JASC 5330
Service difficulty reports · 79,329
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 CALA2019040100501Skin · dentedDENT AT FUSELAGE SKIN APPROX STA 1022 BETWEEN STR 13L AND 14L 28IN AFT OF L2 DOOR KNEE HIGH ABOVE FLOR WAS FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY TO SKIN SPLICE FASTNER ROW PER B737 SRM 53-00-01 AD1 STEP 4C TABLE 102 NOTE 1. ACCOMPLISHED PERMANENT REPAIR ASDR SWAA2019040131208Doubler · crackedELECTRICAL GROUND POWER RECEPTACLE SURROUND DOUBLER CRACKED. REPAIRED DOUBLER PER EA & SRM.SDR DALA2019033102054Skin · damagedDAMAGE AFT OF NR 2 ENG PYLON AT UPPER LEFT CORNER OF EMEGENCY EXIT STENCIL. ACCOMPLISHED ERA 576838-14 REV ORIG. STOP DRILLED CRACKS. REMOVED DAMAGE, FABRICATED DOUBLER, AND BEGAN INSTALLATION PER SRM 53-04-3 FIG 2 SHT 3. CLASS 2 REPAIR. COMPLETED INSTALLATIONSDR DALA2019033002043Skin · damagedINITIAL INSPECTION: CREASE ON FUSELAGE SKIN BTW STA Y=1265 AND Y =1277 BTW LONG 27L AND 28R. FUSELAGE SKIN BTW STA Y=1265 AND Y=1277 BTW LONG 27L AND 28R WAS REPAIRED PER ER/A 576844-14 REV.: ORIG. SEC.: I AND ETI-88-19-030 REV: ORIG. ACCOMPLISH SECTION II REPSDR SWAA2019051532645Skin · bulgedEMERGENCY AND EQUIPMENT COMPARTMENT EXTERNAL SKIN BULGED AT BS. 259, STR. 28R. REPAIRED SKIN IAW EA.SDR SWAA2019050632303Skin · damagedEXTERNAL SKIN DAMAGED BETWEEN BS. 380 TO BS. 440, BETWEEN STR. 21R TO STR. 22R. REPAIRED SKIN PER EA AND ER.SDR DALA2019040402190Skin · crackedSKIN STA 1654, S13AR CRACKED. C/W E/RA 567634-14.SDR SWAA2022030446156Skin · corroded***CORROSION*** ON FUSELAGE SKIN; UNDER DORSAL FIN; AT B.S. 967-1007; L.B.L. 9 - R.B.L. 8; AROUND FASTENERS. / FUSELAGE SKIN UNDER DORSAL FIN B.S 967-1007 LBL 9 - RBL 9 REPAIRED IAW EA 1-753-34798 REV IR AND ATS ER 19-02976 REV IRSDR SWAA2022030462838Skin · dentedFUSELAGE SKIN DENT AT STA 1064+21' S-25R (REF:8353403) AND STA 1064+16 S-25R (REF:8353 404) REQUIRES A PERMANENT REPAIR PER CARD# J9987755 / THE DENT DAMAGE HAS BEEN TRIMMED OUT. UPON DAMAGE REMOVAL; S-25R (P/N 148A3370-14) WAS FOUND WITH DENT DAMAGE AS WELL. SDR DALA2019032902051Skin · damagedCONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOCATED AT FR 16 AND STRINGER 34R ON LOWER FUSELAGE. PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN LOCATED AT FR 16 AND STRINGER 34R AS PER ER/A 576631-14 REV ORIGINAL AND PRI 576631-14 REV O JOB COMPLESDR DALA2019032902048Skin · damagedCONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOC FR73 TO FR74 AND STR33R ON LOWER FUSELAGE. PERFORMED PERMANENT REPAIR LOCATED EXTERNAL SKIN BTW FR 73 TO FR 74 STR 33R TO STR 33L AS PER SRM A319 53-51-29-300-002.SDR UIEA2019032903689Skin · crackedCRACK ON FUSELAGE SKIN AT STA 1720, S-45L(<P>1. REPAIR DAMAGE AREA IAW EI NO T2019A53M-1058 REV.1 2. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)SDR UIEA2019032903696Skin · corrodedCORROSION - 33EA CORROSION LOCATION FOUND DURING PERFROM SB 747-53A2878(<P>1. ACCOMPLISHED FUSELAGE SKIN REPAIR IAW EI. NR T2019A53M-1156 REV.3 2. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)SDR REXA2019060427773Tripler · gougedINITIAL INSPECTION: GOUGE ON PREVIOUS REPAIR TRIPLER IN STA. FS= 917 TO FS= 919.5 NEAR STGR 27 AT FUSELAGE SKIN. (FUS) SKIN TO STA. FS= 917 TO FS= 919.5 NEAR STGR 27 AT FUSELAGE SKIN WAS REPAIRED, PER CRJ-900 REO 670-53-00-290 REV.FSDR SWAA2019040431379Filler · crackedEXISTING REPAIR FILLER AT LOWER EXTERNAL POWER DOOR CUTOUT CRACKED. / REPAIRED CUTOUT PER SRM.SDR DALA2019033102056Skin · dentedFUSELAGE SKIN STA Y=1250-1287 & L27L TO L28R DENTS & SCRATCHES. ACCOMPLISH ER/A 576844-14 SECTION II INSPECTION WITHIN EVERY 8000 CYCLES AFTER ACCOMPLISHMENT OF THE SECTION I REPAIR. (LP1007252)SDR CALA2019032900481Skin · gouged(B757-53-3-6355) EXTERIOR FUSELAGE SKIN HAS A 10 INCH GOUGE AT A PPROX FS 1862.7 BENEATH LT HORIZONTAL STABILIZER 08-04. REF ON V N/R CARD NO 0050691. FOUND FUSE SKIN AT STA 1863 TO 1865 S-14L TI S-17L OUT OF LIMITS IAW SRM 53-80-01 FIG 101, CUT OUT DAMAGE ANDSDR LR7A2019032701488Skin · crackedDURING SCHEDULED C-8 CHECK UNDER JOB CARD HC5321, FOUND THE LT FWD FUSELAGE SKIN WITH CRACKED RIVET HOLES AT FS146, WL210-218, LBL76. REPAIRED IAW SRM, FIG. 51-140-10. NR 2042.SDR LR7A2019032701487Skin · buckledDURING SCHEDULED C-8 CHECK UNDER JOB CARD HC5321, FOUND THE RT FS797 AFT FUSELAGE SKIN BUCKLED AT WL200, RBL85. REPAIRED IAW SRM, FIG. 51-140-10. NR 2032.SDR LR7A2019032701485Skin · crackedDURING SCHEDULED C-8 CHECK UNDER JOB CARD HC5321, FOUND THE RT FUSELAGE SKIN CRACKED AT TWO RIVET HOLES AT FS156-165, WL235, RBL55. REPAIRED IAW SRM, FIG. 51-140-10. NR 2009.SDR DALA2019040262088Doubler · corrodedFWD CARGO AT STA 676 - STA 698 AND S-36L - S-35L FOUND DOUBLER CORROSION OUT OF LIMITS. DOUBLER REPLACED. (LP 1002059)SDR DALA2019033102055Skin · damagedFUSELAGE SKIN AFT LAV SERVICE DOOR CUTOUT STA Y=1307-1322, L-22L SKIN & INTERNAL DOUBLER/ CORROSION. ACCOMPLISH ER/A 576847-14 SECTION II INSPECTION WITHIN EVERY 3000 CYCLES UNTIL SECTION III IS ACCOMPLISHED WITHIN 8000, ALL AFTER ACCOMPLISHMENT OF SECTION I. SDR SWAA1939030131166Skin · damagedFUSELAGE SKIN CREASED BETWEEN BS 325 TO BS 340, BETWEEN STR 20R TO STR 21R. REPAIRED SKIN PER SRM.SDR SWAA2019041031558Skin · dentedSKIN DENTED AT BS. 927, BETWEEN STR. 23R. TO STR. 24R. REPAIRED SKIN IAW EA AND ER.SDR R61A2019041025373Skin · dentedA DENT WAS FOUND ON LH FWD FUSELAGE. A PERMANENT REPAIR WAS C/W IAW EMB 175 SRM 53-10-01. AIRCRAFT REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.SDR SIMA20190325002Skin · peelingTRANSFERED FROM AML PAGE 4191593 ITEM 3. FOUND POSSIBLE CRACK/SKIN PEELING AT FRAME 25 STRINGER 21L REF. ITEM 1 OF THIS LOG PAGE. C/A-COMPLIED WITH REPAIR OF DAMAGED AREA AT FRAME 25 STRINGER 21L AND 21R IAW SRM 53-22-01.SDR DALA2019032501966Plate · missing(LOG 5795013) DURING INSPECTION FOUND 2 LOWER ANTENNAS BASE PLATES ON LOWER AFT FUSELAGE APPEAR TO BE MISSING. MAINTENANCE REINSTALLED ANTENNA BASE PLATES CHECKS GOOD.SDR ASOA201903247034Skin · corrodedTYS A/C IS IN C-CHECK WHEN INSPECTION FOUND FUSELAGE CORRODED UNDER THE RA ANTENNA BETWEEN FRAMES 69 AND 70 AND STR 21L AND 21R. MAINTENANCE PERFORMED A DOUBLER ON THE FUSELAGE BELOW THE RA ANTENNA AT FRAMES 69 AND 70 IAW SRM 53-00-23. ALL WORK ACCOMPLISHED ASDR CA190328011Skin · corroded(CAN) 4-OFF BLENDED CORROSION DAMAGES IN LOWER FUSELAGE SKIN AREA AS FOLLOWS. LOWER FUSELAGE SKIN PANEL - (DWG: SH690-37061) BTW STR25L-26L, BTW FS847.00+48 - FS847.00+62 AND FS881.00 - FS897.7. STRINGER 26L - (DWG: SH690-37067) BTW FS881.00 & FS897.7 INSDR ASAA2019040328874Skin · damagedGROUND EQUIPMENT HIT FUSELAGE. SCRATCH FOUND ON A/C BELOW AFT PIT DOOR ON BELLY. GROUNDED - YES. INSTALLED CAT C REPAIR IAW EA 900ER-53EA-21438.SDR AC2R2019032213901Deck Plate · delaminatedSEVERAL DELAMINATION'S OCCURRED THROUGHOUT DECK.SDR CALA2019032200458Skin · dented1 SMALL DENT @ STA732 A/C RT 3 INCHES BELOW STG.17R LOG 8238405 HAS INCORRECT INFORMATION FOR LOCATION AND DENT SIZE. (REF NR 99833439) ACCOMPLISHED SKIN DOUBLER REPAIR AT RT FUSELAGE STA 442 TO STA 465 STR 17R TO STR 20 REF SRM 53-00-01. REPAIR 21 FIGURE 202 SDR EE4Y2019032208466Skin · corrodedDURING THE STRUCTURE INSPECTION, IT WAS FOUND AT LOWER FUSELAGE SKIN WITH CORROSION AT BS 648 BETWEEN STRINGER 28R AND 28L, DME2 ANTENNA AREA. THE DAMAGED AREA WAS REPAIRED PER INSTRUCTIONS PROVIDED ON SR 4-4392840368 AND APPROVED UNDER FAA FORM 8100-9 PROVIDESDR SWAA2022030449768Skin · puncturedFUSELAGE SKIN DAMAGE FROM GROUND EQUIPMENT REPORTED HOLE/PUNCTURE AT APPROX STA 1008 BETWEEN STA 12L AND 13L. PUNCTURE MEASURES TO BE 4.5' X 6'. TRANSFERED FROM NRC D189648 / ACCOMPLISHED REPAIR OF DAMAGED SKIN REF EA REPAIR 53A-06548 REF SA-M 326 A1134064SDR DALA2019032201904Skin · dentedSHIP 6702 LOCATED DENT AT FUSELAGE SKIN STA 650 JUST ABOVE STR 18L (REF LOG PAGE #7605177). CORRECTIVE ACTION: EVALUATED DENT AND FOUND TO BE OUT OF LIMITS. REPAIRED PER ERA 575608-14 REV ORIG.SDR R61A201903200321Skin Panel · dented***WHILE A/C WAS OUT OF SERVICE FOR HEAVY CHECK*** FWD FUSELAGE EXTERNAL SKIN 2 DENTS FOUND IN ADJACENT BAY BTWN FR 9-10 AND BTWN STR 14L-16L. FWD FUSELAGE EXTERNAL SKIN 2 DENTS IN ADJACENT BAY BTWN FR 9-10 AND STR 14L-16L WAS MEASURED AND FOUND W/I LIMITS IAWSDR CHIA201903213828Skin · crackedDURING RAMP CHECK IS WAS NOTED VISUALLY THAT THERE WAS A 6+" SKIN CRACK STA 520 BL20L WL+97. VP-000265-19 HAS BEEN CREATED TO DO THE REPAIR.SDR SWAA2022030304806Skin · dentedMOD TYPE: 6 NBR 22971 REV: POS: SKIN DENT STA 1035; 2 INCHES ABOVE STR 15L DIMENSIONS 2 INCHES LENGTH 6 INCHES WIDTH .215 INCHES DEEP PER SRM 53-00-01-1A-1- 4.C.3.B DENT FOUND TO BE WITHIN LIMITS. RE-INSPECT FOR CORROSION AND CRACK AT EACH 5000 FLT CYCLE INTERSDR SWIA2019050145794Skin · corrodedEXTERIOR BOTTOM SKIN AT APPROX. FS 559+112 EITHER SIDE OF BL 0 HAS SEVERAL AREAS OF CORROSION AROUND FASTENER HOLES FOR FAIRING 195BB AS WELL AS A DETERIORATED SEALING PAD. (C-CHECK) RO: 04/28/2019 REMOVED CORROSION FROM EXTERIOR BOTTOM SKIN AT APPROX. FS 559+SDR SWIA2019050145793Skin · corrodedEXTERIOR BOTTOM SKIN FROM APPROX. FS559.0 TO FS559.0+112 AND SEVERAL INCHES EITHER SIDE OF BL 0 HAS MULTIPLE AREAS OF CORROSION AROUND FASTENERS AS WELL AS AROUND BELLY DRAINS. (C-CHECK) RO: 04/28/2019 REMOVED CORROSION UNDER FASTENERS HEAD APPROXIMATELY FROMSDR WVER2019032611Doubler · corrodedTCAS DOUBLE AT STGR 27, FS 295 TO 310 IS CORRODED.SDR SWAA2019032030850Skin · crackedSKIN CRACKED AT BS 827+3, STR 26R. REPAIRED SKIN PER SRM.SDR R61A2019040418340Doubler · corrodedDURING HEAVY CHECK MAINTENANCE FOUND HEATED DRAIN MAST DOUBLER HAS SIGNS OF CORROSION BETWEEN FRAMES 86 AND 87 STRINGERS
28R AND 27R. REMOVED AND REPLACED AFT HEATED DRAIN MAST DOUBLER, REF SRM 51-40-08. A/C REMAINS IN CHECK.SDR WVER20190402119Skin · gougedFUSELAGE SKIN GOUGED AT 6 0CLOCK POSITION APPROX BS 977 AT LOCATION OF PREVIOUS REPAIR.SDR CALA2019032200436Skin · crackedLT FR 35 STR 30. AFT LOWER FASTENER HOLE HAS CRACK INDICATION REPAIRED LOWER AFT HOLE IN LT FR35 STR 30 IAW ECRA 5311-02101. ACOMPLISH THE INITAL INSPECTION REQUIREMENTS AT FR 35 STR 30L PA RT 2 OF ECRA 5311-02101 ON OR BEFORE THE A/C REACHES 38,013 TOTAL F/C SDR AALA201904089019Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON INTERNAL FUSELAGE SKIN IN THE BULK CARGO COMPARTMENT BETWEEN FR 65 AND FR 66, BETWEEN S31R AND S32R. REPAIRED SKIN PER EA 292127.SDR DALA2019031701761Skin · crackedON WALK AROUND FOUND 2 CRACKS LEFT SIDE STA 1265.603 6" ABOVE AFT AIRSTAIR DOOR CUTOUT. INSTALLED PERM REPAIR PER SRM 53-01 PAGE 12 FIG 2. (LP5835229)SDR DALA2019031701755Skin · crackedCRACK ON CUTOUT SURROUND ALSO ON FUSELAGE SKIN AT FWD LOWER CORNER OF LAVATORY SERVICE ACCESS (FUS). NRC 00015: CRACK ON CUTOUT SURROUND ALSO ON FUSELAGE SKIN AT FWD LOWER CORNER OF LAVATORY SERVICE ACCESS WAS REPAIRED PER ETI-17-19-028 REV 4 AND ER/A 576379-1SDR SWIA201904125751Doubler · corrodedFS 409 STR 27 TO 26 R DOUBLER HAS CORROSION LOWER EDGE. (C-CHECK) RO: 04/11/2019 REMOVED AND INSTALLED NEW VHF SUPPORT INTERCOSTAL IAW REO. LEAK CHECKS GOOD.SDR ASAA2019031528669Skin · corrodedLAV VENT HAS CORROSION ARROUND OUTER SKIN. GROUNDED - YES. REPAIRED LAV VENT SKIN CORROSION IAW SRM 53-70-01-2R-3 THIS IS A CATEGORY B REPAIR. INSPECTION THRESHOLD SET AT 50,000 TOTAL FLIGHT CYCLES WITH AN INTERVAL OF 5,000 CYCLES. SEE SRM 53-70-01-2R-3 FOR ME
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