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 CALA2016072295576Skin · crackedRIGHT FUSELAGE SKIN BS 2260 HAS A CRACK APPROX 1.5 INCHES IN LENGTH. REPAIRED IAW SRM-53-00-01, REPAIR-4, ZONE-B.SDR CALA2016072295573Doubler · not reportedLEFT AIRFONE ANTENNA REQUIRES DOUBLER REPAIR FR 63-64 STR 41L-42L FABRICATED, LOCATED & DRI LLED & INSTALLED REPAIR DOUBLER IAW SRM 53-00-11-201 FIG 230SDR FDEA201607202559Skin · damagedRIGHT UPPER FUSELAGE FRAME 32 EXTERNAL SKIN HAS A LIGHTNING STRIKE. PERFORMED PERMANENT REPAIR IAW SRM 53-10-12, FIG. 203, SHEET 3, 6 AND 7. MAJOR REPAIR.SDR R61A201607200421Skin · dentedLT FORWARD FUSELAGE SKIN, DENTED AND SCRATCHED BETWEEN FRAMES 10-11 AND STRINGERS 15-16L. REPAIRED IAW ETD2016-170-065491 AND SRM 53-10-01 REPAIR 12P. MAJOR REPAIR.SDR COEA2016071946811Skin · damagedLIGHTNING STRIKE DAMAGE ON FWD FUSELAGE LOWER SKIN PANEL BETWEEN FRAMES 21 & 22 AT STRINGER 21L. REPAIRED IAW SRAS CETS-3588/16.SDR COEA2016071945811Skin · damagedBRIDGING CHECK COE/MAJOR REPAIR. EXTERNAL FUSELAGE SKIN HAS A LIGHTNING STRIKE BETWEEN FRAMES 3/4, STRINGERS 14R & 15R. REPAIRED PER SRM 51-21-17.SDR SWIA201642444Skin · corrodedEXTERIOR SKIN HAS CORROSION COMMON TO TCAS ANTENNA BETWEEN BS 295 AND 310, STRINGER 27. COMPLIED WITH ALL STEPS OF EA PERMANENT REPAIR.SDR ASAA2016071917561Skin · crackedCHEM MILL HAS A CRACK IN THE RT FUSELAGE SKIN, BS 727D+2. ACFT GROUNDED. REPAIRED THE SKIN IAW SRM 53-00-01-2R-31 DET VII.SDR SWAA2016072554184Skin · crackedFUSELAGE SKIN CRACKED AT BS 967+5, STR 5R. REPAIRED SKIN IAW SRM.SDR IPXA2016072306168Floor Panel · damagedINSPECTION TYPE:C, MAIN CABIN BS 1100 FLOOR PANEL 242XKF DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-H.SDR FDEA201607192540Skin · corrodedLONGERON 48, BS 1733 SKIN AREA JUST ABOVE BEAUTY STRIP IS CORRODED. CLEANED THE CORROSION AND TREATED IAW SRM 51-21-01.SDR FDEA201607192537Skin · corrodedLOWER FUSELAGE LEFT SIDE, LONGERON 48, BS 1542, SKIN AREA JUST ABOVE BEAUTY STRIP IS CORRODED. REMOVED THE CORROSION AND TREATED SKIN IAW SRM 51-21-01SDR ASAA2016071817635Skin · crackedRIGHT FUSELAGE AT R1 DOOR LOWER HINGE CUTOUT IS CRACKED. ACFT GROUNDED. REPAIRED THE SKIN IAW SRM 53-10-01-2R-15.SDR ABXA20160718117Skin · corrodedREMOVED CORROSION IAW SRM 57-51-02, FIG 101. INITIAL THICKNESS .094, REMAINING THICKNESS .061. BLENDED AREAS REQUIRED REPAIR AND WERE REPAIRED ON REA B657-62130. CORRODED LEVEL 2, PN 113T1621-58, SKIN, FS/BS LOCATION: FROM R/W T/E TO UPPER STR, WS LOCATION: SDR ABXA20160718116Skin · corrodedFOUND SKIN CORROSION COMMON TO THE TRIMMED OUT SECTION OF THE FAIL SAFE. CORROSION IS ISOLATED TO THE LOWER HOLE. COMPLIED WITH TASK CARD EA 53500014-004 AND DOCUMENT 470080RD10 CORROSION WAS REMOVED, WITHIN THE ALLOWABLE LIMITS. CORRODED, LEVEL 2, PN 145T34SDR SWAA2016080254381Skin · crackedLOWER BULKHEAD SKIN CRACKED AT BS 540, STRINGER 22L. REPAIRED IAW EA.SDR A6WA2016080144109Doubler · corrodedACFT BELLY INSIDE SKIN DOUBLER HAS CORROSION, BETWEEN BS 409+32 TO 409+16 AND STRINGERS 25 - 26L IN THE FWD E & E BAY. REPLACED THE SKIN DOUBLER AND FILLER IAW EC 601R-53-4534.SDR FXGA201607181618Skin · damagedFUSELAGE SKIN AND STRINGER REPAIR AT BS 341, STRINGER 27L. TO REPAIR THE CORRODED SKIN AND STRINGER 27L AT BS 341. CUT-OUT OF THE CORRODED SKIN AND REPAIR PER A&B OVERHAUL MANUAL FIGURE 12-22. CUT STRINGER 27L BETWEEN BS 332 AND 350. REPAIR PER A&B OVERHAUL MSDR ASOA20160719016Skin · dentedSKIN DENTED AT FRAME 2 STRINGER 2R. CUTOUT DAMAGED SECTION, FABRICATED FILLER AND DOUBLER, INSTALLED , PRIMED AND PAINTED. AIRCRAFT RELEASED AND RETURNED TO SERVICE.SDR QXEA2016080300504Doubler · corrodedFOUND CORROSION ON MACHINE DOUBLER AT LAVATORY SERVICE DOOR. FOUND OUT OF LIMITS IAW SRM 52-42-10-02-01 FIG. 201. REPLACED THE DOUBLER IAW SRM 51-42-05-02-01.SDR CALA2016071800428Skin · burnedLIGHTNING STRIKE ON SKIN BS 2039 1/2" DIA 1 PLY DEEP (0.009") BETWEEN S37 - 38R. WITHIN LIMITS IAW SRM B787-A-53-80-01-02A-661A-A TABLE 1.SDR CALA2016071800427Skin · burnedLIGHTNING STRIKE ON SKIN BS 1952 1.75" DIA 2 PLYS DEEP (0.017" ) BETWEEN S37-36R. WITHIN LIMITS REF SRM B787-A-53-80-01-02A-661A-A TABLE 1.SDR CALA2016071800426Skin · damagedLIGHTNING STRIKE ON SKIN STA 1728 1.5" DIA 2 PLYS DEEP (0.017") AT S34R. WITHIN LIMITS IAW SRM B787-A-53-70-01-02A-661A-A TABLE 1. REPAIRED IN ACCORDANCE WITH SRM B787-A-51-73-02-03A-663A-ASDR DALA2016071705370Skin · damagedLIGHTING STRIKE ON RT WINDOW BELT AFT LOWER CORNER BS 1060 - 1079. WINDOW BELT PANEL WAS REPAIRED AND WITHIN LIMITS IAW ER/A 547849-14 REV. ORIGINAL SECTION I.SDR DALA2016071705369Skin Panel · damagedINITIAL LIGHTING STRIKES ON RT WINDOW BELT ON FWD AN AFT UPPER CORNER AT WINDOW PASSENGER BETWEEN STA Y598 TO 617. WINDOW BELT PANE STA Y=598-617, RT WAS REPAIRED AND IT IS WITHIN LIMITS IAW ER/A 547845-14, REV ORIGINAL, SECTION I.SDR A6WA201644104Skin · dentedLEFT LOWER FUSELAGE SKIN HAS DENT AT FS 621.00 AND STR 19L. REPAIRED LT LOWER FUSELAGE SKIN AT FS 621.00 AND STR 19L IAW EA CRJ253-0430, REV IR
DATED 07/09/2016.SDR SWAA2016090655475Bear Strap · crackedL2 DOOR CUTOUT UPPER AFT CORNER BEAR STRAP CRACKED AT BS 986.5. REPAIRED THE BEAR STRAP IAW SRM.SDR IXXA20160818050Skin · crackedLEFT FUSELAGE SKIN CRACKED BS 1654 BETWEEN STRINGERS 4 - 6R. REPAIRED THE SKIN IAW SRM 53-80-01 REPAIR 4.SDR DALA2016071605463Skin · damagedFWD LOWER FUSELAGE SKIN DAMAGED BETWEEN FRAMES 1 AND 2. COMPLIED WITH FINAL ER/A 548858-14.SDR GTIA2016071501509Skin · damagedDURING INSPECTION, FOUND LIGHTNING BURN ON UPPER FUSELAGE AT FRAME 38. A PERMANENT REPAIR OF TEH LIGHTNING STRIKE WAS PERFORMED IAW EO 5331-1628.SDR DALA2016071805371Skin · damagedSCRATCHES ON WINDOW BELT BS 886 - 905. BLENDED OUT, MEASURED AND TREATED. ALL ARE WITHIN LIMITS IAW 53-05 FIGURE 111.SDR DALA2016071605361Skin Panel · damagedINITIAL, LIGHTING STRIKE ON RT WINDOW BELT FWD, AFT LOWER CORNER BETWEEN STA Y= 503-522. WINDOW BELT PANEL STA Y= 503-522, RT WAS REPAIRED AND IT IS WITHIN LIMITS IAW ER/A 547844-14, REV ORIGINAL SECTION I.SDR DALA2016071605360Skin Panel · damagedINITIAL, LIGHTING STRIKE ON RT WINDOW BELT AFT LOWER CORNER BETWEEN STA Y=1022-1041. WINDOW BELT PANEL STA Y=1022-1041 RT WAS REPAIRED AND IT IS WITHIN LIMITS IAW ER/A 547848-14, REV ORIGINAL SECTION I.SDR DALA2016071605359Skin Panel · damagedINITIAL, LIGHT STRIKE ON RT WINDOW BELT AFT UPPER CORNER BETWEEN STA Y= 712-731. WINDOW BELT PANEL STA Y=712-731 RT WAS REPAIRED AND IT IS WITHIN LIMITS IAW ER/A 547846, REV ORIGINAL SECTION I.SDR DALA2016071605338Skin · crackedRIGHT FUSELAGE EXTERIOR SKIN CRACKED AROUND FASTENER HEAD STA 1095 JUST ABOVE LONGERON 14R. REPAIRED RT FUSELAGE EXTERIOR SKIN AT STA 1095 AND LONGERON 14R IAW ER/A 547486-14, ORIGINAL REV ASSOCIATED ER/A 00-547486.SDR DALA2016071605333Skin · wornWEAR ON FUSELAGE SKIN IN LONGERON 20RT BETWEEN STA Y=520-526, SM, CARD 27, ZONE 110. DAMAGE WAS REPAIRED IAW ETI-17-16-084, REV 1 AND ER/A 547867-14, REV ORIGINAL. RII COMPLETED.SDR DALA2016071605332Skin · wornWEAR ON FUSELAGE SKIN IN LONGERON 21RT BETWEEN STA Y=503-508,SM, CARD 28, ZONE 110. WEAR ON FUSELAGE SKIN IN LONGERON 21RT BETWEEN STA Y=503-508 OUT OF LIMITS. ORIGINAL THICKNESS 0.050" REMAINING THICKNESS 0.035", DAMAGE WAS REPAIRED IAW ETI-17-16-084, REV 1SDR FDEA201607142485Skin · damagedDAMAGED AT LOWER CORNER OF FUSELAGE AT FWD SIDE OF AFT CARGO DOOR FROM A PREVIOUS DOUBLER REPAIR.SDR REXA2016071401317Skin · dentedDENT ON FUSELAGE SKIN BELOW GROUND AIR DOOR BETWEEN FS 1031 AND FS 1047, STR 26R AND 25R. C/W EA CRJ953-04538, REV IR DATED 07/05/16.SDR FDEA201607142445Skin Panel · dentedDENT ON EXTERNAL FUSELAGE BS 422 AND ABOVE STR 24R FURTHER DENT EVALUATION, IT WAS FOUND OUT OF LIMITS IAW SRM 53-00-01-1A, FIG 101, DETAIL III, A/Y=7.8. THE SKIN WAS REPAIRED IAW SRM 53-00-01-2R, FIG 201, REPAIR NR 7 AND SRM 51-40-02. MAJOR REPAIR, CAT-B.SDR WVER0714201600009Skin · dentedMULTIPLE SCRATCHES AND GOUGES TO FUSELAGE SKIN BETWEEN BS 1015 - 1047, STRINGERS 21-25R, CAUSED BY LOW PRESSURE AIR CAP.SDR WVER0714201600008Skin · dentedEXTERNAL FUSELAGE SKIN DENTED AT BS 565 BETWEEN STRINGERS 16 - 17L.SDR DALA2016071305329Skin · corrodedCORROSION FOUND ON THE AREA JUST AFT OF THE LAV SERVICE PANEL. CORROSION AT BS 720, BETWEEN STRINGERS S27-29R. CORROSION WAS ALSO DISCOVERED ON BOTH SIDES OF THE LOWER AFT BREAK RING. THE CORROSION WAS REMOVED IAW ER/A 548800-14, INSTALLED A SKIN DOUBLER ANDSDR DALA2016071305319Skin · corrodedCORROSION ON THE FUSELAGE SKIN AND PRESSURE DOME FRAME BS 1720, STRINGERS 27 - 29R. REPAIRED IAW ERA 548800 DTE.SDR AALA20160713006Skin · crackedDURING ACCOMPLISHMENT OF J1724AB_002, THE AFT FASTENER ROW, THIRD DOWN, HAS A CRACK INDICATION IN THE SKIN. REPAIRED THE SKIN IAW SB 737-53-1294 REV2 AND EA 261258.SDR C77A20160713001Skin · damagedDURING BASIC CHECK, INSPECTION FOUND THE AFT FUSELAGE LT LOWER SKIN PANEL TO HAVE A PROTRUDING DENT AND CRACK DAMAGE CAUSED BY IMPACT DAMAGE FROM A DOOR RIG BALANCE WEIGHT. THE DAMAGE IS LOCATED BETWEEN FRAMES 85 & 86 AND STRINGERS 25-26L. MAJOR REPAIR.SDR SWAA2016080254390Skin · crackedSKIN CRACKED AT BS 540, BETWEEN STRINGERS 22 - 23L. REPAIRED THE SKIN IAW EA.SDR CALA2016071495561Skin · damagedFUSELAGE SKIN ABOVE L1 DOOR DAMAGED. REPAIRED IAW SRM 53-00-01 REPAIR 4.SDR SWAA2016071353771Doubler · crackedGROUND POWER CONNECT DOOR CUTOUT CRACKED AT AFT FLANGE. REPAIRED IAW SRM.SDR FOTR20160712001Skin · crackedFUSELAGE SKIN CRACKED AT BS 509 I/B OF STRINGER 28R
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