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 SWIA201744236Skin · damagedSKIN PANEL DAMAGED. BLENDED SKIN PANEL IAW REO.SDR SWIA201744234Skin · damagedSKIN PANEL DAMAGED. BLENDED SKIN PANEL IAW REO.SDR SWIA201744233Skin · damagedSKIN PANEL DAMAGED. BLENDED SKIN PANEL IAW REO.SDR SWIA201744232Skin · damagedSKIN PANEL DAMAGED. BLENDED SKIN PANEL IAW REO.SDR DALA2017121808793Skin · corrodedCORROSION ON INTERNAL SKIN AT FRAME 66, STRINGER 32R IN THE AFT CARGO BAY. PERFORMED A PERMANENT REPAIR IAW PRI 563236-14, REV 0, AND ERA 563236-14 AD REV ORIGINAL.SDR SWAA2022020753172Skin · damaged47D) FASTENER AND SKIN DAMAGED AT STA 247. 2IN. ABOVE L/H NLG W/W. / CHEMICALLY REMOVED PAINT AND INSPECTED DAMAGE WITH 10X MAGNIFIER. REPAIRED DAMAGE PER SRM 53-00-01-2R-41 AND 53-00-01-1A-1 SURFACE BLENDING. DAMAGE DIMENSIONS LENGTH 0.040??? X WIDTH 0.040???SDR SWAA2022020753170Skin · damaged47B) FASTENER AND SKIN DAMAGED AT STA 241. 2IN. ABOVE L/H NLG W/W. / CHEMICALLY REMOVED PAINT AND INSPECTED DAMAGE WITH 10X MAGNIFIER. REPAIRED DAMAGE PER SRM 53-00-01-2R-41 AND 53-00-01-1A-1 SURFACE BLENDING. DAMAGE DIMENSIONS LENGTH 0.050??? X WIDTH 0.050???SDR SWAA2022020753171Skin · damaged47C) FASTENER AND SKIN DAMAGED AT STA 242. 2IN. ABOVE L/H NLG W/W. / CHEMICALLY REMOVED PAINT AND INSPECTED DAMAGE WITH 10X MAGNIFIER. REPAIRED DAMAGE PER SRM 53-00-01-2R-41 AND 53-00-01-1A-1 SURFACE BLENDING. DAMAGE DIMENSIONS LENGTH 0.040??? X WIDTH 0.050???SDR SWAA2022020753169Skin · damaged(47A) FASTENER AND SKIN DAMAGED AT STA 240. 2IN. ABOVE L/H NLG W/W. / CHEMICALLY REMOVED PAINT AND INSPECTED DAMAGE WITH 10X MAGNIFIER. REPAIRED DAMAGE PER SRM 53-00-01-2R-41 AND 53-00-01-1A-1 SURFACE BLENDING. DAMAGE DIMENSIONS LENGTH 0.050??? X WIDTH 0.050??SDR CALA2017121504462Skin · damagedDAMAGED FASTENER HOLEAT STA 259.5 @ STR 19R FUSELAGE SKIN, BULKHEAD CHORD AND SPLICE STRAP INTERIM REPAIR ACCOMPLISHED AT STA 259.5 STR 19R IAW ECRA 5330-06275.SDR R61A201712141017Skin · corrodedCORROSION ON THE LAV SERVICE DOOR CUTOUT WASTE BOX, EXTERNAL SKIN AREA, INNER DOUBLER & CENTER FUSELAGE III, STRINGER 28R BETWEEN FRAMES 86 & 87 AND STRINGERS 27R AND 28R. REPAIRED IAW ETD2017-170-112028, ETD2017-170-111343A, SRM 51-41-01, 51-43-04, 51-41-0SDR JGVR20171219003Skin · corrodedAIRCRAFT DATA TAG ON LOWER TAIL HAS APPROX 6 AREAS OF CORROSION AROUND PERIMETER OF AIRCRAFT DATA TAG. REMOVED AIRCRAFT DATA TAG LOCATED ON LOWER TAIL. MECHANICALLY REMOVED AREAS OF CORROSION LOCATED UNDERNEATH AIRCRAFT DATA TAG ON SKINS P/N 692029-1 AND 69120SDR DALA2017121508689Skin · crackedCRACK ON FUSELAGE SKIN AROUND AFT HINGE OF LEFT HAND AFT NOSE LANDING GEAR DOOR. REPAIRED I AW SRM 53-30-01.SDR DALA2017121508629Skin · bulgedSKIN LAP END IS BULGED, FS 1582, JUST AFT OF LAV VACUUM O/B DUMP PORT. C/W ERA 563704-14SDR DALA2017121408598Skin · dentedFUSELAGE / SKIN / FS STA 291 - 307 / LONG. 23L - 25L / DENT REPAIR - DTA-INFORM ENGINEERING. ERA273604-14 REV B FS STA 291-307/LONG, 23L-25L/DENT REPAIR TIME LIMITED. THIS LP IS TO BE TERMINATED. THE DTA HAS BEEN ACCOMPLISHED AND REQUIRES REPAIR REPLACEMENT PRSDR JR2R20171213037Skin · corrodedFUSELAGE SKIN AT AFT LAV SERVICE DOOR LWR FWD CORNER HAS BULGING CORROSION. REPAIRED FUSELAGE SKIN IAW STS EA 30-2017-171.SDR SWAA2018012519317Skin · crackedLOWER BULKHEAD SKIN CHORD CRACKED AT BS 540, STR 22R. REPAIRED SKIN PER ER & EA.SDR SWAA2017122118589Skin · damagedFORWARD AIRCRAFT CREASE LOWER NOSE AREA CREASED AT BS 196.5+0, RBL 0 + 2.3. REPAIRED SKIN PER EA.SDR DALA2017121208534Skin · damagedSTATIC DISCHARGES AT STATION 54 STR 2L. INSTALLED MS90354U5 AND CONICAL WASHERS PER SRM 53-21-11 PB201. LP 0334795SDR DALA2017121208533Skin · damagedSTATIC DISCHARGES AT STATION 53.2 STR 4-5L. INSTALLED MS90354U5 AND CONICAL WASHERS PER SRM 53-21-11 PB201. LP 0334733SDR DALA2017121208532Skin · damagedSTATIC DISCHARGES AT STATION 46 STR 5L. INSTALLED MS90354U6 AND CONICAL WASHERS PER SRM 53-21-11 PB201. LP 0334721SDR DALA2017121208531Skin · damagedSTATIC DISCHARGES AT STATION 40.3 STR 4L. INSTALLED MS90354U5 AND CONICAL WASHERS PER SRM 53-21-11 PB201. LP 0334710SDR DALA2017121208530Skin · damagedSTATIC DISCHARGES AT STATION 39.1 STR 3L. INSTALLED MS90354U5 AND CONICAL WASHERS PER SRM 53-21-11 PB201. LP 0334691SDR DALA2017121208529Skin · damagedSTATIC DISCHARGES AT STATION 40 STR 4L. INSTALLED MS90354U5 AND CONICAL WASHERS PER SRM 53-21-11 PB201. LP 0334675SDR DALA2017121108512Doubler · wornWEAR ON PREVIOUSLY REPAIRED DOUBLER ON FRAME STA 1437, LONGERON 5LH AT AFT ACCESSORY COMPARTMENT. (LP$0333740)SDR ASOA201712117030Skin · crackedR/H REAR FUSELAGE SKIN AT FRAME 75 STRINGER 1R-3R CRACKED.CUT-OUT DAMAGE SECTION OF EXT FUSELAGE SKIN, FABRICATED REPAIR PARTS AND INSTALLED. AIRCRAFT STILL IN C CHECK.SDR SWAA2018010318768Skin · crackedFUSELAGE SKIN CRACKED AT BS 540, STR 22L. REPAIRED SKIN IAW ER AND EA.SDR SWAA2018010318760Skin · crackedFUSELAGE SKIN CRACKED AT BS 540, STR 22R. REPAIRED SKIN IAW ER AND EA.SDR SWAA2022020453159Scuff Plate · crackedAFT CARGO FWD CORNER SCUFF PLATE IS CRACKED. / INSTALLED FORWARD CORNER SCUFF PLATE PER AMM 53-11-02 PRESSURE CHECK GOOD PER AMM 05-51-91SDR SIMA20171208002Skin · dentedDENT FOUND BELOW GPU DOOR. ACCOMPLISHED A PERMANENT REPAIR IAW SRM 53-12-01 .SDR FDEA201712083346Skin · wornAFT, R/H FUSELOGE, ABOVE AND AFT OF HORIZ, STA 2150, 4 NUTPLATE NUTS WORN THROUGH NUTPLATE AND SKIN. SRM 53-20-00, FIG 22 VOL 1. REPAIRED NUTPLATES PER EA # 8-5320-T0337311, PART # 1 AND SRM 53-20-00 FIG 22 VOL 1SDR DALA2017120808507Skin · corrodedCORROSION LEVEL: 2 AFT CARGO COMPARTMENT FOUND SKIN CORROSION BETWEEN STA 1087 AND STA 1109. UNDER STRINGER. C/W ERA 563670-14. (LP 0330277)SDR CALA2017120804344Skin · damagedMATERIAL LOSS NOTICED ON SKIN AT STA 500 G AT STR 17L+ 1" FUSELAGE SKIN STA 500 G @ STR 17L + 1" HAS BEEN REPAIRED IAW ECRA 5331-02175 AND SRM 53-00-01 REP 36 INSP THRESHOLD AT 50000 FLT CYC''S AFTER AIRPLANE DELIVERY FOLLOWED BY REPEAT INTERVALS AT EACH SUBSSDR JR2R201712080031Skin · gougedAFT CARGO DOOR CUTOUT DAMAGED FROM BAGGAGE LOADER. REPAIRED DAMAGE IAW AAR EA NO. 16774SDR JR2R20171208003Skin · damagedAFT CARGO DOOR CUTOUT DAMAGED FROM BAGGAGE LOADER. REPAIRED DAMAGE IAW AAR EA NO. 16774.SDR DALA2017120808559Skin · unknownEXISTING RE-WORK EXTERNAL SKIN AT FR 64+2 AND STRG 41R ON LOWER FUSELAGE, PERFORMED PERMANENT REPAIR EXTERNAL SKIN AT FR 64+2" AND STR 41R ON LOWER FUSELAGE AS PER ER/A 563230-14AD REVISION ORIGINAL AND PRI 563230-14 REVISION 0.SDR DALA2017120808510Skin · gougedFUSELAGE SKIN HAS A GOUGE 12" UP FROM LOWER FWD CORNER OF C-1 CUT-OUT. C/W ERA 563736-14.SDR SWAA2022020413104Scuff Plate · crackedFORWARD CARGO BAY AFT CORNER THRESHOLD IS CRACKED / FWD CARGO BAY AFT CORNER THRESHOLD WAS REPAIRED ON CUSTOMER CARD #EA 1-A53-2076 REV 11SDR SWAA2022020413107Scuff Plate · crackedAFT CARGO BAY; CENTER BULLNOSE SCUFF PLATE IS CRACKED IN THE RADIUS 14' FROM AFT EDGE / AFT CARGO BAY; CENTER BULLNOSE SCUFF PLATE WAS REPAIRED ON CUSTOMER CARD EA 1-A53-2076. REV 11SDR CALA2017120804340Skin · dented(B757-06-3-0221) LOWER FUSELAGE SKIN BETWEEN STA 520 AND STA 540 , STGR 27R AND 28R HAS SCUFFED DENTS 3EA 209-029 ACCOMPLISED EC/RA 5330-06240 REV-INSTALLED DECAL PER EC/RA 2060- 01042 ON SKIN BETWEEN STA 520 AND STA 540, STR 27FR AND STR 28R FOR AREAS MARKED SDR CALA2017120804339Skin · dented(B757-06-3-0269) LOWER FUSELAGE BETWEEN STA 560 AND STA 520, STGR 27R AND STGR 28R HAS 2EA DENTS 209-013 ACCOMPLISHED PERMANENT REPAIR ON FUS.SKIN BETWEEN ST500 & STA520 . STR27R & STR28R IAW EC/RA5330-06240 REV- & EC/RA5330-06241 REV -.SDR RAIA201712050001Skin · damagedREAR FUSELAGE EXTERNAL SKIN DENTED AND SCRATCH BETWEEN FRAMES 72 - 73, STRINGERS 10R-13R. FABRICATED AND INSTALLED A STRAP AND REPAIR PARTS.SDR SWAA2018010318643Skin · corrodedFUSELAGE SKIN CORRODED AT BS 1016, STRINGER 21L. REPAIRED THE SKIN IAW EA.SDR FDEA201712053351None · noneREPAIR ASSESSMENT: LOWER FUSELAGE, RIGHT SIDE , AT APPROX. STA. 755, LONGERON 42R- 43R, HAS AN EXISTING SKIN REPAIR APPROX. 9X12 INCHES. DOT 11. EXISTING MAJOR REPAIR WAS PREVIOUSLY INSTALLED PER SRM 53-20-00 FIG. 6 SH. 7 VOL.1. REFERENCE E.A. 8-5100-T03360SDR FDEA201712053350Skin · damagedREPAIR ASSESSMENT: LOWER FUSELAGE, STA. 545, LONG. 42R, HAS AN EXISTING DOUBLER AT AFT UPPER CORNER OF ACM EXHAUST CUT-OUT. DOT 5. EXISTING MAJOR REPAIR WAS PREVIOUSLY INSTALLED PER SRM 53-20-00 FIG. 2 VOL.1 REFERENCE E.A. 8-5100-T0336013 "REPAIR CATALOG MSDR CALA2017120804335Skin · dentedB757-06-03-0221 LOWER FUSELAGE SKIN AT STA 500 STA 520 STGR 27R AND 28R HAS GAUGE DENT 209-028 ACCOMPLISHED INTERIM REPAIR ON FUSELAGE STRINGER 27R BETWEEN B.S 500 AND B.S. 520 IAW ECRA 5330-06254 REV-.PART1. SEE PART 2 FOR INSPECTION REQUIREMENTS AND PART 3 FSDR C77A20171205001Skin Panel · gougedDENT AND GOUGE DAMAGE WAS DISCOVERED IN PHX BETWEEN FR10/FR11 AND S-17L/S-18L ON THE P/N 170-03387-003 FORWARD FUSELAGE LT LATERAL AFT SKIN PANEL IN TWO AREAS. DAMAGE AREA NR 1 CONSISTED OF A 1.8 INCH DENT TO A DEPTH OF 0.065 INCHES WITH A GOUGE AT THE DEEPESTSDR SWAA2022020442148Skin · corroded***CORROSION*** ON FUSELAGE SKIN; UNDER DORSAL FIN; FROM B.S. 887-1006. / REPAIRED SKIN CORROSION DAMAGE BS 887-1006 STR 2L - STR 2R ON CROWN OF SKIN IAW EA # 1-753-32083 IR & ER # 17-05457 IR.SDR SIMA20171204002Skin · dented2 DENTS AND 1 PROTRUSION BTW FR 19-20 STR 11-12L-C/A-REPAIRED 2 DENTS AND 1 PROTRUSION BTW FR 19-0 STR 11-12L IAW ERS-EM-53MR-3029SDR CALA2017120804334Skin · dentedON WALKAROUND FOUND DENT ON LEFT FUSELAGE AT STATION 390. REPAIR INSTALLED PER SRM 53-00-01 REPAIR 14. THIS REPAIR REQUIRES REPETETIVE INSPECTIONS PER TABLE V. THIS IS A CATEGORY B REPAIR. DOUBLER THICKNESS IS .071, INSPECTION THRESHOLD IS 30,000 PTC WITH R
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