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 R61A2022092300565None · corrodedLOWER CF III SHEAR CLIP CORRODED FWD OF WASTE SERVICE BOX AT FR 88, STGR 27R TO STGR 26R REMOVED CORRODED SHEAR CLIP AND INSTALLED NEW SHEAR CLIP FWD OF WASTE SERVICE BOX AT FR 88, STGR 27R TO 26R, RESTORED SURFACE PROTECTION AND APPLIED CIC. REF EMB 175 SRM SDR JJBA20220908006None · noneCRACK SUSPECTED (14X) ON RH SKIN AROUND SEVERAL FASTENERS BTW FR 77-80 BTW STR 3R-9R. PAINT STRIPPED ON RH SKIN BTW FR 77-80 AND BTW STR 3R-9R. (8X) CRACKS FOUND AROUND RIVETS ON RH REAR FUSE SKIN BTW FR77-80 AND BTW STR 3R-9R NEED TO BE REPAIRED ON RH REAR FUSDR DALA2022090605950None · noneSHIP 654 DENT ON FRAME STA 1320 AT STGR 26R IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00194: DENT ON FRAME STA 1320 AT STGR 26R IN AFT CARGO COMPARTMENT WAS REPAIRED PER B757-200 SRM. (2390350)SDR YENA2022090600876None · noneDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE ATTACHMENT AREA CONTINUITY FITTING, LH SIDE, CRACK LENGTH IS 0.200 INCHES APPROX IN COCKPIT (1 EA); REF AEROMAN N/R 2022-408601 WO 2022-178/1 REMOVED AND REPLACED CONTINUITSDR YENA2022090600875None · noneDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE ATTACHMENT AREA CONTINUITY FITTING, RH SIDE, CRACK LENGTH IS 0.200 INCHES APPROX IN COCKPIT (1 EA); REF AEROMAN N/R 2022-408602 WO 2022-178/1 REMOVED AND REPLACED CONTINUISDR 2022F00346None · noneRESULT OF AD 2012-26-02 INSPECTION, CRACK WAS FOUND ON S10RH BETWEEN BS 500 AND BS 500ASDR DALA2022090205905None · noneSHIP 654 DENT ON FRAME STA 1320 AT STGR 26R IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00194: DENT ON FRAME STA 1320 AT STGR 26R IN AFT CARGO COMPARTMENT WAS REPAIRED PER B757-200 SRM. (2390341)SDR CALA2022090202251Skin · noneRIGHT RIGHT INBOARD MAIN FLAP HAS NUMEROUS DENTS DUE TO HAIL REF SRM 57-53-01-1A-1, NO DELAMINATION NOTED FLAP, MULTIPLE DENTS DUE TO HAIL DAMAGE, NO DELAMINATION NOTED. ITEM LOCKED FOR MAINT FERRY UNLOCKED LP FOR UPDATES INDICATING THAT THE REMAINING DENTS AFSDR CALA2022090202250Skin · brokenMRD BROKEN MRD *IAH 03-1402Z* FOR AIRCRAFT 0218 BROKEN ON 12AUG22 10:09:39 ON FLIGHT 1895 FROM IAH TO PHX. REASON: LOG PAGE 9288556 CREATE D NO FURTHER MAINTENANCE ACTION NEEDEDSDR IXXA2022090102Bracket · corrodedBRACKET CORRODEDSDR IXXA2022090101Pressure Web · corrodedRWW PRESSURE DECK CORRODEDSDR K11A2023033100200Seat Track · corrodedEVIDENCE OF CORROSION ON SEAT TRACK AT STA 5D-480 46 INCHES LEFT OF 0-BL.SDR K11A2023032900196Seat Track · corrodedFUSELAGE FLOOR STRUCTURE - SEAT TRACK BETWEEN STA 887 AND STA 867 LBL 58" HAS EVIDENCE OF CORROSION.SDR K11A2023032700191Unknown · corrodedFUSELAGE FLOOR STRUCTURE - SEAT TRACK BETWEEN STA 807 AND STA 827 RBL 46" (APPROX 19" IN LENGTH) HAS EVIDENCE OF CORROSION.SDR K11A2023032400188Unknown · corrodedEVIDENCE OF CORROSION ON SEAT TRACK AT STA 500 60 INCHES RIGHT OF 0-BL.SDR SWIA202266387None · dentedREF EAML 983241 FOR RAMP DAMAGE TO FWD FUSELAGE SKIN BETWEEN FRAMES 21-22 AND STRINGERS 16L-17L, FOUND SKIN PUNCTURE / DENT TO BE DETERMINE OUT OF LIMITS PER ERJ 175 SRM 53-10-01 MEASURING DEPTH .1614" (4.10MM), LENGTH 1.403", WIDTH 0.967". (FILED CLOSED) SDR SWIA202266386None · dentedREF EAML 983241 FOR RAMP DAMAGE TO FWD FUSELAGE SKIN BETWEEN FRAMES 21-22 AND STRINGERS 16L-17L FOUND SKIN DENT TO BE DETERMINE OUT OF LIMITS PER ERJ 175 SRM 53-10-01 MEASURING  DEPTH .012" (0.30MM), LENGTH .967", WIDTH .152" (FILED CLOSED) THIS DISCREPSDR SWIA202266385None · dentedREF EAML 983241 FOR RAMP DAMAGE TO FWD FUSELAGE SKIN BETWEEN FRAMES 21-22 AND STRINGERS 16L-17L FOUND SKIN DENT TO BE DETERMINE OUT OF LIMITS PER ERJ 175 SRM 53-10-01 MEASURING  DEPTH .011" (0.28MM), LENGTH .562", WIDTH .625" (FILED CLOSED) THIS DISCRESDR SWIA202266384None · dentedREF EAML 983241 FOR RAMP DAMAGE TO FWD FUSELAGE SKIN BETWEEN FRAMES 21-22 AND STRINGERS 16L-17L, FOUND SKIN DENT TO BE DETERMINE OUT OF LIMITS PER ERJ 175 SRM 53-10-01 MEASURING  DEPTH .0105" (0.27MM), LENGTH .745", WIDTH 1.471" (FILED CLOSED) THIS DISSDR DALA2022090205902None · noneSHIP 654 PERFORM PERMANENT REPAIR, ON FUSELAGE SKIN, STA 680 BTW S-20L TO S-22L. CORRECTIVE ACTION: SUMMARY OF NRC 00619: PERMANENT REPAIR WAS PERFORMED PER B757- 200 SRM. (2388653)SDR CALA2022090202245None · noneRII INSPECTION REQUIRED - NO REMARKS ENTERED NEED EDDY CURRENT ON #1 WINDOW UPPER LH CORNER FOR CRACK VERIFICATION. PERFORMED HFEC INSPECTIONS OF WINDOWS 1 AND 2 IAW EA 5310-04554 REV. B STEPS 9.1 TO 10.4. NO ADDITIONAL CRACKS NOTED. ALSO IAW NTM 6-51-00-00 PSDR CALA2022090202243Beam · nonePASSENGER CABIN, BETWEEN FR16 AND Y518, RAIL DUMMY HAS CORROSION RMEOVED CORROSION ON RAIL DUMMY AT FR16 T518 IAW SRM 51-74-00, F SRM 51-75-12. EMP: V933986 WC: 36250 STA: ST ENG BFM OUND WITHOUT OF LIMITS IAW SRM 51-11-14-203-007, MEASURE: L=1.90 0", W=1.4", SDR CALA2022090202242Skin · corrodedAFT DRAIN MAST AND FUSELAGE AT ATTACH POINT IS CORRODED. MARKED. REPAIRED AFT FUSELAGE SKIN F.S. 1661-1681 S25R-26R IAW AMES REA 47518REA01 REV A AND UAL ECRA 5360-01663.INSTALLED A NEW DRAIN MAST PN 75-3831-3-0004 IAW B757 AMM 28-31-01-404. REPAIRED AFT FUSELSDR CALA2022090202240None · crackedREFERENCE AMES NR 147450-0200-0166. FUSELAGE FRAME IS CRACKED STA 760 STRINGER 8L. REF AMES NR 147450-0200-0166. REPAIRED FRAME AT STATION 750 STR 8L IAW B757-200 SRM 53-00-07-2 R-8 SEE PARTIAL WORKSHEETS 1 AND 2 FOR PARTIAL WORK ACCOMPLISHED , PARTIAL WORKSHESDR 2A6D20220831001Frame Angle · elongatedDAMAGE TO THE FRAME WAS DISCOVERED IN THE FORM OF AN ELONGATED HOLE TO FRAME AT STA X4709SDR IPXA2022092186475Angle · noneINSPECTION TYPE:3CCABIN FLOOR BEAM HAS A MISS DRILLED HOLE NEXT TO IT STA Y=515 AND X=-10 AND Z=-18REPAIRED MISS DRILLED FLOOR BEAM AT STA Y=515 AND X=-10 , Z=-18 IAW VTSAA EA 011-5320-01-A9685 I/R AND UPS MD11-5310-84693-A FAA FORM 8100-9 (MAJOR)SDR IPXA2022091086102Panel · brokenINSPECTION TYPE:A300PANEL 143CF HAS COMPOSITE DELAMINATED AND BROKEN AT SEVERAL LOCATIONS (WATERCVINSIDE)FAB PANEL 143CF P/N 5024N400001SS-G PER (SREO) A300-5320-57698-ASDR Y2PA2022090622047Skin · corrodedDISCREPANCY: DURING C-CHECK AT COMMERCIAL JET IN KDHN, CORROSION FOUND ON FUSELAGE SKIN INTERNAL DOUBLER AT DRAIN VALVE MOUNTING SURFACE AT STATION 157 SDR YENA2022090200860None · noneFLT#777, BOS-LAS. 'LEVEL 1 ODOR EVENT REPORTED BY INFLIGHT IN CRUISE SMELLED LIKE PAINT MID CABIN FIRST THEN AFT WOULD COME AND GO BRIEFLY NO SMOKE OBSERVED. CA ALSO SMELLED IN DESCENT AT 18KFT AND PERFORMED ECOM ISOLATION W X BLEED SHUT AND PACK 1 OFF AND ODOSDR UIEA2022082500893Structure · crackedRH STA 2231 FWD INNER CHORD S-26R AREA FOUND 1EA CRACK APPROX 1/4" IN LENGTH(<P>REPAIRED IAW SRM 53-60-07-2R-7 REPAIR 7</P>)SDR UIEA2022082400891Panel · damagedAFT CARGO STA 1800 RBL 32" WALKWAY PANEL DAMAGED(<P>AFT CARGO STA 1800 RBL 32" WALKWAY PANEL P/N : 65B09378-39 DAMAGED AREA REPAIRED IAW RI 53-65-15850 REV A.SDR UIEA2022082200882Pressure Panel · crackedMAIN DECK BS 1241 L/H CLOSE UP PANEL LBL 77-98 BETWEEN TRIM DUCT FOUND CRACKED.(<P>M/D STA 1241 TO STA 1265 LBL 75.92 TO LBL 98.58 PRESSURE PANEL P/N : 144U0031-7 REPLACED AND INSTALLED IAW SRM 51-10-02 AND SRM 51-40-02.</P>)SDR UIEA2022082100878Tension Tie · crackedLH STA 1160 TENSION TIE 2EA HOLES FOUND CRACK AT FWD CHANNEL.(<P>UPPER DECK STA 1160 LH TENSION TIE CHANNEL CRACK AREAS REPAIRED IAW SRM 53-40-30-2R-1 REPAIR 1.</P>)SDR QMLA2022083020060None · noneCRACK FOUND AT L/H FRWARD CANOPY FRAME ATTACHMENT STRUCTURE. CRACK IS IN THE AREA "A" IDENTIFIED IN EC130T2 AMM TASK 53-21-00, 6-1. CRACK IS ROUGHLY 15MM (.59IN). FIELD LOCATION. NOT CURRENTLY EQUIPPED TO PERFOM REQUIRED REPAIR PER SAME AMM TASK 53-10-00,8-19.SDR JJBA20220908005None · noneCF1, UNDER FLOOR, RH BEAM HAT BTW FRAME 22-23 DOUBLER REPAIR BARE METAL. CORROSION LEVEL 2: RH REPAIR DOUBLER REMOVED FROM REPLACEMENT AFTER DOUBLER REMOVAL MANY HOLES ELONGATED FOUND ON RH OMEGA BEAM BTW FR 22-23. RH OMEGA BEAM BTW FR 22-23 REPAIREDSDR JJBA20220901032None · noneIN CF3 RH SHEAR CLIP FOUND CRACKED BTW STR 13-14 AT FR48. IN CF3 RH SHEAR CLIP AT FR48 BTW STR 13-14 REMOVED FOR REPLACEMENT. NEW SHEAR CLIP LOCALLY FABRICATED. SURFACE FINISH DONE ON LOCALLY FABRICATED SHEAR SLIP. IN CF3 RH SHEAR CLIP AT FR48 BTW STR 13-14 RESDR CALA2022083102233None · noneREF AMES NR 147450-0100-0127 DEEP TOOL MARK IN PANEL SUPPORT T-CHORD ABOVE RIGHT WING I/B FL AP I/B END APPROX. STA 1180 "SEEN WITH FLAPS EXTENDED"SDR 2022FA0000483None · noneDURING THE FINAL INSPECTION OF THIS REGULATOR AND OTHERS (S/N P11101156), WHEN SIDE LOAD WAS PLACED ON THE SHUTOFF VALVE, THE VALVE LEAKED. THIS SIDE LOAD PRESSURE IS NOT PART OF THE FUNCTIONAL TEST OF THE VALVE, BUT NOTICED DURING THE INSPECTION. THE MANUALSDR R61A2022092000555Doubler · corrodedWASTE BOX DOUBLER BTWN FR 88-89 AND STRN 28R-27R CORRODED. PEFORMED REPAIR IAW SRM 53-23-60 REPAIR 01.SDR HNAA2022091200263None · noneE932337 - SSI# 53-20-11 GALLEY L/H #1 FLOOR BOARD SUPPORT HAS CORROSION .... REMOVED CORRODED GALLEY LH #1 FLOORBOARD SUPPORT AND INSTALLED SERVICEABLE FLOOR BOARD SUPPORT IAW EMB145 SRM 51-40-02 AND EMB 45 SRM 51-20-03.SDR HNAA2022091200262None · noneE932336 - SSI# 53-20-11 GALLEY CENTER OMEGA BEAM GUSSET HAS CORROSION .... REMOVED CORRODED GALLEY CENTER OMEGA BEAM GUSSET, PREPPED AND INSTALLED SERVICEABLE GUSSET IAW EMB 145 SRM 51-40-02, EMB 145 SRM 51-20-03.SDR HNAA2022082900252None · nonePDIS 639 05-50 2662134 28AUG22 CLT ASSGN
ENG 1 SHUTDOWN UNCOMMANDED IN FLIGHT. 22-26K FT. (NO ROTATION WITH ATTEMPTED RESTART, CREW SAID DURING CLIMB THE VERTICAL POWER FELT WEAKER THAN USUAL BUT ENG1 N2 INDICATION NORMAL) ORIGINAL LOG PAGE 266SDR HALA2022082900252None · noneMAJOR STRUCTURAL REPAIR DUE TO GROUND DAMAGE, DENTS OUT OF LIMITS. SKIN PANEL FRAME 67 BETWEEN STR 51RH AND STR 55RH. MAJOR STRUCTURAL REPAIR ACCOMPLISHED PER A330 SRM 53-41-11-300-017 AND DL ERA 599655-14.SDR YENA2022082900829None · noneFLT#187, BOS-LAX. 'FUMES EVENT 10,000 FEET UNTIL LANDING IN CABIN ONLY- ODOR REPORT FILLED OUT; COMPLIED WITH INFO NOTICE 2017-TO-1SI NO PREVIOUS WRITE UP IN THE LAST 25 FL. PERFORMED PER TSM 05-50-00-810-831. PERFORMED GVI OF APU PER AMM 49-16-00. NO FINDINGSDR R61A2022092700610Support · corrodedLEVEL 2 CORROSION FOUND ON WING TO FUSELAGE FAIRING SUPPORT STRUCTURE FRAME WEB AT FR52. FRAME WEB REPLACED IAW SRM 51-41-01SDR R61A2022092000562Seat Track · corrodedDURING HEAVY CHECK MAINTENANCE FOUND CFIII, LH IB SEAT TRACK BETWEEN FR80 AND 81 HAS CORROSION. CFIII LH IB SEAT TRACK BETWEEN FR80 AND 81 REPAIRED IAW EMB SRM 53-00-10 - REPAIR 02.SDR R61A2022092000561Seat Track · corrodedDURING HEAVY CHECK MAINTENANCE FOUND CENTER FUSELAGE III, RH IB SEAT TRACK HAS CORROSION BETWEEN FR83-84. CFIII RH IB SEAT TRACK BETWEEN FR83-84 REPAIRED IAW ERJ 170 SRM 53-00-10, REPAIR 2.SDR EBVR202305300001Unknown · unknownCORROSION WAS FOUND ON THE LH & RH AFT FUSELAGE SKIN ALONG THE AFT FUSELAGE CLOSEOUT FAIRING ATTACHMENT LINE. REPAIRED PER AQRD ERO 972834. THIS IS A MAJOR/PERMANENT REPAIR.SDR R61A2022092700608Seat Track · corrodedLEVEL 2 CORROSION FOUND ON CENTER FUSELAGE 2 RH IB SEAT TRACK FR43-59. REPLACED RT INBD SEAT TRACK IAW SRM 51-43-05SDR R61A2022092700607Fitting · corrodedLEVEL 2 CORROSION FOUND ON RH MLG UPLOCK FITTING AFT LOWER HOLE. REPLACED MLG UPLOCK FITTING IAW SRM 51-43-04
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