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 CALA2022040600890Skin · dentedUPPER FUSELAGE SKIN FROM STA 807-827 STR 5L-6L DENT #17 REQUIRES PERMANENT REPAIR (REF. AAR NR 99927801).SDR V0XD20220405002Skin · damagedRH FUSE SKIN LIGHTNING STRIKES FS202.75 TO FS 661.00 STR 16-20 R- CORRECTIVE ACTION: PERFORMED PERMANT REPAIR TO AREAS AFFECTED IAW OLIVER WYMAN CAVOK EA 21-C953-0640 REB B DATE 03/28/2022 REPAIRS REQUIRE DTE WITHIN 12 MONTHS OF RTS DATE FOR THE SECTION III RESDR R61A2022040500236None · damagedRH HORIZONTAL STABILIZER BEARING FITTING DAMAGED ON I/B SIDE AROUND ENTIRE CIRCUMFERENCE. REPAIRED DAMAGE TO RH HORIZONTAL STABILIZER BEARING FITTING ON O/B SIDE BY BLEND OUT AND SPOT FACE PER ETD2022-170-009919.SDR R61A2022040500235Skin Panel · burnedFIVE LIGHTNING STRIKE WELD MARKS ON LOWER FUSELAGE SKIN FR 3-4, STGR 28L-28R. COMPLIED WITH 3 THROUGH DAMAGE REPAIRS, 1 FREEZE PLUG REPAIR, AND 1 DOUBLER REPAIR ON LOWER FUSELAGE SKIN FR3-4 STGR 28L-28R. REF ETD2022-170-010248 REV: C. SDR WRITTEN FOR DOUBLER RSDR R61A2022040500234None · damagedLH HORIZONTAL STABILIZER BEARING FITTING DAMAGED ON I/B SIDE AROUND ENTIRE CIRCUMFERENCE. REPAIRED DAMAGE TO LH HORIZONTAL STABILIZER BEARING FITTING ON O/B SIDE BY BLEND OUT AND SPOT FACE PER ETD2022-170-009927SDR SWIA202265846None · cracked* R/H WINDSHIELD SIDE POST SUPPORT CRACKED. (C-CHECK RO 6/1/2022) REMOVED AND REPLACED CRACKED R/H WINDSHIELD SIDE POST SUPPORT FITTING WITH NEW REF. CRJ 200 SRM 51-42-21 AND DWG #601R33007 REV -U. COMPLIED SKYWEST CARD 51-900-1003-SKY AND FORM M-337.SDR SWIA202265845None · cracked* L/H WINDSHIELD SIDE POST SUPPORT CRACKED. (C-CHECK RO 6/1/2022) REMOVED AND REPLACED L/H WINDSHIELD SIDE POST SUPPORT REF. CRJ200 SRM 51-42-21 AND DWG 601R33007 REV -U. COMPLIED WITH TASK CARD 51-900-1003-SKY.SDR JJBA20210404018None · noneAT CF IV AREA, CRACKS FOUND ON LH FRAME 59 BTW STR 15L-17L. LH SPLICE FR59 BTW STR 15L-17L REMOVED. AT CFIV AREA ON LH FRAME 59 BTW STR 15L-17L INSTALLED REPAIR SPLICE. DURING INSPECTION, FRAME REPAIR AND SPLICE FOUND TO BE FABRICATED WITH WRONG THICKNESSSDR JJBA20220404017None · noneAT REAR FUSE AREA, CORROSION FOUND ON FWD L-SHAPE CARGO DOOR SURROUND STRUCTURE AT FR65 AND BTW STR 16L-17L. AT REAR FUSE, AT FR65 BTW STR 16L-17L L-SHAPE IS OUT OF LIMITS. REPLACED WITH NEW PART SECTION AT REAR FUSE AREA ON FWD L-SHAPE CARGO DOOR SURROUND STRSDR JJBA20220404016None · noneCF1 REPAIR ON RH FLOOR BEAM AT FR 23 FOUND CORRODED. CF1 REPAIR ON RH FLOOR BEAM AT FR23 BLENDED OUT OF LIMITS. REMOVED CF1 REPAIR ON RH FLOOR BEAM AT FR23 FOR REPLACEMENT. FABRICATED REPAIR DOUBLER FOR RH FLOOR BEAM AT FR23. INSTALLED NEW FABRICATED REPAIR DOSDR NACA2022040400002None · noneEVIDENCE OF CORROSION AT LH FUSELAGE ABOVE LH HORIZONTAL STAB APPROX STA 1843, INSTALLED REPAIR AT LH FUSELAGE ABOVE LH HORIZONTAL STAB APPROX STA 1843 IAW AIRBORNE ENGINEERING DOC 47303-REA23SDR NACA2022040400001None · noneEVIDENCE OF CORROSION AT RH FUSELAGE ABOVE HORIZONTAL STAB APPROX STA 1843. PERFORMED REPAIRS AT RH FUSELAGE ABOVE HORIZONTAL STAB APPROX STA 1843 PER AIRBORNE ENGINEERING DOC # 47303REA22SDR CALA2022040600879None · corrodedAFT CARGO DOOR TORQUE BOX HAS MULTIPLE AREAS OF CORROSION ON UPP ER SURFACE ON HAECO LCQ REF 9296693/28693 SPEC A3NB-53-3-6217. N R GENERATED BY V079881 BLEND CORROSION, BEYOND ALLOWABLE LIMITS. REMOVED & REPLACED TOR QUE BOX COVER PLATE IAW A319 SRM 51-72-11-SDR CALA2022040600884Skin · dentedDENTS #1,2, AND 3 AT STA 360-380 STR 7L TO 9L REQ ALT REPAIR (RE F. AAR NR 99927731). SKIN INSTALLED BETWEEN STA 360 AND STA 380 FROM STR6L TO STR10L ON AC N38403 IAW THE LATEST REV OF ECRA 5331-02871. UPON THE ACCUMULATION OF 50,000 TOTAL FLIGHT CYCLES PERFORSDR JJBA20220404004None · noneSIGNS OF CORROSION AT RH SERVICE DOOR AT STRINGER 16 FRM ST20 AND 22 LWR FWD AND AFT CORNERS. REMOVED AND REPLACED SILL AT SERVICE DOOR AT STR 16 FR 20 AND 22SDR VNAA202204049992Skin · corrodedCORROSION ON EXTERNAL SKIN AT FWD FUSELAGE FAIRING SETTLEMENT AREA BTW. FS. 597 - FS. 693( UNDER ACCESS PANELS 191AB, 191BB, 192BB). SDR VNAA202204049991Skin · noneWEAR ON SKIN BELOW DOUBLER AT POTABLE WATER FILL PANEL FS. 953 - FS. 969 BTW STRG. 23L AND STRG. 24L
SDR CALA2022040400859None · cracked(SDR) RH FR16: DURING ROTO INSP OF RH FR16 DOUBLE JOGGLE, CRACK INDICATION WAS NOTED IN HOLES #B, #C, AND #D. V934344. ACCOMPLISH INITIAL INSPECTION OF FR16 LHS HOLES #C AND BEFORE THE AIRCRAFT REACHES 37,691 TOTAL AIRCRAFT FLIGHT 4,700 FLIGHT CYCLES THEREAFTESDR SWIA202265876None · chafedEVALUATE CHAFE ON SKIN DOUBLER JUST AFT OF FS977, STGR 27. (MARKED) (C-CHECK RO 6/6/2022) EVALUATED. ORIGINAL MATERIAL THICKNESS IS 0.063" REF. REO # 670-53-00-290, REV. -F DATED: 2019-04-26, MATERIAL LOST 0.020", REMAINING MATERIAL IS 0.043" NO DAMAGE SDR MASA20220426208Stringer · corrodedCORROSION ON STRINGER 23 RH BTW FS319.5-FS333, AT MAIN E/E COMPARTMENT.
STRINGER 23 RH BTW FS319.5-FS333, AT MAIN E/E COMPARTMENT WAS REPAIRED PER CRJ-900 SRM 53-00-03-201-001-A02SDR MASA20220426207Stringer · corrodedCORROSION ON STRINGER 21 RH BTW FS295-FS333, AT MAIN E/E COMPARTMENT.
STRINGER 21 RH BTW FS280 TO FS333 WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-20-001-001-A01SDR MASA20220411182None · corrodedCORROSION ON STRINGER 19RH BTW FS295-FS330, AT MAIN E/E COMPARTMENT.
CORRECTIVE ACTION: STRINGER 19RH BTW FS295-FS330 WAS REPLACED PER CRJ900 SRM 53-00-03-201-001-A02.SDR CALA2022040400871Floor Support · corroded(A3NB-05-3-6049) MAIN CABIN, FLOOR CABIN STRUCTURE HAS CORROSION AT FR20 DOT 132-98() BLEND OUT AREA AT MAIN CABIN STR FR20 -Y1588 ORG. THICKNESS 0.07 6 AND INSTALLED FLOOR CABIN WEB IAW SRM 51-42-1144-008. ACCOMPLI 1", MAT REMOVED 0.020, MAT REMAINING 0.051" SDR CALA2022040400870Beam · corroded(A3NB-05-3-6049) MAIN CABIN, FLOOR CABIN SEAT TRACK HAS CORROSIO N AT FR 20 -Y765 DOT 132-99() EVALUATED BLENDING OUT IAW SRM 51-42-15 FOUND TO BE OUT OF LIMIT S AND REMOVED AND INSTALL NEW SEAT TRACK -Y765 FR20 ON FLOOR CAB IN IAW SRM 51-42-11/001. ACCOMPLISHSDR VNAA202204039994Skin · wornWEAR MARKS ON DOUBLER AND TRIPLER REPAIR FS. 969 -FS. 985 BETWEEN STRG. 26L AND 26R.
CORRECTIVE ACTION:WEAR MARKS ON DOUBLER AND TRIPLER REPAIR FSSDR VNAA202204039992Skin · corrodedCORROSION ON EXTERNAL FUSELAGE SKIN BETWEEN FS. 1015- FS. 1031 ON STRG.24R AROUND DRAIN.
CORRECTIVE ACTION: CORROSION ON EXTERNAL FUSELAGE SKIN BETWEEN FS. 1015- FS. 1031 ON STRG. 24R AROUND DRAIN. WAR REPAIRED PER EA 22-C7-53-192 REV.IRSDR SWIA202265805None · corrodedAFT GALLEY 2 SUPPORT BRACKET, PART# SH670-41512-1, ATTACHED TO STRG 21R AND STRG. 20R APPROX. FS 372.00 IS CORRODED. (C CHECK RO 5/23/22) AFT GALLEY 2 SUPPORT BRACKET, PART# SH670-41512-1, ATTACHED TO STRG 21R AND STRG. 20R APPROX. FS 372.00 IS CORRODED SDR SWIA202265804None · corrodedAFT GALLEY 2 SUPPORT BRACKET, PART# SH670-41511-5, ATTACHED TO STRG 21R AND STRG. 20R APPROX. FS 372.00 IS CORRODED. (C CHECK RO 5/23/22) AFT GALLEY 2 SUPPORT BRACKET, PART# SH670-41511-5, ATTACHED TO STRG 21R AND STRG. 20R APPROX. FS 372.00 IS CORRODEDSDR SWIA202265383None · crackedLH MLG - FRAME 52 "L" ANGLE CRACKED. (C CHECK RO 4/16/22) REMOVED AND REPLACED LH MLG - FRAME 52 "L" ANGLE REF SRM 51-40-08. RESTORED SURFACE PROTECTION REF SRM 51-23-06SDR COEA2022052406901Web · corrodedWO 235601 NR 100043 HEAVY CHECK COE/MAJOR REPAIR: INTERNAL FUSELAGE, CREASE BEAM WEB BETWEEN L/H FRAMES 13-14 HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: CREASE BEAM WEB REPLACED WITH NEW PER ATR SRM.SDR COEA2022052405901None · damagedWO 235601 NR 100042 HEAVY CHECK/MAJOR REPAIR: INTERNAL FUSELAGE L/H FRAME 13, FRAME FLANGE IS DAMAGED BETWEEN STRINGER 14-15. CORRECTIVE ACTION: SPLICE REPAIR AT FRAME 13 IAW ATR SRM 533140-300-803-A01.SDR COEA2022052404901Floorbeam · corrodedWO 235601 NR 100029 HEAVY CHECK COE/MAJOR REPAIR: FLOORBEAM 13 LOWER SURFACE OF UPPER ANGLE HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: SPLICE REPAIR PER SRAS ES_0158021_01...18918 ISSUE A, DATED 5/6/2022.SDR COEA2022051703901Intercostal · corrodedWO 235601 NR 100028 HEAVY CHECK COE/MAJOR REPAIR: FLOORBEAM 10 LOWER SURFACE OF UPPER ANGLE HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPLACED FLOORBEAM INTERCOSTAL WITH NEW IAW SRM 51-25-02.SDR COEA2022051702901Floorbeam · crackedWO 235601 NR 100009 HEAVY CHECK COE/MAJOR REPAIR: L/H LONGITUDINAL FLOORBEAM CRACKED BETWEEN FRAMES 27-28. CORRECTIVE ACTION: REPAIRED PER EO 5315-01.SDR R61A2022042000284Seat Track · corrodedCF III RH I/B SEAT TRACK AT XBEAM FR 84 CORRODED. R&R IAW EMB 170/175 SRM 53-23-10.SDR JJBA20220401001None · noneCABIN LATERAL FLOOR SUPPORT BETWEEN FRAMES 48-52 AT STRINGER 15R HAS SIGNS OF CORROSION. REMOVED AND REPLACED CABIN LATERAL FLOOR SUPPORT BETWEEN FRAMES 48-52 STRINGER 15RSDR IXXA2022040101Rub Strip · crackedREPAIR - CHAFE STRIP BEHIND ENGINE MOUNT ACCESS PANEL 436AL BROKEN OFF NAC 203-NAC 203SDR HNAA2022041300155None · noneE907210 - EVIDENCE OF CRACK AT TWO FASTENERS ON THE LH SIDE AT FRAME 78 .... INSTALLED SKIN BUSHING (1 LOCATION) ON THE LH SKIN AT FRAME 78 AT LOWER FASTENER LOCATED 1" BELOW STR 6L IAW EMB145 SRM 53-32-01RE, ITEM 9, FIG 213 AND EO1-53-22-0053.SDR JJBA20220331053None · nonePASSENGER DOOR FRAME HAS SIGNS OF CORROSION UNDER THRESHOLD FR15-FR18. REMOVED AND REPLACED SHAPE YSDR YENA2022040100322None · noneFLT#108, MBJ-EWR. 'DIRTY SOCK SMELL. SUSPECT PACK 2 OR ENGINE 2 WITH ENG RUN IN JAMAICA; REF. LOG PAGE 3270652 ITEM 1 & 2 (PERFORMED HOT PACKS BURN AND DECONTAMINATION AND INSPECTION OF THE APU, ENG #1 AND #2 FOR OIL EVIDENCE IAW STM 05-50-00-810-831-A. FALLOWSDR CALA2022033100851Frame · noneFR35-36 ON R/H PRESS PANEL HOLES CRACKED. ECRA 5331-02868 PART 1.3, PLANNING TO CONTACT EG AFTER 70,336 TTFC, OR 150,519TTLFH, WHICHEVER COMES 1ST, BUT BEFORE 71,336TTFC OR 151,519 TTLFH WHICHEVER COMES 1ST FOR ECRA 5331-02868 INSPECTION REQUIREMENTS. 71,336TTSDR UIEA2022033000257Seat Track · corrodedM/D STA 1840 RBL 77 SEAT TRACK CROWN FOUND CORROSION.(<P>M/D STA 1840 RBL 77 SEAT TRACK CROWN CORROSION REMOVED IAW IAI SRM 51-10-02 AND REPORTECTED IAW IAI SRM 51-20-01, CHECKED WITHIN IAI SRM 53-00-52 ADL 1, FIG 101</P>)SDR UIEA2022033000256Seat Track · corrodedM/D STA 1820 RBL 77 SEAT TRACK CROWN FOUND CORROSION(<P>M/D STA 1820 RBL 77 SEAT TRACK CROWN CORROSION REMOVED IAW IAI SRM 51-10-02 AND REPORTECTED IAW IAI SRM 51-20-01, CHECKED WITHIN IAI SRM 53-00-52 ADL 1, FIG 101</P>)SDR UIEA2022033000255Seat Track · corrodedM/D STA 1800 RBL 77 SEAT TRACK CROWN FOUND CORROSION(<P>M/D STA 1800 RBL 77 SEAT TRACK CROWN CORROSION REMOVED IAW IAI SRM 51-10-02 AND REPORTECTED IAW IAI SRM 51-20-01, CHECKED WITHIN IAI SRM 53-00-52 ADL 1, FIG 101</P>)SDR UIEA2022033000254Shear Web · crackedM/D STA 140 LH STR 26 FLOOR WEB FOUND CRACK APPROX 1.3"(<P>M/D STA 140 - STA 160 L/H FLOOR TO SKIN SHEAR WEB CRACK AREA REPAIRED IAW SRM 53-10-51-2R-7 REPAIR 7 REV 114 20 FEB 2022</P>)SDR FDEA202203300765Angle · crackedAREA AFT OF BULK CARGO, MAIN CABIN FLOOR SUPPORT STRUCTURE SPLICE IS CRACKED BETWEEN STA 1562 AND 1582 AT APPROX. RBL 80. REMOVED ANGLE AND REPLACED WITH NEW ANGLE IAW BAC DWG 146T5650, REV. C.SDR EVCA0330222Stiffener · crackedLH FS145 STIFFENER CLIP CRACKEDSDR EVCA033022None · crackedTHERE IS A SMALL CRACK, (1/4 INCH LONG), FORWARD LH SIDE THAT WE WILL STOP DRILL.SDR CALA2022033100847Frame · noneDURING ROTO INSP OF "LH" FR35 STGR30 A CRACK INDICATION WAS NOTE D ON AFT LOWER HOLE. INTERIM REPAIR WAS ACCOMPLISHED PER ECRA 5321-02067 REF VT MAE NR0024388. EXTERNAL ANGLE FITTING BEFORE AC4010 REACHES 61391TFC / 132942TF ECRA 5321-02067 H WHICHEVER OCCURS SDR CALA2022033100846Frame · noneDURING ROTO INSP OF "RH" FR35 STGR30 A CRACK INDICATION WAS NOTED ON AFT LOWER HOLE #2RH FR35 STGR30 DIP CREATED PER STEP 36 OF ECRA 5321-02067 REF VT MAE NR0024389 132942TFH WHICHEVER OCCURS FIRST PER PART 2.1 OF THE LATEST RE OF ECRA 5321-02067 INTERIM REPAI
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