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 DALA2016102707757Skin · corrodedAFT CARGO BILGE AREA, THE SKIN HAS CORROSION AROUND LAVATORY DUMP DUCT BS 1190 STRINGER 30. REPAIRED THE SKIN IAW ER/A 532884-14 REV O.SDR R61A201505300321Skin · dentedDURING HEAVY CHECK, MAINTENANCE C/W PERMANENT REPAIR OF DENT ON LT FUSELAGE IAW RD 8/4-53-6774 AND 8/4-53-5330. AIRCRAFT REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.SDR R61A201503200257Skin · dentedDURING HEAVY CHECK, FOUND DENT ON LT FUSELAGE X321 TO X341, STR 12P TO 13P FROM TEMP REPAIR RD 8/4-53-5330. MAINTENANCE INSTALLED A REPAIR DOUBLER IAW RD 8/4-53-6774, ISSUE 1.SDR SIMA20150320002Splice · damagedHAIL DAMAGE EVENT. CFI LT UPPER BUTT SPLICE AT FRAME 16, STRINGER 1L-1R GOUGED. PERFORMED REPAIR IAW ERS-EM-53MR-1174.SDR A6WA201542542Skin · damagedEXTERNAL AC POWER CONNECTOR RECEPTACLE SURROUND SKIN & LANDING DAMAGED.SDR AALA20150320016Skin · damagedSKIN DAMAGED AT FS 185 & LONGERON 26 LT. REPAIRED SKIN IAW SRM 53-04-03-001 & SRM 53-34-00-001 FIG 1 SHEETS 2 & 3 ITEM 27.SDR AALA20150320012Skin · damagedDAMAGE TO THE FUSELAGE SKIN AT STATION 867 & STRINGER 23 RT. DOUBLER REPAIR ACCOMPLISHED IAW EA B737-53-038979, DATED 19 MAR 15.SDR UHLA2015031900323Skin · looseDURING INSPECTION, LOOSE RIVETS WERE FOUND ON THE LT AND RT FUSELAGE SKIN AT FRAME 77 BETWEEN STRINGERS 3L-8L AND 3R-8R. THE SKIN WAS REPAIRED IAW ETD 2015-145027458, REV 8.SDR DALA2015031902265Skin · corrodedAFT CARGO COMPARTMENT FOUND BODY SKIN SURFACE CORROSION AT STA 1197+22 TO STA 1197+44 BETWEEN S-39L AND S-39R. REFER TO CPCP TASK NR 53-558-00. BODY SKIN SURFACE CORROSION REMOVED AFT CARGO COMPARTMENT AT STA 1197+22 TO STA 1197+44, BETWEEN S-39L AND S-39R. SDR DALA2015031902264Skin · corrodedAFT CARGO COMPARTMENT FOUND BODY SKIN SURFACE CORROSION AT STA 1197+44 TO STA 1197+66 BETWEEN S-39L AND S-39R. REFER TO CPCP TASK NR 53-558-00. BODY SKIN SURFACE CORROSION REMOVED AFT CARGO COMPARTMENT AT STA 1197+44 TO STA 1197+66 BETWEEN S-39L AND S-39R. SDR DALA2015031902263Skin · corrodedAFT CARGO COMPARTMENT FOUND BODY SKIN SURFACE CORROSION AT STA 1197+110 TO STA 1197+132 BETWEEN S-39L AND S-39R. REFER TO CPCP TASK NR :53-558-00. BODY SKIN SURFACE CORROSION REMOVED AFT CARGO COMPARTMENT AT STA 1197+110 TO STA 1197+132 BETWEEN S-39L AND S-39SDR DALA2015031902262Skin · corrodedAFT CARGO COMPARTMENT FOUND BODY SKIN SURFACE CORROSION AT STA 1197+88 TO STA 1197+100 BETWEEN S-39L AND S-39R. REFER TO CPCP TASK NR:53-558-00. CORROSION REMOVED AFT CARGO COMPARTMENT AT STA 1197+88 TO STA 1197+100 BETWEEN S-39L AND S-39R. THE REWORKED AREA SDR DALA2015031902261Skin · corrodedAFT CARGO COMPARTMENT FOUND BODY SKIN SURFACE CORROSION AT STA 1197+132 TO STA 1197+154 BETWEEN S-39L AND S-39R. BODY SKIN SURFACE CORROSION REMOVED AFT CARGO COMPARTMENT AT STA 1197+132 TO STA 1197+154 BETWEEN S-39L AND S-39R. THE REWORKED AREA CLEAN UP DEPSDR DALA2015032002256Skin · damagedDURING NDT INSPECTION A DISCREPANT AREA WAS FOUND, DOUBLER REPAIR ON FUSELAGE SKIN AT BS 1418 AND BETWEEN LONG 1-3L. DOUBLER REPAIR IS ATTENDED WITH ER/A 496150-14, REV ORIGINAL AND WILL BE INSPECTED PRIOR TO REACHING 56.250 TOTAL CYCLES.SDR SWAA2015032337732Post · crackedLEFT NR 3 WINDOW FRAME E - F POST NR 8 FASTENER HOLE CRACKED, FWD & AFT SIDE OF HOLE. REPAIRED POST IAW EA.SDR SWAA2015032337731Post · crackedRIGHT NR 3 WINDOW FRAME E - F POST NR 8 FASTENER HOLE CRACKED, FWD & AFT SIDE OF HOLE. REPAIRED POST IAW EA.SDR SWAA2015032337730Post · crackedRIGHT NR 3 WINDOW FRAME E - F POST NR 7 FASTENER HOLE CRACKED, AFT SIDE OF HOLE. REPAIRED POST IAW EA.SDR SWAA2015032037662Post · crackedRIGHT NR 3 WINDOW FRAME E - F POST NR 6 FASTENER HOLE CRACKED, AFT SIDE OF HOLE. REPAIRED POST IAW EA.SDR SWAA2015032037661Post · crackedRIGHT NR 3 WINDOW FRAME E - F POST NR 5 FASTENER HOLE CRACKED, AFT SIDE OF HOLE. REPAIRED POST IAW EA.SDR LR7A2015031800546Skin · crackedDURING SCHEDULED C-11 CHECK WHILE PERFORMING SB 382-57-85 R2 APPENDIX A NDI AND SP-141 NDI, FOUND 2 CRACKS EVIDENT ON THE RT CENTER WING LOWER PLANK LAYER AT FS596, CWS59R WL256 AND 1 CRACK EVIDENT ON THE RT CTR WING REAR BEAM LOWER CAP LAYER AT FS596 CWS59R. SDR LR7A2015031800542Skin · crackedDURING SCHEDULED C-11 CHECK WHILE PERFORMING SB 382-57-85, R2 APPENDIX D NDI AND SB 382-57-86 R1, FOUND 2 CRACKS EVIDENT AT RT CENTER WING LOWER PANEL NR 1 COMMON TO THE RT ATTACH ANGLE AT FS518, CWS72R, WL256. REPAIRED IAW LAC MEA 382-57-14-053. NR 2261.SDR LR7A2015031800541Skin · crackedDURING SCHEDULED C-11 CHECK WHILE PERFORMING SB 382-57-85 R2 APPENDIX D NDI AND SB 382-57-86 R1, FOUND 1 CRACK EVIDENT AT LT CENTER WING LOWER PANEL NR 1 COMMON TO THE LT ATTACH ANGLE AT FS518, CWS72L, WL256. REPAIRED IAW LAC MEA 382-57-14-052. NR 2260.SDR LR7A2015031800540Skin · crackedDURING SCHEDULED C-11 CHECK, WHILE PERFORMING SB 382-57-85, R2 APPENDIX B NDI, FOUND 1 CRACKED FASTENER HOLE EVIDENT ON RT CENTER WING LOWER NR 1 PANEL AT FS538, CWS 178R, WL 256. REPAIRED IAW LAC MEA 382-57-14-051, NR 2259.SDR LR7A2015031800533Skin · crackedDURING SCHEDULED C-11 CHECK, WHILE PERFORMING SB 382-57-85 R2 APPENDIX A NDI, FOUND THE LT CENTER WING LOWER SURFACE PANEL UNDER THE LT WING ATTACH ANGLE HAD 1 CRACK EVIDENT; FS 570, CWS 60L, WL 256. REPAIRED IAW LAC MEA 382-57-14-040, NR 2234.SDR LR7A2015031800532Skin · crackedDURING SCHEDULED C-11 CHECK, FOUND THE LT FWD FUSELAGE EXTERIOR SKIN HAD CRACKED AT THE BATTERY PANEL CUTOUT ACCESS AT THE REAR UPPER CORNER; FS 155, WL 180, LBL 55. REPAIRED IAW SMP 583, SRM FIG 51-140-12, NR 2232, PSE 53-30-08, AD 2012-06-09.SDR LR7A2015031800528Skin · corrodedDURING SCHEDULED C-11 CHECK, FOUND THE RT CENTER WING LOWER PLANKS HAD SURFACE CORROSION AROUND PIN RIVET HEADS AT BEHIND NR 3 ENGINE EXHAUST, ABOVE NACELLE; FS 576 TO FS 590, CWS 188R TO CWS 206R, WL 256. REPAIRED IAW LAC MEA 382-57-14-056, NR 2199.SDR CALA2015031800174Skin · crackedEVIDENCE OF CRACKS & CORROSION FOUND AT AFT LT EXHAUST FAN VENT TUBE TO SKIN OPENING AT APPROX STATION 907 FOR VACUUM BLOWER LAVATORY VENT. FUSE SKIN IAW IPC 38-32-06-01 LOG PAGE 732033 FOR SKIN REPAIRS & ECRA 5330-05097. REF LOG PAGE 473203 FOR LAVATORY TANSDR ASAA2015031711252Skin · dentedFORWARD CARGO DOOR CUT-OUT 12" FROM LOWER AFT CORNER SKIN DENTED. ACFT GROUNDED. ACCOMPLISHED REPAIR OF FUSELAGE SKIN AT FWD CARGO DOOR CUTOUT LOWER AFT CORNER IAW SRM 53-00-01-22-24. REMOVED DOT J702.SDR EE4Y20150119Skin · dentedLOWER FUSELAGE FROM BS 1000 TO BS 1006 BETWEEN STR 20RT AND STR 24RT SKIN PANEL WITH DENT, CREASE AND SCRIBE LINE.SDR SIMA20150317009Skin · damagedREAR FUSELAGE 1 LOWER SKIN DENT & CREASE. FABRICATED & INSTALLED FILLER & DOUBLER IAW ERS-53MR-1123.SDR AALA20150317028Skin · damagedFUSELAGE SKIN IS DAMAGED BELOW THE FWD CARGO DOOR OPENING BETWEEN STATIONS 468 - 508 & BETWEEN STRINGERS 26RT & 28RT. ACCOMPLISHED PERMANENT REPAIR IAW EA B737-53-038934 DATED 17 MAR 15.SDR SWAA2015032037670Skin · crackedSKIN CRACKED AT BS 540, STRINGER 22R. REPAIRED SKIN IAW ACO.SDR AALA20150317025Skin · corrodedCORROSION BETWEEN FUSELAGE SKIN & STRINGER 39 RT AT STATION 654+70. ACCOMPLISHED SKIN REPAIR IAW SRM 53-00-01.SDR DALA2015031802231Skin · unknownDURING INSPECTION, FOUND SKIN IN THE AFT CARGO COMPARTMENT BETWEEN FR 55 & FR56. ACCOMPLISHED REPAIR IAW SRM 53-00-11, FIG 222.SDR EE4Y20150118Skin · dentedLOWER FUSELAGE, BS 100, STR 24LT SKIN WITH SCRIBE LINE, AND BS 1006 BETWEEN STR 23LT AND 24LT SKIN WITH DENT.SDR SWIA201540933Skin · damagedLEFT SIDE EXTERNAL FUSELAGE SKIN HAS A CREASE AT BS 605 BETWEEN STR 21 - 22L. REPAIRED IAW EA.SDR DALA2015031702279Skin · crackedFUSELAGE SKIN CRACKED AT STA 1475, INBD OF L1R . CUT OUT DAMAGED AREA. FABRICATED AND INSTALLED DOUBLER AND TRIPLER REPAIR IAW SRM 53-30-01, FIG 16.SDR FDEA201503160945Skin · gougedLOWER FUSELAGE SKIN, STATION 507 - 508, STRINGER 27 - 28R, HAS GOUGE. ACCOMPLISHED IAW EA F-5330-T0315849 PT 1. CAT B REPAIR IAW FORM 8100-9 DATED 12 MAR 2015. 1ST & 2ND STAGE APPROVAL. DTA PENDING DUE PRIOR TO 60,100 FLIGHT CYCLES.SDR CALA2015031700169Skin · crackedFUSELAGE STATION 540 SKIN AT STRINGER 22L & 23L, TWO CRACKS AT CHORD HOLES & ONE AT SKIN HOLE. PERFORMED PART 1 INTERIM REPAIR, INSTALLED FREEZE PLUG HOLE A & OPENING HOLE TO .2455 IAW ECRA 5310-06438 REV A. INITIATE DIP TO ACCOMPLISH A PERMANENT REPAIR ON OSDR WVER0316201592506Skin · chafedFUSELAGE SKIN AT FS 913.00 AT STR 27 IS CHAFED APPROXIMATELY 1.5" LONG X .005" DEEP.SDR QXEA2015040600177Skin · corrodedLT FUSELAGE INNER SKIN HAS CORROSION AT AFT PAX DOOR CUTOUT BETWEEN STA X669.3 TO STA 697.6. REMOVED 4 NUTPLATES FOR ACCESS REF SRM 51-42-05 STEP 4E. INSTALLED 4 EA NUTPLATES TO INNER SKIN AT AFT PAX DOOR REF SRM 51-42-05, REPAIR-01. REMOVED CORROSION AT LT FSDR SWIA201540980Skin · corrodedFUSELAGE INTERIOR SKIN AT AVIONICS DOOR CUT-OUT, HAS CORROSION AROUND PERIMETER OF CUTOUT, C-CHECK RO 4/2/15. BLENDED OUT CORROSION FROM FUSELAGE AREA AROUND AVIONICS DOOR CUTOUT INNER SKIN DOUBLER REF 200. REO ORIGINAL THICKNESS OF FUSELAGE INTERIOR SKIN AVISDR SWIA201540976Skin · dentedRIGHT FUSELAGE APPROXIMATELY BETWEEN STG R1 & 2 AND FS 816.25 & FS 830.00 EXTERIOR SKIN HAS DENT. C-CHECK, RO 4/2/15, BLENDED OUT SCRATCHES ON DENT AND DRESSED OUT DENT, RT FUSELAGE BETWEEN FS 816.25 AND FS830.00, IAW STS EA .SDR SWAA2015040238082Skin · crackedL2 DOOR CUT OUT CRACKED AT BS 948+10, STRINGER 17L, FWD LOWER CORNER. REPAIRED CUT OUT IAW EA.SDR AALA20150320001Skin · damagedSKIN DAMAGE TO AFT FUSELAGE AT APPROX STATION 907 & STRINGER 22 RT. REPAIR ACCOMPLISHED IAW EA 53-03028, SRM 53-00-03-2R & 53-00-01-2R.SDR DALA2015031602218Skin · crackedLOWER FORWARD FASTENER HOLE HAS CRACK INDICATION IN SKIN ONLY. COMPLIED WITH ERA 533651-14AD REV ORIGINAL. PRI 533651-14AD, LP 1862494.SDR DALA2015031602151Skin · damagedDURING NDT INSPECTION A DISCREPANT AREA WAS FOUND, DOUBLER REPAIR WITH ER/A 473483-14AD ON FUSELAGE SKIN AT BS 1418 BETWEEN LONGERONS 1-3R.SDR WVER2015031500001Skin · gougedFS 906 HAS A GOUGE .250 DIAMETER X .015 DEEP.SDR FDEA201503140925Skin · corrodedAFT FUSELAGE COMPARTMENT RT SIDE, FUSELAGE SKIN HAS CORROSION & EXFOLIATION LOCATED AT STATION 2007 - 2015 BETWEEN LONGERON R12 & R13. FUSELAGE REPAIR DOUBLERS IAW SRM 53-70-01 FIG 201 REPAIR 3.SDR FDEA201503140924Skin · corrodedAFT FUSELAGE RT SIDE, FUSELAGE SKIN FOR HORIZONTAL STAB FAIRING PANEL 347AF DISPLAYS EXTERNAL & INTERNAL CORROSION & OR EXFOLIATION AT STATION 2007 - 2033, LONGERON 5R - 15R. INTERNAL CORROSION CAN BE VIEWED FROM INSIDE RT UPPER AFT FUSELAGE COMPARTMENT ZON
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