JASC 5300
Service difficulty reports · 8,206
Reports filed under 5300 · Fuselage Structure (General), 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 = '5300' 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 = '5300' 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 MASA20211130596Skin · dentedAIRCRAFT'S FWD FUSELAGE, LH SIDE WAS STRUCK BY VENDOR WITH SCISSOR LIFT CAUSING DAMAGE TO SKIN (LARGE DENT IN SKIN).
NDT INSPECTIONS PERFORMED AND ALL DAMAGE (DENT IN SKIN) REPAIRED PER EMBRAER ETD2021-170-039036 REV.:/.
NO DEFECTS NOTED. THIS IS A PERM REPSDR JR2R20218327581Seat Track · corrodedSEAT TRACK BEAM P/N 170-03263-001 CORRODED BETWEEN FR13 AND FR14SDR MASA20211129586None · dentedFUSELAGE LOWER SKIN PANEL BETWEEN FS1047.0- FS1051.0, STR. 22L- STR. 23L WAS FOUND WITH A DENT. PERFOMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-61-01 , EA 20-2021-198.SDR MASA20211129584None · noneFUSELAGE LH SKIN PANEL BETWEEN FS501 & FS525 AND STGR14L & STGR15L WAS FOUND TO HAVE PREVIOUS BLENDOUTS. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-31-01, FIGURE 53-31-01-99-804, ITEM 1, EA 85-2021-003.FS501 & FS525 / STGR14L & STGR15LSDR HALA2021112900176None · noneC-CHECK - DURING REP HFEC INSPECTION GP306929-1 - FOUND MATERIAL FLAW INDICATION AT L/H WINDOW BELT BETWEEN STA 598 AND STA 617 FWD UPPER CORNER // E105-475407-PERM ISSUED. PERFORM HFEC SURFACE INSPECTION ON THE INTERIOR AND EXTERIOR SURFACE OF THE SKIN, PER SDR JR2R20211129564Shear Panel · corrodedRH SHEAR PANEL CORRODED AT FR88SDR JR2R20211129570Shear Panel · corrodedCENTER SHEAR PANEL IS CORRODED AT FR88SDR JR2R20211129575Beam · corrodedFLOOR BEAM CORRODED AT RBL9 AND FR87SDR JR2R20211129377Angle · crackedLH WHEEL WELL FR52 STUB ANGLE CRACKEDSDR JR2R20211129574None · corrodedFLOOR SUPPORT CLIP CORRODED AT RBL36 AND FR87SDR CALA2021112902184Floor Support · corrodedFLOOR SUPPORT STRUCTURE AT STA 365 RBL 25 FOUND TO BE CORRODED. REF AMES ILN N/R 139533-0200-0224. REMOVED AND REPLACED FLOOR SUPPORT STA 365 RBL 25 IAW SRM 51-40- 02 AND BOEING DWG 141N5130. SEE AMES ILN N/R 139533-0200-0224 FOR DETAILS OF WORK ACCOMPLISH ED.SDR CALA2021112902182Door Sill · corrodedR2 DOOR SILL HAS CORROSION AR FR66. PER HAECO LCQ NR 9292548/205 48 GENERATED BY V061742. REMOVED AND REPLACED R2 DOOR SILL FR 66-68 IAW A319 SRM 51-72-11 -911-001. ACMP BY MECH V061742 INSP BY V077960SDR CALA2021112902180Drain · unserviceableREF LP 7489334, AFT BILGE AREA FROM BODY STA 727+4 TO BODY STA 1006 BETWEEN BUTT LINE S21L AND S24L WILL REQUIRE "IN-DEPTH CLEANUP". AND S24L. WITHIN 7 DAYS, ACCOMPLISH EC/RA 2011-01000, GALLEY SPILL, SECTION 2.B., IN-DEPTH CLEANUP, IN THE APPROXIMATE AREA FROSDR R61A2021120901004Splice · corrodedCORROSION FOUND ON AFT WET AREA FLOOR SPLICE AT FR 88, LH SIDE. REPLACED IAW SRM 51-42-02SDR UIEA2021111902425Doubler · noneUPON REOMOVAL OF EXISTING DOUBLER #2 PYLON FOUND ELONGATED HOLE ON THE PYLON WEB BOTTOM(<P>REMOVED AND REPLACED DOUBLER,FILLER,AND 2EA. ANGLES ON #2 PYLON STRUT FWD UPPER SPAR WEB. REPAIRED ELONGATED HOLE IAW B767 FAS 21091 REV:IR SRM 51-40-02, 51-40-05, 51-20SDR UIEA2021111902427None · noneMAIN CABIN CENTER WING UPPER SURFACE HAS AREA OF CORROSION AT BS 954 RBL 75. DOT 024(<P>REPAIRED CORROSION AT MAIN CABIN CENTER WING SKIN UPPER SURFACE STA 954 RBL 75 IAW FVCI EO: 21194 REV:IR</P>)SDR A6WA202111277988None · noneWHEN REMOVING FIXED BALLAST FOUND CORROSION IN SEAT TRACK FROM F.S 559+112 TO 574 R/H O/B SEAT TRACK ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION FROM SEAT TRACKSDR CALA2021112902177Fitting · crackedLT MLG DOOR ACTUATOR FITTING HAS CRACK INDICATION IN FWD OB HOLE (IN ACT FITTING LAYER) AD RELATED SUPPORT TASK: PER HAECO LCQ N/ R 9296413/30413 GENERATED BY V892444. ACCOMPLISHED REPAIR LT MLG DOOR ACTUATOR FITTING IAW ECRA 5330-0 6886/REO-L23354 REV 1R. REQSDR SWIA202164117None · corroded*AFT CARGO FLOOR SILL SUPPORT ANGLE AT APPROX. FS.1047 TO FS.1051 STRG 17L HAS CORROSION (MARKED) (C CHECK RO 02-03-22) REPAIRED AFT CARGO FLOOR SILL SUPPORT ANGLE AT APPROX. F.S 1047 TO F.S 1051 STRG 17L REF REO 670-53-61-2018 REV-- DATED 2021-12-06SDR SWIA202164116None · corroded*AFT CARGO DOOR SILL AT APPROX. FS.1000 TO FS.1047 HAS MULTIPLE SPOTS OF CORROSION (MARKED) (C CHECK RO 02-03-22) REMOVED AND REPLACED AFT CARGO DOOR SILL BETWEEN FS 1000 - 1047 IAW CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-21-001-001-A01, CRJ700 SSDR CALA2021112902175Door Sill · corrodedR2 DOOR SILL SHAPE SILL IS CORRODED PER NR 9292359 / 20359 GEN B Y V892442 SPEC # A3NB-53-3-6187 RMVD AND RPLD R2 DOOR SHAPE SILL IAW SRM 51-72-11-911-002 REPAIR ED TOPCOAT IAW SRM 51-85-12-911-002 BY MECH V061742 INSP BY V077 960SDR EE4Y2021112614434Stringer · corrodedDURING THE STRUCTURAL INSPECTION IT WAS FOUND AT CENTER FUSELAGE III, BETWEEN FR85 AND FR86, AND BETWEEN FR89 AND FR90 THE STRINGER 23L WITH CORROSION ON HORIZONTAL FLANGE ONLY, THE DAMAGE
WAS REPAIRED INSTALLING REPAIR DOUBLER AS PER E.O. # COO-EO-2021-1431SDR MK1Y20211126003None · noneDURING MAINTENENCE INSPECTION FOUND EXISTING SKIN REPAIR DAMAGED WITH CORROSION ON FUSELAGE OUTER SKIN AT STA 1809.5, STR 39L.SDR JJBA20211125047Unknown · unknownRH FWD FUSELAGE I, TWO LIGHTING STRIKES SUSPECTED BTW FR 1A & 2 AND ABOVE STR 13R. DURING LIGHTING STRIKE INVESTIGATION MULTIPLE STRIKE SPOTS BLENDED WITHIN LIMITS, SOME ACCEPTED AS IS AND 2 BLEND OUT FOUN OUT OF LIMITS AND NEED A EXTERNAL DOUBLER REPAIR. FIRSSDR JJBA20211125045Unknown · unknownMULTIPLE DENTS FOUND ON EXTERNAL SKIN OF MAIN DOOR BTW STR 06L AND STR 08L, STR 12L AND STR 15L. MULTIPLE DENTS ON EXT SIGN OF MAIN DOOR BTW STR 06L-08L AND STR 12L-15L STRIPPED FOR INVESTIGATION ON EXT SKIN OF MAIN DOOR BTW STR 06L-08L AND STR 12L-15L DENTS 1SDR JJBA20211125044None · noneCF1, SKIN FOUND WITH EXISTING BLEND BTW FR 20-21 STR 11-12L. CF1, SKIN BTW FR 20-21 AND STR 11-12L FOUND BLENDED OUT OF LIMITS. REPAIR WAS MADE.SDR GTIA2021112636144None · nonePER WEEKLY R2 AND L2 DOORS EMER ASSIST BOTTLE REQ SERVICE.-SERVICED R2 AND L2 DOORS EMER ASSIST BOTTLE IAW AMM 52-10-00.SDR SWIA202163997None · corroded* CORROSION SPOT ON INTERIOR SKIN DOUBLER IN AVIONICS BAY BEWEEN STR.25R AND 26R AT APROX. FS.337.00 (MARKED). (C-CHECK RO 1/19/2022) REPLACED INTERIOR SKIN DOUBLER AT APPROX STGR 25R - STGR 26R, FS337 REF NCR C808091944 DATED 22-OCT-2008. COMPLIED WITHSDR SWIA202163995None · corrodedT-CAS DOUBLER CORRODED BETWEEN FS 295.00 AND 310.00 (C-CHECK RO 1/19/2022) REMOVED AND INSTALLED NEW T-CAS DOUBLER REF CRJ 900 SRM 51-42-06-001-001-A01,51-42-21-001-001-A01 AND DRAWING SH670-30023 REV G. / COMPLIED WITH TASK 51-900-1002-SKYSDR SWIA202162955None · damagedTRANSFER FROM EAML 788798 : REF EAML 787361 FOR BIRD STRIKE IMPACT, FOUND DENT OUT OF LIMITS MEASURING APPROX 4"L X 4.75"W X 0.094"D ON FUSELAGE SKIN ON LEFT SIDE BETWEEN FS193.00 - FS202.75 ABOVE STR 13L (FLIGHT 3270 - FILED CLOSED) REMOVED AND REPLACED SDR FDEA202111242982Seat Track · corrodedTHE Z220 FLOOR SEAT TRACK FR14-FR19 Y-953 WAS FOUND CORROSION. REPLACED THE CORROSION SEAT TRACK WITH NEW PART. I.A.W. A300-600 SRM 51-72-10-001 PAGE.2, 51-40-21-001 PARA.7 PAGE.24-50.SDR JJBA20211124043None · noneCENTER FUSE II, FRAME 25 CRACKED BTW STR 16R-15R. FRAME REPAIREDSDR JJBA20211124041None · noneCRACK FOUND ON LH FRAME 59 BTW STR 15L-16L IN CF IV AREA. FRAME REPAIREDSDR SWIA202162752None · damagedFOUND DAMAGE TO PAX DOOR INNER SKIN AT DOOR ASSIST MOTOR PULLEY ON AFT SIDE OF DOOR TO BE OUT OF LIMITS PER SRM 52-11-01, THIS HAS BEEN DETERMINED TO BE A MAJOR REPAIR PER GMM 3-26. SEE CP 23892009 FOR DETERMINATION OF MAJOR OR MINOR REPAIR. (FILED - CLOSEDSDR 2A6D2021112409703Latch · crackedLH CREW DOOR LOWER LATCH SUPPORT SHELL CRACKEDSDR SWIA202164184None · corroded* AFT FUSELAGE WING TO BODY SUPPORTS, CONNECTING ANGLE CORRODED AT APPROX. FS 939.00, BL 0.0. (C CHECK RO 02-03-22) REMOVED AND REPLACED AFT BODY FAIRING WING TO BODY SUPPORT ANGLE REF CRJ700 SRM 51-42-06-001-001-A01SDR SWIA202164183None · corrodedPAX DOOR STEP BOTTOM ANGLE HAS CORROSION (C CHECK RO 02-03-22) REMOVED CORRODED PAX DOOR BOTTOM ANGLE AND INSTALLED NEW STEP BOTTOM ANGLE AT PAX DOOR REF CRJ700 SRM 51-42-06-001-001-A01 AND SRM 51-42-10-001-001-A01SDR MASA20211124578None · corrodedUPPER CAP OF THE RBL9.00 AFT FLOOR BEAM AT FS693.00 WAS FOUND TO HAVE CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-31-43-001-001-A03, FIGURE 53-31-43-991-801, ITEM 7, EA 79-2021-260.SDR MASA20211124577None · noneFUSELAGE LOWER SKIN PANEL BETWEEN FS565 & FS581 AND STGR21R AND STGR22R WAS FOUND TO HAVE A PREVIOUS BLENDOUT. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-31-01, FIGURE 53-31-01-99-806, ITEM 1, EA 72-2021-217.SDR MASA20211124576None · noneFUSELAGE LOWER SKIN PANEL BETWEEN FS597 & FS629 AND STGR20L & STGR22L WAS FOUND TO HAVE PREVIOUS BLENDOUTS. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-31-01, FIGURE 53-31-01-99-806, ITEM 1, EA 72-2021-216.SDR CALA2021112302166Skin · dentedREF LP 5057224 FOR ORIGINAL WRITE UP. DENT LOCATION IS STA 312-325 BETWEEN STR 27L-27R. DENT MEASURES 4.3"X3.5"X0.125"D OVER A SHEAR TIE. DAMAGE W/Y FOUND TO BE 28, OUT OF LIMITS FOR NO REPAIR NECESSARY REMOVED FASTENERS COMMON TO DAMAGE IAW AVO 8607 STEP 11. SDR CALA2021112302164Joint · corrodedAFT VARGO COMPT BILGE AREA EXISTING STRINGER REPAIR AT FRAME 55- 56 STR 43LH HAS CORRISION. TABLE 008. REPAIRED AFT CARGO STRINGER SPLICE AT FRAME 55-56 STR 43 LH IAW A320 SRM 53-00-13-300-001. INSPECTION THERSHOLD FROM TIME OF ADL /REPAIR EMBODIMENT 60,000FC/SDR SWIA202164107None · dented* LOWER FUSELAGE SKIN AT APPROX. FS 985.00, BL 0.0 HAS 2 DENTS. (C CHECK RO 02-03-22) CUT OUT DENTS AND APPLIED DOUBLER TO LOWER FUSELAGE SKIN AT APPROX FS985, STGR27 REF REO 670-53-00-290 REV -F 2019/04/26 AND REO 670-53-00-680 REV -- 2021-12-30. / COMPLSDR CALA2021112302163Beam · corrodedA3NB-53-3-6038 CABIN FLOOR STRUCTURE SUPPORT BEAM HAVE CORROSION FR 16 Y518 DOT 42-052 () REMOVED AND REPLACED CABIN SUPPORT BEAM AT FR12-24 Y518 IAW SRM RUDDER IAW AMM 27-24-00-710-001-A CHECK GOOD ACCOMPLISHED BY EMP 51-42-11 & SRM 51-21-14. INSTALLED CABLE SDR MASA20211123573None · noneFUSELAGE SKIN BETWEEN FS897.00 - FS927.00, STGR27, WAS FOUND WITH (2) PREVIOUS BLEND OUTS. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-51-01-001-003-A02, FIGURE 53-51-01-991-806, ITEM 1, D, EA 79-2021-257.SDR IXXA202112210001Stringer · damagedNR 0200-0090 R/H FRAME STA 859 THE FRAME INNER CHORD
IS CRACKED ON LOWER END COMMON TO THE
STUB BEAM. (VERIFIED WITH HFEC SURFACE
SCAN.)SDR GTIA2021112236135None · noneR4 DOOR ASSIST BOTTLE LOW-SERVICED R4 DOOR ASSIST BOTTLE IAW AMM 52-10-00. LEAK CHECK GOOD, NO DEFECTS NOTEDSDR R61A2021120800995Shear Tie · corrodedLEVEL 2 CORROSION FOUND FWD FUSELAGE LOWER SHEAR CLIPS AT FR17 BETWEEN STRG 25L AND STRG 26L. CLIP WAS REPLACED IAW SRM 51-41-01SDR R61A2021120800994Shear Tie · corrodedLEVEL 2 CORROSION FOUND FWD FUSELAGE LOWER SHEAR CLIPS AT FR16 BETWEEN STRG 24R AND STRG 25R. CLIP WAS REPLACED IAW SRM 51-41-01SDR IPXA2021112076182Tie Down · corrodedINSPECTION TYPE:SEGAFT CARGO COMPARTMENT ON RH SIDE STA 1200-1380 TRANSITION PANEL HAVE 2 FITTINGS CORROTED..REMOVED AND REPLACED 2 EA FITTINGS IAW B-757 SRM 51-40-02-0G
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