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 DALA2021012100404Skin · damagedDURING INSPECTION FOUND FUSELAGE SKIN DAMAGED FROM STA 177.73 TO STATION 211.67 A/C LEFT. INSTALLED REPAIR IN ACCORDIANCE WITH ER/A 589214-14 REV ORIGINAL.SDR DALA2021012100387Skin · corrodedCORROSION INTERNAL SKIN LOCATED BETWEEN STR 38R AND 39R, FR 64 AND FR 65 IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: PERFORMED REPAIR PER ER/A 589304-14AD REV ORIGINAL AND PRI 589304-14 REV O AND 1.SDR SWIA202157037Doubler · corrodedI* IN BETWEEN FS 295.0 TO FS 310.0 ANTENNA DOUBLER HAS CORROSION. (C-CHECK) RO 3/25/2021 REMOVED AND REPLACED ANTENNA DOUBLER BETWEEN FS295 AND FS310, STGR 27. REF. CRJ700 SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 AND DWG# SH670-30023 REV. G SHEESDR SWIA202156873Skin · dentedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA64677-601R-53-11-3643 962SW MXCODEID54006-PR - FOUND DENT APPROX 2" LONG BETWEEN FS.250 AND FS.265 AND BETWEEN STRG 27 AND STRG 26R. COMPLIED WITH TEMPORARY REPAIR PER REO 601R-53-11-3643 REV -A DATED 2020-12-10. PERSDR SWIA202156668Skin · corrodedEXTERIOR SKIN UNDER LOWER ADF ANTENNA HAS CORROSION. (C-CHECK) RO 3/4/2021 REMOVED CORROSION ON EXTERIOR SKIN UNDER LOWER ADF ANTENNA IN LIMITS REF MHIRJ REO 690-53-31-553 REV. --, DATED: 2021-01-31 AND CRJ-900 SRM 51-21-06-001-001-A01. COMPLIED WITH 51-9SDR SWAA2021021547975Skin · damagedCROWN SKIN HAS DAMAGE UNDER DORSAL FIN AT STR. 1 B.S. 847. / FACT AS A RESULT OF POST REPAIR INSPECTIONSDR JJBA20210120051Skin · damagedLEFT SIDE FUSELAGE EXTERNAL HAS DAMAGE AT APPROXIMATELY FRAME 11 LEFT STRINGER 15 LEFT. MADE SURE THE DENTED AREA BETWEEN FRAMES 10 & 11 AND ST 15L AND 17L ON THE FF II LT SKIN IS FREE OF SHARP EDGES, OIL CANNING, AND CREASES THERE IS NO SIGN OF MISSING, SHEASDR JJBA20210120033Doubler · corrodedLOWER FUSELAGE ANTENNA RAD ALT NO 1 INTERNAL DOUBLER CORRODED. CUT OUT DONE. DOUBLER HOLES PATTERN DRILLED ON SKIN. DOUBLER INSTALLED WITH FILLER.SDR JJBA20210120031Skin · corrodedCARGO AREA UNDER FLOOR FR 67 AROUND WATER DRAIN SKIN SHOW SIGN OF CORROSION, CORROSION LEVEL 2. CARGO AREA UNDER FLOOR FR 67 AROUND WATER DRAIN SKIN SHOW SIGN OF CORROSION OUT OF LIMITS REMOVED BY CUT OUT. REPAIR PARTS FAB, REPAIR CARRIED OUT. FOR SKIN REPRSDR JJBA20210120030Skin · crackedRF 1 LT FUSELAGE SKIN AT FR 75.700 BELOW STGR 2L 2 CRACK FOUND AT ONE RIVET LOCATION. ON RF1 LT FUSELAGE SKIN AT FR 75.700 BELOW STGR 2L CUT OUT DONE. ON RF1 LT FUSELAGE SKIN AT FR 75.700 BELOW STGR 2L SKIN REPAIRED.SDR A6WA202101227561Skin · corrodedUPPER FUSELAGE TCAS ANTENNA MATING SURFACE FS 310, STGR 1R TO STGR 1L HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. BLENDED OUT DAMAGE ON TCAS ANTENNA MATING SURFACE FS 310, STGR 1R TO STGR 1L, P(1) 1.0L X 0.70W, P(2) 1.2L X 0.60W, P(3) 0.8L X 0.95W, P(4) 1.SDR DALA2024032103604Skin · damagedSHIP 3242 DISC: A TOTAL OF (21) EXISTING TEMPORARY LIGHTNING STRIKE REPAIRS (TEMPORARY FASTENERS) FOUND IN UPPER SKIN PANEL BTWN FR 24 & FR 32, AND BTWN STR 3L - STR 2R. C/A: ***DTE REQUIRED*** PER SECTION DTE OF 589262-14, THE RPEAIR OF SECTION I IS LIMITED TSDR SWIA202157143Skin · dentedDENT LOCATED ON RIGHT SIDE OF AIRCRAFT NOSE BETWEEN STRINGER 12A & 13A AFT OF FS220.00. DAMAGE DIMENSIONS: 4€? X 1.5€? X .102 DEEP. COMPLIED WITH TEMP REPAIR PER REO 670-53-11-1548 REV -- DATE 2019-10-06 AND REO 670-51-00-085 REV €“ A, DATED 2017-08-23. PSDR SWIA202157032Doubler · chafed* EXISTING REPAIR AT APPROXIMATELY FS969-FS985 STGR26L-STGR26R HAS 2EA CHAFES (C-CHECK) RO 3/25/2021 REMOVED AND REPLACED EXISTING REPAIR AT APPROXIMATELY FS969-FS985 STGR26L-STGR26R REF REO 670-53-00-290 REV F DATED 2019-04-26, NO LEAKS NOTED. COMPLIED SDR SCNA20210205034Panel · puncturedFUSELAGE BODY PANEL 193AR COMPOSITE PUNCTURED INSIDE PANEL. REPAIRED PUNCTURE ON INNER SURFACE OF FUSELAGE BODY PANEL 193AR PER SRM 53-40-70-2R-1 TABLE 201 AND SRM 51-70-05-2R-1.SDR DALA2021012000372Skin · corrodedCORROSION FRAME 33 TO FR 34 INTERNAL SKIN AND BETWEEN STR 40R TO STR 42R IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: INSPECTED AREA, AS PER SRM A320 53-21-11-283-007.SDR DALA2021012000371Skin · corrodedCORROSION FRAME 33 TO FRAME 34 INTERNAL SKIN BETWEEN STR 42R TO STR 44 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: INSPECTED AREAS, PER SRM A320 53-21-11-283-007. CONT IN SERVICE.SDR CALA2021012000058Skin · damagedA/C SUSTAINED DAMAGE JUST AFT OF STA 1620 ABOVE S-20R. DAMAGE BETWEEN STRINGERS S-19R AND S-20R. REMOVED 25 EXISTING FASTENERS AROUND THE PERIMETER OF DAMAGE FOR REPAIR. COMPLIED WITH STEPS 1 THRU 5 OF AVO 8768 PERFORMED HFEC ON TRIM OUT, PER PT 6 51-00-01,SDR CALA2021012000059Skin · damagedA/C SUSTAINED DAMAGE JUST AFT OF STA 1701 BETWEEN STRINGERS S-20R AND S-21R. FOUND A PREVIOUS REPAIR OVER STRINGER 19R AFT OF STA 1701 APPROXIMATELY AND ABOVE TO DMG AREA. REMOVED REPAIR FOR ACCESS. COMPLIED WITH AVO 8767 STEPS 1 THRU 5 TO CONTINUE. HFEC CSDR DALA2024032103624Skin · dentedSHIP 5650 DTA MONITOR INSPECTION LOG REF ERA 589420-14AD, FUSELAGE / LOWER SKIN DOOR CUT OUT / BS 460 AND S-28R - DENT. CORRECTIVE ACTION: REF ERA 589420-14AD. (1708302)SDR R61A2021012100089Skin · inadequateMAJOR: WHILE AIRCRAFT WAS IN FOR HEAVY CHECK, EXTERNAL DOUBLER LOCATED AT FR 18 STGR 27R AND 28R REQUIRES REMOVAL AND EVALUATION. REMOVED EXISTING EXTERNAL DOUBLER/FILLER LOCATION FR 18 STGR 27R-28R, PER EMB175 SRM 51-40-08. INSTALLED NEW REPAIR DOUBLER AND SDR R61A2021012200088Doubler · inadequateMAJOR: WHILE AIRCRAFT WAS IN FOR HEAVY CHECK. EXTERNAL DOUBLER LOCATED FR 22, STGR 13L-15L REQUIRES EVALUATION. COMPLIED WITH ETD2021-170-001535. REMOVED DOUBLER, LOCATED AND DRILLED NEW DOUBLER AND FILLER. INSTALLED NEW DOUBLER AND FILLER, IAW ETD2021-170SDR MASA20210118008Skin · gougedGOUGE IN AFT LOWER FUSELAGE SKIN. REMOVED GOUGE DAMAGE REPAIR AND REPLACE WITHIN NEW EXTERNAL REPAIR WITH PROTECTIVE PLATE, IAW GREO 670-53-00-290 REV E.SDR SWIA202157028Skin · dented*FS310.00 STRG 22RH-23RH EXTERIOR SKIN DENT (MARKED) (C-CHECK) RO 3/25/2021 DENT FOUND TO BE OUT OF LIMITS REF. CRJ-700 SRM, 53-21-01-101-006-A01. COMPLIED WITH REPAIR OF DENT REF. REO 670-53-21-1941 REV -- DATED: 2021-02-18, ALL STEPS COMPLIED WITH, COMPSDR SWIA202157027Skin · dented*FS295.00 STRG 23RH-24RH EXTERIOR SKIN DENT (MARKED) (C-CHECK) RO 3/25/2021 REPAIRED DENT REF REO 670-53-21-1941 REV --, DATED: 2021-02-18. ALL STEPS COMPLIED WITH AND COMPLIED WITH TASK CARD 51-900-1002-SKY, SEE CONTIMNUE CARD FOR FURTHER DETAILS.SDR SWIA202156322Skin · dentedDENT LOCATED 4 INCHES FORWARD OF FS 394 STGR 16R. (C-CHECK) RO 2/17/2021. REPAIRED DAMAGE IAW REO 601R-53-21-3378 REV-- DATED 2021-01-21, COMPLETED MAJOR REPAIR TASK CARD 51-900-1003-SKY, AND FORM M-337. NO WEIGHT CHANGE.SDR HNAA2021020200034Skin · damagedEXTERNAL FUSELAGE SKIN HAS CREASE BTW FRAMES 19-20, STRINGER 13-14L....REPAIRED EXTERNAL FUSELAGE SKIN HAS CREASE BETWEEN FRAMES 19-20, STRINGER 13-14L IAW PIEDMONT EO1-53-21-0018.SDR A6WA202101217559Skin · dentedUPPER SURFACE OF FUSELAGE HAS DENT AT FS 596.00, STGR 3R AND STGR 4R. AIRCRAFT REMOVED FROM SERVICE. EVALUATED DENT AT FS 596.00, STGR 3R AND STGR 4R, 1.7 L X 1.6 W X 0.057 D, FOUND TO BE OUT OF LIMITS FOR SHARP CREASES. IAW CRJ200 SRM 53-00-31, (REV 38). ASDR SWIA202155454Skin · dentedTRANSFER FROM EAML 560725: DENT AND SCRATCH (14.5L X 1.2"W X .100" MAX DEEP, REF) ON FUSELAGE SKIN PANEL (DWG. SH670-31071; .047" THK IN THE DAMAGED AREA, REF) BETWEEN FS 453.00-FS 469.00 AND STR 15R -16R. OUT OF SRM LIMITS. THIS HAS BEEN DETERMINED TO BE A SDR SWAA2021021844722Fastener · brokenBROKEN EXTERNAL SKIN FASTENER ON DRAG ANGLE AT BS 540 LT SIDE AT LEVEL STR 22L AT LOWER FUSELAGE (1 EA). REPLACED EXTERNAL SKIN FASTENER ON DRAG ANGLE AT BS 540 LT SIDE AT LEVEL STR 22L AT LOWER FUSELAGE (1 EA) IAW B737-700 SRM 51-40-02-0G-0.SDR FDEA202101150117Doubler · misinstalledWHILE ACCOMPLISHING LH E.O.#G-5310-E0332629 I P5 FOUND NEW FUSELAGE SKIN DOUBLER EXISTING HOLE AT STA 998 STR. S-35L NEAR MILLED EDGE COMPLIED WITH E.A.#:G-5310-T0359410 P1 TITLE : FUSELAGE-MAINFRAME-DEVIATIONS TO SB- 777-53-0087 R1 - LHS AND RHS UNDERWING SDR FDEA202101150116Doubler · misinstalledWHILE ACCOMPLISHING RH E.O.#G-5310-E0332629 I P6 FOUND NEW FUSELAGE SKIN DOUBLER EXISTING HOLE AT STA 998 STR. S-35R NEAR MILLED EDGE. COMPLIED WITH E.A.#:G-5310-T0359410 P2 TITLE : FUSELAGE-MAINFRAME-DEVIATIONS TO SB- 777-53-0087 R1 - LHS AND RHS UNDERWINGSDR FDEA202101150115Skin · crackedDURING ACCOMPLISHMENT OF HFEC INSPECTION ON RH FUSELAGE SKIN COMMON TO UNDERWING LONGERON, FOUND CRACK INDICATIONS AROUND 01 EA FASTENER HOLE STA 1028 STR 37R, APPROX 1.5" IN LENGTH. COMPLIED WITH E.O.#:G-5310-E0332629 I P6. TITLE: FUSELAGE-MAINFRAME-INSPESDR FDEA202101150114Skin · crackedDURING ACCOMPLISHMENT OF HFEC INSPECTION ON LH FUSELAGE SKIN COMMON TO UNDERWING LONGERON, FOUND CRACK INDICATION AROUND FASTENER HOLE AT STA 1033 STR 37L, APPROX 1.5" IN LENGTH, AS MARKED. COMPLIED WITH E.O.#G-5310-E0332629 I P5. TITLE:FUSELAGE- MAINFRAMSDR SWAA2021012744683Skin · dented2 EACH DENTS LOCATED AT STA 188 AND STA 211 S-24L, REFERENCE DEFECTS: 0211796 AND 0211797. ACCOMPLISHED CATEGORY 'B' REPAIR, IAW B737 SRM 53-10-01-2R-8 REPAIR 8 AT STA 188 AND 211, S-24L.SDR SWIA202156837Skin · corrodedSURFACE CORROSION ON FUSELAGE SKIN AROUND MULTIPLE NUTPLATE HOLES FOR FUSELAGE TO WING FAIRINGS 191BB AND 192BB (C-CHECK) RO 3/10/2021 REMOVED CORROSION AND REPAIRED FUSELAGE SKIN AT FUSELAGE TO WING FAIRING 191BB AND 192 BB IAW REO 601R-53-31-1176 REV --SDR SWAA2021021542070Bear Strap · crackedCRACK NOTED IN FWD SERVICE DOOR BEAR STRAP BETWEEN STR 8R AND STR 9R FWD OF DOOR CUTOUT. / REPAIRED FWD SERVICE DOOR BEAR STRAP BETWEEN STR 8R AND STR 9R FWD OF DOOR CUTOUT IAW SRM 53-10-01-2R-6SDR SWAA2021021548281Skin · dentedDENT ON FUSELAGE SKIN BS 767 + 6.5; 2.5' BELOW STR 14L / THE DAMAGE WAS REPAIRED PER ATS ER 21-01085 REV IR AND SWA EA 21-153-00276 REV IR. REFER TO NRC U264629 FOR TRACKINGSDR SWAA2021021548280Skin · dentedDENT ON FUSELAGE SKIN BS 767 + 6.5; 1' BELOW STR14L / REPAIRED DENT ON FUSELAGE SKIN BS767+6.5; 1' BELOW STR 14L PER ATS ER 21-01085 REV IR & EA 21-153-00276 REV IRSDR LR7A2021011402761Skin · corrodedDURING P4-LAS SCHEDULED C-3 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE FS 737 FUSELAGE RT SKIN CORRODED AROUND FASTENERS AT WL 258, RBL 63. REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12 NR 1000327399.SDR LR7A2021011402756Skin · crackedDURING P4-LAS SCHEDULED C-3 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE FUSELAGE SKIN CRACKED AT FS 476.5, RBL 21, WL 282 AT AFT OUTBOARD HOLE OF RBL 20 LONGERON. REPAIR BY REPLACEMENT ACCOMPLISHED, IAW LOCKHEED SMP583 SRM, CH 51-60 & 51-70 NR 1000318SDR LR7A2021011402706Skin · buckledDURING P4-LAS SCHEDULED C-3 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE FUSELAGE LT SKIN BUCKLED AT FS 385, WL 155, LBL 82. REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12 NR 1000311514.SDR LR7A2021011402701Skin · scratchedDURING P4-LAS SCHEDULED C-3 CHECK UNDER JOB CARD HC5321, FOUND THE FS 800.0E BELLY SKIN SCRATCHED AT RBL 42, WL 135. REPAIRED, IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12 NR 1000310145.SDR LR7A2021011402679Stiffener · chafedDURING P4-LAS SCHEDULED C-3 CHECK UNDER JOB CARD HC5314, FOUND THE FS 787.0E BELLY SKIN STIFFENER CHAFED AT FS 787.0E, RBL 32, WL 131. REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-21 NR 1000303625.SDR LR7A2021011402671Stiffener · gougedDURING P4-LAS SCHEDULED C-3 CHECK UNDER JOB CARD HC5314, FOUND THE FS 727 BELLY SKIN STIFFENER GOUGED AT RBL 31, WL 131. REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-21 NR 1000303161.SDR LR7A2021011402668Stiffener · gougedDURING P4-LAS SCHEDULED C-3 CHECK UNDER JOB CARD HC5314, FOUND THE FS 387 BELLY SKIN STIFFENER GOUGED AT FS 387, RBL 31, WL 132. REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-21 NR 1000303148.SDR LR7A2021011402659Stiffener · chafedDURING P4-LAS SCHEDULED C-3 CHECK UNDER JOB CARD HC5314, FOUND THE FS 427 BELLY SKIN STIFFENER CHAFED AT LBL 35, WL 133. REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-21 NR 1000302550.SDR SWIA202156771Doubler · corrodedANTENNA DOUBLER FROM F.S. 295.00 TO F.S. 310.00 HAS MULTIPLE SPOTS OF CORROSION FROM STRINGER. 26L-26R (C-CHECK) RO 3/10/2021 REPLACED ANTENNA DOUBLER FROM F.S. 295.00 TO F.S. 310.00 FROM STRINGER. 26L-26R IAW CRJ 700 SRM 51-42-06-001-001-A01. ATTACHED SSDR SWAA2021021541636Skin · crackedFUSELAGE - BS 540 S-22L REF FIG 2 CIRCLE NOTE 1 AD 2019-11-06; EO 14516. CRACK INDICATION FOUND. REF B737 NDT PART 4 53-20-02. B/C19498. REQ. REMOVE FASTENERS AND PERFORM A OHEC PROCEDURE TO VERIFY CRACK INDICATION IAW B737 NDT PART 6; 51-00-00 PROC. 16. / ACCSDR S6G2021F00000Skin · crackedA CRACK WAS DISCOVERED IN THE SKIN, LEFT SIDE OF AIRCRAFT AT THE TOP SIDE OF THE BAGGAGE DOOR FRAME EXTENDING UP APPROXIMATELY 5 INCHES AS STATION 5741.00. THE REPAIR IS LISTED IN THE SRM AND WILL COMPLY WITH SRM 3C-A-53-42-01-02A-664A-D, LT SKIN FUSELAGE STA
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