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 ABXA20150524071Skin · crackedELT ANTENNA LOCATION, SKIN HAS HFEC CRACK INDICATION AT MID OTBD ANTENNA MOUNT HOLE. REPAIRED ELT ANTENNA SKIN AT MID OTBD ANTENNA MOUNT HOLE IAW EWO NR 57133-0000-0005 & SRM 53-00-01 REPAIR 14. SDR INFO, PN 146T1331-1, PART NAME SKIN, SN NSN, CRACKED .200, SDR SWAA2015060840462Post · crackedNUMBER 3 LT COCKPIT WINDOW POST CRACKED. REPAIRED POST IAW ACO.SDR SWAA2015060840461Post · crackedNUMBER 1 LT COCKPIT WINDOW POST CRACKED. REPAIRED POST IAW ACO.SDR A6WA201542776Skin · dentedLEFT AFT FUSELAGE SKIN HAS PROTRUDING DENT AT FS 712.00.SDR 7C7A201505230037Skin Panel · dentedDENT DAMAGE TO LT FUSELAGE SKIN PANEL 85330103, X600 - X606 STR 27P-28P. REPAIRED PERMANENT DENT ALLOWANCE IAW ECO 008.53-15.39SDR 7C7A201505230036Skin Panel · dentedDENT DAMAGE TO RT AFT FUSELAGE STA 581 STR 25S - 26S. REPAIRED WITH PERMANENT DENT ALLOWANCE IAW ECO 008.53-15.38SDR 7C7A201505230034Skin Panel · dentedDENT DAMAGE TO LT FUSELAGE SKIN PANEL 85320313. REPAIRED WITH PERMANENT DENT ALLOWANCE IAW ECO 008-53-15.41SDR 7C7A201505230033Skin Panel · dentedDENT DAMAGE TO RT FUSELAGE SKIN PANEL PN 85310533. REPAIRED WITH PERMANENT DENT ALLOWANCE IAW ECO 008.53-15.43SDR 7C7A201505230026Skin Panel · dentedDENT DAMAGE TO REAR FUSELAGE OUT OF LIMITS FOR SRM OR GENERIC REPAIRS. REPAIRED DENT IAW ECO 008.53-15.42SDR SWAA2015070641372Skin · corrodedAFT CARGO BAY ON INNER SURFACE OF OUTER SKIN CORRODED BETWEEN BS 727E+15 - 747, BL 0. REPAIRED SKIN IAW ER & EA.SDR SIMA20150522006Skin · crackedLEFT UPPER FUSELAGE SKIN CRACKED JUST AFT OF FRAME 75 & ABOVE STRINGER 2L, CRACK IS APPROX 3/4" IN LENGTH. EASI 8071 USED FREQ=400KHZ, V-GAIN=76.0, H-GAIN=64.0, LPF=100, 50-500KHZ PROBE. ACCOMPLISHED REPAIR TO LT UPPER FUSELAGE SKIN JUST AFT OF FRAME 75 & ABSDR SIMA20150522007Skin · crackedRIGHT UPPER FUSELAGE SKIN CRACKED JUST AFT OF FRAME 75 & ABOVE STRINGER 2R, CRACK IS APPROX 3/8" IN LENGTH. EASI 8071 USED FREQ=400KHZ, V-GAIN=76.0, H-GAIN=64.0, LPF=100, 50-500KHZ PROBE. ACCOMPLISHED REPAIR TO RT UPPER FUSELAGE SKIN CRACKED JUST AFT OF FRAMSDR SIMA20150522008Skin · crackedRIGHT UPPER FUSELAGE SKIN CRACKED JUST ON FRAME 75 AT FIRST FASTENER BELOW STRINGER 2R, CRACK IS APPROX 3/8" IN LENGTH. EASI 8071 USED FREQ=400KHZ, V-GAIN=76.0, H-GAIN=64.0, LPF=100, 50-500KHZ PROBE. ACCOMPLISHED REPAIR TO RT UPPER FUSELAGE SKIN CRACKED JUSTSDR WX0A2015060372629Skin · corrodedLOWER EXTERNAL FUSELAGE SKIN CORRODED AT STATION 807, LONGERON 29R. ACCOMPLISHED BLEND OUT REPAIR, LOCATED DRILLED & INSTALLED EXTERNAL DOUBLER BETWEEN LONGERON 28R & LONGERON 30, STATION 807 IAW EA 05-2015-024. WORK ACCOMPLISHED ON WO 251582 M301 ITEM 161, SDR DALA2015052303508Skin · crackedAIRCRAFT SKIN HAS 1.5" LONG CRACK NEAR BS 1494, OTBD OF LONGERON 3R. ANOTHER CRACK INBD OF LONGERON 4R. COMPLIED WITH PRI 536060-14, REV O AND ERA 536060-14, REV O.SDR WX0A2015052772617Skin · crackedNOSE LANDING GEAR BAY RT AFT DOORS, THE FUSELAGE SKIN IS CRACKED AT AFT HINGE AREA AT STATION 94.55 & R 28 POSITION. REPAIRED IAW SRM 53-O5 FIG-158. DOUBLER LENGTH 19"", WIDTH 5.5 & DEPTH .071. WORK ACCOMPLISHED ON WO 1011806-1200-0081 M301 ITEM 430.SDR AALA20150522011Skin · crackedFUSELAGE SKIN CRACKED AT STATION 1380 ABOVE LONGERON 14R. REPAIRED SKIN IAW SRM 53-01-00-001.SDR DALA2017081706280Skin · dentedDENT ON SKIN AT FRAME 10, TWO FEET FWD OF THE L1 DOOR. UNDER FLOOR LINE. DENT 3 INCHES BY 4 INCHES DEPTH.100, PERFORMED A PERMANENT REPAIR IAW SRM 53-00-11, PAR 4W, FIGURE 240.SDR ABXA20150521069Skin · chafedVERTICAL STABILIZER ACCESS 324AL FUSELAGE MOUNTED FWD & AFT FLANGE COMMON TO PANEL MATING SURFACE CHAFED. R & R SKIN FAIRING IAW SRM 51-40-05 & 51-40-02. APPLIED PROTECTIVE COATINGS IAW SRM 51-20-01. APPLIED TOP COAT IAW AMM 51-21-10. SDR INFO, CORRODED PNSDR SIMA20150521010Skin · crackedLEFT AFT FUSELAGE, SKIN CRACK AT FRAME 75 ABOVE STRINGER 2L. ACCOMPLISHED REPAIR LT AFT FUSELAGE AT FRAME 75 ABOVE STRINGER 2L IAW ERS-EM-53MR-1322. SEE WIPS & TASKS FOR DETAILS.SDR SWAA2015052840169Skin · crackedFUSELAGE SKIN BULKHEAD CHORD CRACKED AT BS 540, BETWEEN STRINGER 22L - 23L. REPAIRED SKIN IAW EA.SDR DALA2015052203442Skin · crackedSKIN CRACKED FROM FASTENER HOLE AT BS 1475 JUST INBD OF L1R. REPAIRED IAW SRM 53-30-01, FIG 16.SDR FDEA201505211615Skin · gougedAFT CARGO COMPARTMENT 1975 INTERNAL BETWEEN LONGERON 49L - 50L SKIN GOUGED IN NUMEROUS PLACES. INSTALLED DOUBLER IAW EA 8-5330-T0317549 P1.SDR FDEA201505211606Skin · dentedFUSELAGE EXTERNAL SKIN DENTED AT BS 743, 3" BELOW STRINGER 3L. ACCOMPLISHED EA F-5330-T0315854 PT 1. CROWN SKIN HAS A DENT WITH CREASE, FORM 8110-3 DATED 04 16 15 ATTACHED. THIS IS A CAT B REPAIR, MAJOR REPAIR.SDR SWAA2015070141310Skin · crackedAFT GALLEY DOOR CUTOUT LOWER FORWARD CORNER CRACKED. REPAIRED IAW SRM.SDR DALA2015052203448Skin · crackedAIRCRAFT SKIN HAS A CRACK NEAR BS 1494, OTBD OF LONGERON 3L. REPAIRED IAW SRM 53-00-01, FIG 6.SDR YENA20150520128Finger Doubler · corrodedON HEAVY MAINTENANCE CHECK, FOUND AFT CARGO DOORWAY FWD END FINGER DOUBLER HAS CORROSION. BLENDED, REWORKED, CORROSION DAMAGE AND HFEC PERFORMED. REPLACED AFFECTED FASTENERS. APPLIED SURFACE PROTECTION TO REWORKED AREA. ALL WORK ACCOMPLISHED IAW EA E15-509SDR CALA2015052100412Skin · dentedFUSELAGE SKIN AT STATION 193 BETWEEN STRINGER 20R & 21R HAS TOOLING DENT AROUND RIVET THAT WAS REPLACED. MEASURES 1" IN DIAMETER & .047 IN DEPTH. IAW SRM 53-00-01 AD 5 FIG 102 SH 6 IS OUT OF LIMITS Y RATIO 21.27. REPAIRED IAW SRM 53-00-01 REP 6.SDR DALA2015052103409Skin · damagedEXISTING REPAIR FOUND AT EXTERNAL FUSELAGE SKIN FWD NOSE AREA NEAR THE FWD NOSE JACKING POINT. THE EXISTING REPAIR HAD 1 FASTENER LOCATION ELONGATED THROUGH DOUBLER TRIPLER SKIN, INTERNAL DOUBLER AND FRAME. PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN 22" BELOSDR WVER201505200004Skin · arcedFUSELAGE SKIN SHOWS SIGNS OF MOVED METAL IN BAY BETWEEN BS 1031-1047, STR 4L-5L.SDR WVER020150520001Skin · arcedFUSELAGE SKIN PANEL SIX INCHES FORWARD OF VERTICAL STAB REAR SPAR SHOWS SIGNS OF MOVED METAL BETWEEN STRINGERS 4R-5R.SDR ASOA2015060513064Skin · corrodedUPPER FUSELAGE SKIN UNDER THE ADF ANTENNA HAS MULTIPLE AREAS OF CORROSION. REPAIRED IAW EA 32-2015-205.SDR ASAA2015051911867Skin · corrodedAFT PIT RT TRANSITION PANEL, UPPER & LOWER SURFACE SKIN CORRODED AT SEVERAL SPOTS. DOTTED. BS 767 - BS 792, RBL 25 - 35, STR 26R. ACFT GROUNDED. REMOVED DAMAGE FROM AFT PIT RT LWR MAIN SILL-SHIELD IAW SRM 53-00-53-1A-2 4.A.2. ORIGIONAL THICKNESS IS .050 IAWSDR DALA2015052003440Skin · crackedAIRCRAFT SKIN HAS TWO CRACKS NEAR BS 1494, OTBD OF LONGERON 3 AND INBD OF LONGERON 4. REPAIRED IAW ERA 536060-14.SDR CALA2015052100410Doubler · dentedLARGE DENT ON EXISTING FUSELAGE SKIN DOUBLER AT STATION 620 & STRINGER 16L. REMOVED DAMAGE FROM STATION 590 - 650, STRINGER 13L - 20L, REPAIRED IAW SRM.SDR V0XD20150521135Skin · gougedLOWER FUSELAGE SKIN HAS TWO GOUGES AT STRINGER 27, FS 985 UNDER AFT WING TO BODY FAIRINGS. BLENDED GOUGES IAW REO 670-53-00-014 DATED 7 JUN 05. BOTH GOUGED AREAS WITHIN LIMITS.SDR UIEA2015051900278Skin · gougedSKIN AT STATION 1180 RT SIDE HAS A GOUGE WHERE WING TO BODY FAIRING MOUNTS. REMOVED FASTENER, REWORKED AREA, INSTALLED NEW FASTENER AS REQUIRED & RESTORED FINISH IAW SRM GUIDELINES & SR 3-3261261089.SDR ASOA2015060413038Doubler · corrodedDOUBLER CORRODED AT BS 349, WL 79.50 AT RBL 42.5. FRAME FITTING HAS SEVERE INTERGRANULAR CORROSION. REMOVED 349 FITTING AND MATCH DRILLED NEW SERVICEABLE 349 FRAME FITTING IAW SRM 51-42-21-001-001-A01 SRM 51-40-11-001-001-A01. INSTALLED NEW SERVICVEABLE FITSDR FDEA201505181534Skin · dentedSKIN DENTED LBL 40, BS 288, & STRINGER 23 & 24L. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01A DET III. REPAIRED IAW SRM 53-00-01-2R. MAJOR REPAIR.SDR DALA2015051903345Skin · crackedACFT HAS SKIN CRACKED, BS 1494, TWO INCHES OTBD OF LONGERON 3 AND 4. REPAIRED.SDR KO0R201505180049Doubler · corrodedCORROSION ON INTERNAL SKIN DOUBLER BETWEEN STRINGER 52R & 51R STATION 1155 IN CTR E & E BAY.SDR WVER0518201500003Skin · damagedEXTERIOR SKIN HAS 2 SCRATCHES AND GOUGES BETWEEN STR 20 - 21R.SDR SIMA20150517006Skin · damagedHAIL DAMAGE EVENT. REPLACE RT CTR FUSELAGE I. R & R RT CFI IAW SRM 51-40-02, 51-40-03, 51-20-01, 51-20-03, 51-40-06, 53-21-01, ETN-EM-51-118 & ETN-EM-53-262R1.SDR SWAA2015052640029Skin · crackedL2 DOOR CUT OUT FWD LOWER CORNER SKIN CRACKED BETWEEN BS 967 - 951, STRINGER 17L. REPAIRED SKIN IAW SRM & EA.SDR DALA2015051803382Skin · corrodedDURING INSPECTION, FOUND CORROSION WITHIN WIFI AREA FRAME 25 TO 26 STRINGER 44. INSTALLED STR IAW SRM 53-21-13, C/W PRI/ERA 535082-14AD, REV O.SDR DALA2015051803381Skin · dentedDURING INSPECTION, DENT FOUND FRAME 21.+2 BETWEEN STRINGERS 23-24R.SDR CALA2015051800404Skin · damagedBELLY SKIN THICKNESS CHECK FROM STATION 1325 - 1420 FOUND DAMAGED & OUT OF LIMITS AT STATION 1330, STRINGER 30. DIMENSIONS GIVEN TO ENGINEERING MEASURED 0.0490. REPAIRED IAW SRM 53-00-01 REPAIR 2 CATEGORY B, SEE NR 4893220, 21, 22, 24, 26, 27, 28, 29, 489315SDR ASOA2015061713112Skin · corrodedCIRCUMFERENTIAL JOINT AT FS 280, STR 26L-26R HAS CORROSION. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. CSDR DALA2016111008458Access Panel · corrodedCORROSION ON COUNTERSINK AREA ON FUEL ACCESS PANEL 2302 ON THE CENTER FUEL TANK. THE CORROSION WAS REMOVED AND FOUND TO BE OUT LIMITS. THE ACCESS PANEL WAS REPLACED IAW SRM 51-22-2A.SDR ASAA2015051514492Skin · gougedLEFT FUSELAGE SKIN AT GROUND A/C DOOR CUTOUT IS GOUGED. ACFT GROUNDED. REPAIRED FUSELAGE SKIN AT AC DOOR CUTOUT IAW SRM 53-30-01-2R-2. THIS IS A CATEGORY B REPAIR WITH INSPECTION THRESHOLD OF 30,000 FLT CYCLES, FLT CYCLES AFTER REPAIR WITH INSPECTION INTERVA
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