 53 - 54 AND STRINGER 41L, REPAIR ON EXTERNAL SKIN BTW FR 53 TO FR 54 AND STR 37L TO STR 42L ON LOWER FUSELAGE IAW ER/A 554926-14AD REV. ORIGINALFeb 24, 2017 · N327NW · Airbus A320211
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