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 IXXA20161130153Skin · corrodedCORROSION ON SKIN AT STRINGER 36 - 37R AND BS 588 - 610. REPAIRED IAW SRM 53-00-01, REPAIR 14 PAGE 201 STEPS 1-17.SDR SWIA201642733Skin · dentedDENT FOUND ON SKIN LT SIDE AFT FUSELAGE JUST AFT OF CARGO COMPARTMENT DOOR. REPAIRED DENT IAW EA.SDR SWIA201642732Skin · dentedDENT ON RIGHT FUSELAGE SKIN JUST FWD OF AFT EQUIPMENT ACCESS . REPAIRED IAW EA.SDR SWAA2016100308343Skin · crackedGROUND POWER RECEPTACLE ACCESS DOOR MATING FLANGE CRACKED. REPAIRED FLANGE PER SRM.SDR QMLA2016092916112Skin · crackedWHILE CONDUCTING INSPECTION OF THE ENGINE FIREWALLS. WHEN REMOVING THE NR 1 INLET CHANNEL (PN 713M2077101)FOR INSPECTION AND SAW THAT IT WORN A HOLE INTO THE SKIN OF THE DRIVE SHAFT TUNNEL. WHILE CLEANING AND INSPECTING THE DAMAGE AREA FOUND THAT THE SAME SKSDR SWAA2016102409016Skin · crackedSKIN CRACKED AT BS 540, STR 22R. REPAIRED SKIN IAW EA.SDR SWAA2016102108940Skin · crackedFUSELAGE SKIN CRACKED AT BS 540, STRINGER 22L. REPAIRED SKIN IAW EA.SDR ASAA2016092818403Bear Strap · crackedL1 DOOR LOWER HINGE CUT OUT SHOWS CRACK INDICATION IN HOLE. GROUNDED, YES. CRACKS FOUND AT UPPER AND LOWER HINGE CUT OUTS REPAIR OF BOTH CRACKS TO BE REPAIRED ON MIG5 OK33947 W/O 1013489 2000/0110.SDR ASAA2016092818402Bear Strap · crackedL1 DOOR UPPER HINGE CUT OUT SHOWS CRACK INDICATION IN HOLE MARKED. GROUNDED, YES. REPAIRED CRACKS AT UPPER AND LOWER HINGE CUT OUTS IAW EA 400-53EA-17876. THIS IS A CATEGORY B REPAIR WITH STAGE 1 APPROVAL 2ND AND 3RD STAGE DT DATA TO DEMONSTRATE COMPLIANCE SDR SWAA2016101908910Skin · crackedSKIN CRACKED AT BS 540, STR 22L. REPAIRED SKIN IAW EA.SDR DALA2016100407027Skin · damagedLIGHTING STRIKE AT BS 1430 STRINGER 25L (SKIN DAMAGE AWAY FROM A FASTNER). CORRECTIVE ACTION: LIGHTING STRIKE WAS AWAY FROM A FASTNER. REPAIRED DAMAGE PER SRM.SDR DALA2016100307022Skin · damagedLIGHTNING STRIKE AT BS 751 STRINGER 26L ( SKIN DAMAGE AWAY FROM A FASTNER). LIGHTING STRIKE WAS AWAY FROM A FASTNER. REPAIRED DAMAGE PER SRM.SDR DALA2016100307021Skin · damagedLIGHTNING STRIKE AT STA 732 STRINGER 26 (SKIN DAMAGE AWAY FROM A FASTNER. CORRECTIVE ACTION:LIGHTNING STRIKE WAS AWAY FROM A FASTNER LOCATION. REPAIRED DAMAGE PER SRM. (2701338)SDR DALA2016100307020Skin · damagedLIGHTING STRIKE AT STA 1387 STRINGER 25L. LIGHTING STRIKE WAS AWAY FROM A FASTENER. REPAIRED DAMAGE PER SRM. (2701342)SDR DALA2016100106989Skin · dentedDENT AT STA 475, LONGERON 7, APPROX .75" X .- 5", .025" BELOW SKIN SURFACE. REPAIRED PER ERA 551073-14 REV ORIGINAL.SDR DALA2016100106988Skin · dentedDENT AT STA 570, LONGERON 7, APPROX 1.25" X .75", .029" BELOW SKIN SURFACE. REPAIRED PER ER/A 551073-14 REV ORIGINAL.SDR DALA2016100106987Skin · dentedDENT AT STA 416, LONGERON 7, APPROX 1.5" X 1.25", .031" BELOW SKIN. REPAIRED PER ERA 551073-14 REV ORIGINAL.SDR QXEA2016092900627Skin · damagedEXTERNAL FUSELAGE BELLY SKIN HAS "BURN MARKS" FROM FS (-) 39.00 TO FS (+) 1.00, BETWEEN STGRS 32L AND 31L (6 PLACES) MARKED. PERFORMED Q400 SRM REPAIR 53-20-31 REPAIR-03 REF Q400 SRM 51-42-05, 51-23-00, 51-25-10. C/W ET INSP REF Q400 NDTM 51-00-06 NO DEFECTS NSDR QXEA2016092900625Skin · damagedEXTERNAL FUSELAGE BELLY SKIN HAS "BURN MARKS" FROM FS (+) 1.00 TO FS 71.200, BETWEEN STRGS 31L AND 30L (5 PLACES) MARKED. REMOVED DAMAGE ON EXTERNAL FUSE BELLY SKIN AT 5 PLACES FROM FS X 31.2 TO FS X 71.200 BTWN STR 31L AND STR 32L REF Q400 SRM 53-00-00-02-08 SDR DALA2016092906945Skin · dentedDENT AT FRAME BS 294, 3.5" ABOVE LONGERON #9, APROX 1.25" X 1.0", .033" BELOW SURFACE SKIN. INSTALLED REPAIR PARTS IAW ERA 551073-14 REV ORIGINAL.SDR DALA2016092906944Skin · dentedDENT AT BS 370, LONGERON 8, APROX 1.25' X .375", .017" BELOW SKIN SURFACE. REPAIR PER ER/A 551073-14 REV ORIG.SDR DALA2016092906943Skin · dentedDENT AT BS 416, LONGERON 7, APROX 1.5" X 1.25", .031" BELOW SKIN SURFACE. REPAIRED PER ERA 551073-14 REV. ORIGINAL.SDR DALA2016092906942Skin · dentedDENT AT BS 570, LONGERON 7, APROX 1.25" X .75", .029" BELOW SKIN SURFACE. REPAIRED PER ER/A 551073-14 REV. ORIGINAL.SDR DALA2016092906941Skin · dentedDENT AT BS 475, LONGERON #7, APROX .75" X .- 5", .025" BELOW SKIN SURFACE. REPAIRED PER ERA 551073-14 REV. A.SDR DALA2016092906940Skin · dentedDENT AT FRAME BS 275 , 2" ABOVE LONGERON #9, APROX .5" X .75", .018" BELOW SURFACE SKIN. REPAIRED IAW SRM 53-04-02SDR FDEA201609283384Skin · damagedVERTICAL SCRATCHES ON EXTERNAL SURFACE OF THE FUSELAGE SKIN AT BS 1395 - 1404.5, JUST BELOW STRINGER 4R. TWO SCRATCHES AT BS 1396 AND THREE AT BS 1404. REPAIRED IAW EA F-5330-T0328332 PART 1.SDR DALA2016092806920Skin · dentedDENT AT STA 370, LONGERON NR 8, APPROXIMATELY 1.25" X .375", .017" BELOW SKIN SURFACE. REPAIR IAW ER/A 551073-14, REV ORIG.SDR DALA2016092806919Skin · dentedDENT AT FRAME STA 294, 3.5" ABOVE LONGERON NR 9, APPROXIMATELY 1.25" X 1.0", .033" BELOW SURFACE SKIN. INSTALLED REPAIR PARTS IAW ERA 551073-14, REV ORIGINAL.SDR DALA2016092806918Skin · dentedDENT AT FRAME STA 275 , 2" ABOVE LONGERON NR 9, APPROXIMATELY .5" X .75", .018" BELOW SURFACE SKIN. REPAIRED IAW SRM 53-04-02 REF ER/A 551073-14, REV ORIGINAL.SDR DALA2018021300886Lap Joint · damagedFUSLAGE SKIN LAP SPLICE DAMAGED, STRINGER 14L, BS 1701. REPAIRED THE SKIN IAW ERA 551173-14AD, REV A. SECTION 2.SDR DALA2017092607123Skin · damagedWHILE IN DTW FOR SCHEDULED MOD, DAL MTC IS ACCOMPLISHING REMOVAL OF THE AFT ATG ANTENNA PER GOGO DWG P19112-24406, REV C. UPON REMOVAL OF THE DOUBLER, MTC REPORTED MULTIPLE EXISTING HOLES WERE FOUND TO BE ELONGATED. MAINTENANCE REPAIRED PER ERA 551111-14.SDR 4AER20161014008Skin · corrodedEXTERNAL FUSELAGE SKIN FROM BS 907-1016 & STRINGERS 25L-25R HAS CORROSION.SDR SIMA20160927006Filler · corrodedDURING HMBV INSPECTION, QA FOUND PREVIOUS REPAIR FILLER BETWEEN FR 64 - 65, STGR 21L-21R CORRODED. AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED PREVIOUS REPAIR CORRODED FILLER IAW SRM 53-31-01RE ITEM 2. AIRCRAFT WILL BE RETURNED TO SERVICE.SDR QXEA2016092900626Skin · damagedLIGHTNING STRIKE OF FUSELAGE BELLY SKIN APPROX 3.5" FWD OF X 321.000 BETWEEN. DAMAGE TO FUSELAGE SKIN 3.5" FWD OF X 321.00 STR 31L TO 32L BLENDED/REMOVED REF Q400 SRM 53-00-00 REPAIR-02. MINIMUM THICKNESS AFTER BLENDING .055" ORIGINAL THICKNESS .055" REF BOMBASDR QXEA2016092800622Skin · damagedFUSELAGE BELLY SKIN HAS BURNS FROM BS 258 - 301, BETWEEN STRINGERS 30 & 32L. REPAIRED IAW SRM 53-00-00-02-08, SRM 53-00-00-01-01, SRM 51-42-05-02-01. PERFORMED ET & UT INSPECTIONS IAW NDTM 51-00-06 AND 51-00-04. NO DEFECTS NOTED. FOUND TO BE WITHIN LIMITS SDR QXEA2016092800621Skin · damagedFUSELAGE BELLY SKIN BURNED FROM BS 71.2 - 156 BETWEEN STRINGERS 30 AND 31L . REMOVED DAMAGE IAW SRM 53-00-00-02-08, SRM 53-00-00-01-01. COMPLIED WITH ET INSPECTION IAW NDTM 51-00-06. NO DEFECTS NOTED. NDT SHOWS NO DEFECTS. REPAIR IS WITHIN ALLOWABLE LIMITS SDR QXEA2016092800620Skin · damagedLIGHTNING STRIKE ON FUSELAGE BELLY SKIN TWO INCHES FWD OF BS 388 AT RIVET HEAD IN STRINGER 30. REMOVED THE RIVET, UPSIZED HOLE TO NUMBER 10 IAW SRM 53-00-00 DAMAGE-01, 51-42-05. INSTALLED A NEW RIVET IAW SRM 53-00-00 AND 51-42-05-02-01 (01-01). COMPLIED WITHSDR QXEA2016092800619Skin · damagedLIGHTNING STRIKE ON FUSELAGE BELLY SKIN 1.5 INCHES FWD OF BS 439.5 AT RIVET HEAD IN STRINGER 29. REMOVED AND REPLACED THE FASTENER IAW SRM 51-42-05, AND SRM 51-42-05-02-01.SDR HEER20160927243Skin · corrodedFORWARD ROOF SKIN WAS FOUND TO BE CORRODED COMMON TO LT & RT SKYLIGHT INSTALLATIONS. REPAIRED.SDR DALA2016092706896Skin · dentedDENT AT STA 416, LONGERON- NR 7, APROX 1.5" X 1.25", .031" BELOW SKIN SURFACE. REPAIRED IAW PRI 551073-14, REV 0 AND ERA 551073-14, REV ORIGINAL.SDR DALA2016092706895Skin · dentedDENT AT STA 662, LONGERON NR 6, APPROXIMATELY 1.5" X 1.25", .018 BELOW SKIN SURFACE. REPAIRED IAW PRI 551073-14, REV 0 AND ERA 551073-14, REV ORIGINAL.SDR DALA2016092706894Skin · dentedDENT AT STA 570, LONGERON NR 7, APPROXIMATELY 1.25" X .75", .029" BELOW SKIN SURFACE. REPAIR IAW PRI 551073-14, REV 0 AND ERA 551073-14, REV ORIGINAL.SDR DALA2016092706893Skin · dentedDENT AT FRAME STA 636, 1.75" BELOW LONGERON NR 6, APPROXIMATELY 1.0" X 1.125", .019 BELOW SKIN SURFACE. REPAIRED IAW PRI 551073-14 REV 0 AND ERA 551073-14, REV ORIGINAL.SDR DALA2016092706892Skin · dentedDENT AT STA 601, 3.5" ABOVE LONGERON NR 7, APPROXIMATELY 1.125 X 075", .015 BELOW SKIN SURFACE. REPAIR COMPLETED IAW PRI 551073-14, REV 0, AND ER/A 551073-14, REV ORIGINAL.SDR DALA2016092706891Skin · dentedDENT AT STA 475, LONGERON NR 7, APPROXIMATELY .75" X .-5", .025" BELOW SKIN SURFACE. REPAIRED IAW PRI 551073-14 REV 0 AND ERA 551073-14, REV ORIGINAL.SDR WVER2016092791306Doubler · chafedFUSELAGE LOWER SKIN BETWEEN FS 913.00 AND FS 927.00 HAS 2 SCREW CHAFES ON PREVIOUS REPAIR DOUBLER AT STR 27.SDR FDEA201609263366Skin · dentedFUSELAGE SKIN DENTED AT BS 1398 BETWEEN STRINGERS 34-35L. COMPLIED WITH EA H-5330-T0328464 P1. FABRICATED A REPAIR DOUBLER AND FILLER. INSTALLED REPAIR.SDR K11A20161416001Skin · crackedFUSELAGE SKIN BS 266 LONGERON 5L HAS EVIDENCE OF A CRACKSDR CALA2016092795778Skin · dentedSMALL DENT FOUND ON RT FUSELAGE, ONE FOOT ABOVE UPPER WINDOW LINE & 7 WINDOWS AFT OF OVERWING EXIT. DENT WAS OUT OF LIMITS IAW SRM 53-41- 11 FIG.101. FABRICATED & INSTALLED A REPAIR DOUBLER IAW SRM 53-00-11 FIG 231, PG 503-504.SDR CALA2016092795777Skin · dentedEXTERIOR FUSELAGE SKIN DENTED AT THREE PLACES BETWEEN FRAMES 23 & 24 AND STRINGERS 23 & 24L. FOUND TO BE OUT OF LIMITS IAW SRM 53-11-11 FIG.115. FABRICATED AND INSTALLED A REPAIR DOUBLER IAW SRM 53-00-11 FIG.232 PG. 505-506.
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