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 HEER20190710093Skin · corrodedFORWARD SHELL ASSEMBLY OUTER SKIN WAS FOUND TO BE CORRODED -LOCAL TO AN EXISTING INSERT LOCATION. THE REPAIR DOCUMENTATION WILL BE SUBMITTED FOR FAA APPROVAL. THE FORWARD SHELL ASSEMBLY WILL THEN BE REPAIRED IN ACCORDANCE WITH THE FAA-APPROVED REPAIR DATA.SDR COEA2019070801816Floorbeam · crackedL/H LONGITUDINAL FLOORBEAM CRACKED AFT OF FRAME 17. REPAIRED IAWE.O. 5315-02.SDR ALGA201908090002Panel · corrodedDURING 10YR INSP LOWER PANEL ASSY WAS FOUND TO HAVE CORROSION DAMAGE TO FOUR (4) AREAS. OEM REPAIR: RS139-5336-0241 ISSUE A.SDR ASOA201906277061Skin · crackedL/H UPPER FUSELAGE SKIN CRACKED AT FRAME 75 STRINGER 2L - 3L. CUTOUT DAMAGED SKIN, FABRICATED FILLER, DOUBLER AND DRAG ANGLE AND INSTALLED.SDR HKGA201906260028Plate · crackedPLATE CRACKED. REMOVED DOOR STOP PLATE, MATCH DRILLED NEW PART AND INSTALLED IAW SRM 51-40-02, AND 51-25-00 REV 58.SDR ALGA201908090004Deck Plate · corrodedDURING 1200HR INSPUPPER DECK ASSY WAS FOUND TO BE CORRODED & DE-BONDEDSDR IPXA201906213559Indicator · crackedACCESS PANEL 811AR INDICATOR ASSEMBLY CRACKED. REMOVED & REPLACED INDICATOR ASSEMBLY IAW A300-600 SRM 51-40-21.SDR UIEA2019060704419Bracket · corrodedCORROSION - CLIP, 147AL PNL INTERIOR.(<P>REMOVED DAMAGED PART I.A.W. SRM 51-40-02 REV.105. INSTALLED NEW PART I.A.W. SRM 51-40-02 REV. 105 AND DWG NO. 146U8023 SH3 REV. A. JOB COMPLETED AND CONDITION CHECK SATISFIED. </P>)SDR YV3R2019012200115Panel · crackedCUSTOMER REPORTED PANEL ASSEMBLY WAS FOUND CRACKED.SDR CA190529010Bolt · defective(CAN) A REPLACEMENT ATTACH BOLT FOR THE FLIGHT CONTROL RODS WAS PURCHASED & RECEIVED BY NWA STORES. UPON PRE-INSTALLATION INSPECTION OF THE BOLT, (P/N NAS464P5-25) AN OPEN DEFECT WAS NOTED ON THE TOP CENTER OF THE HEAD AS WELL AS A DARK LINE IN THE SHANK JUST SDR CALA2019042900664Panel · missingPDA 1 PANEL 194FR FOUND MISSING JUST BEFOR DEPARTURE. PLACED PANEL ON CDL, CDL CARD 524810 COMPLIED WITH.SDR C77A2020022500015Seat Track · corrodedDURING BASIC CHECK AT EAMS, CORROSION WAS FOUND ON THE FOLLOWING FORWARD WET AREA RH FLOOR SILL P/N 170-05661-003 BETWEEN FRAME 17 AND FRAME 18. REFERENCE ETD2019-170-055130, FIGURE 1, FOR THE DAMAGE LOCATIONS AND DIMENSIONS. EAMS REQUESTED AND RECEIVED PERMANSDR A6WA201904296590Structure · puncturedPUNCTURE 1.25" LONG AT FS 625.30 STR 18RSDR UIEA2019042604026Seat Track · crackedM/D - STA 1720 LBL 11 .33" SEAT TRACK FOUND CRACK.(<P>CABIN-STA 1670.45 TO STA 1776.45 LBL 11.33" SEAT TRACK REPAIRED IAW RL-53-65-13525 REV.A AND SRM 53-00-52-2R-12 REPAIR 12.<BR /></P>)SDR CA190417003Latch · loose(CAN) AIRFRAME VIBRATION FELT IN CABIN AND FLT DECK DURING CLIMB FL250 TO FL350 . NEW HOOK LATCH INSTALLED I.A.W SRM 51-40-00. (TC# 20190417003)SDR JJBA201904171010Panel · corrodedFR 65 PANEL Z HAS 7 EA AREAS OF CORROSION. REPAIRED FR 65 PANEL Z CORROSION BY BLEND OUT, FABRICATION INSTALLATION NEW DOUBLER ON PANEL Z FR 65.SDR UIEA2019021863233Unknown · vibrationSUBSTANTIAL AIRFRAME VIBRATION WHEN ENGINES SPOOL UP FROM IDLE IN FLIGHT. NO VIBRATION INDICATION ON ENGINE PAGE.(<P>PERFORMED AIRFRAME VIBRATION CONDITIONAL INSPECTION I.A.W A.M.M 05-51-38. NO ABNORMALITIES OR DEFECTS NOTED<BR /></P>)SDR SWAA2022030331195Track · corrodedLBL 3 FLOOR TRACK HAS DEEP PITTING CORROSION ON NUT PLATE HOLES FROM STA 947 TO STA 887 / REMOVED AND REPLACED FLOOR TRACK PER SRM 51-40-02 REF SA-M 326 - A1133984SDR AALA201903139013Cleat · crackedFORWARD CARGO CLEAT WAS CRACKED AT FRAME 35.5, STRINGER 30L. REPLACED THE CLEAT IAW SRM 51-72-11, AND 51-42-11.SDR R61A2019021310174Beam · corroded***WHILE A/C WAS OUT OF SERVICE FOR HEAVY CHECK*** EXTERNAL CF I, FWD CARGO DOOR LOWER SILL BEAM FOUND CORRODED UNDER FWD FITTING. EXTERNAL CF I, FWD CARGO DOOR LOWER SILL BEAM REPLACED IAW E-170 SRM 51-43-04. A/C REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETSDR AALA201901049003Unknown · vibrationDURING DECENT FROM 14000 FT TO 10000 FT, WITH SPEED BRAKE DEPLOYED AT 1/4 TO 1/2 WAY, THE AIRCRAFT VIBRATED MODRATLY AND MORE THAN NORMAL, 260 KNOTS AND DECENDING. THE AIRCRAFT WAS GROUNDED. MAINTENANCE ACCOMPLISHED TSM 27-30-00-810 AND GVI OF ALL SPOILERSDR CALA2018122872667Repair · not reportedAD RELATED 2016-18-09 UPON REMOVAL OF FR34 BELLY FAIRING BETWEEN STR43L-43R REPAIR DOUBLER WAS FOUND. DOUBLER REQ''S PREVIOUS REP AIR INFO AT HAECO LCQ PER REF NO.9294479 BY MECH V913402 REMOVED AND REPLACED SKIN DOUBLER AT FR34,STR43L TO STR43R IAW S RM 53-00SDR DALA2018122607389Doubler · noneERA472703-14 REV ORIG FUSELAGE/DOUBLER-FWD TOILET SERVICE DOOR J AMB DOUBLER P/N 5953050-85/FS=288, LONG 20-21L/BLEND OUT REPAIR TIME-LIMITED. THIS LOGPAGE IS SUPERSEDED BY LOGPAGE 0873134. THE REPAIR INSTALLED PER ER/A 472703-14 HAS BEEN REMOVED, AND IS INCORSDR DALA2023052604208None · noneSHIP 680 ERA 571509-14 REVISION A REQUIRES THE FOLLOW-ON SECTION II ONE TIME INPECTION AT THE NEXT C-CHECK. CORRECTIVE ACTION: REF ERA 571509-14. (0868168)SDR R61A201812121200Shear Panel · corrodedCORROSION-AFT WET AREA L HAND SHEAR PANEL BETWEEN FR87 AND FR88 HAS SURFACE CORROSION AS MARKED.SDR FDEA201812103485Panel · unknownREMOVED R/H EMERGENCY LIGHT PANEL PN 4224012-502. FROM OVER R1 DOOR. SEE WRI 52 10 2014. REF AMM 25-23-23-5 PANEL PLACED IN CREW CLOSET. MEL 10DEC18 05:29 LAX U RELEASED FOR SERVICE PER MEL : 33-50-04 CATEGORY : C EXPIRATION : 20DEC18 "MEL 33-50-04: SDR DALA2018121057123Structure · crackedHFEC INSPECTION FOUND 01EA CRACK ON THE RH HORIZONTAL INNER CHORD AS MARK C/W ER/A 565538-14. (LP 0852480)SDR GTIA2018120652995Unknown · vibrationEXTREAMLY STRONG VIBRATION INFLIGHT FELT THROUGH WHOLE AIRCRAFT AT FL 190-230-PERFORMED OPS TEST OF ELEVATOR DAMPING IAW AMM 27-9600-710-008-A TEST OK PERFORMED VISUAL INSPECTION OF FUSELAGE IAW AMM 05-21-00,05-22-00,05-23-00 NO DEFECTS NOTED.SDR A6WA2018112146170Floor Support · corrodedFLOOR BEAM AT RBL 9 FROM FS 559+66 TO 559+80 CORRODED. REPLACED REPLACED FLOOR BEAM AT RBL 9 FROM FS 559 TO 569 IAW CRJ 200 SRM'S 51-42-06, 51-41-21, 51-42-22 AND 53-61-43SDR UIEA2018110902544Structure · crackedONE CRACK FOUND AT THE FASTENER HOLE. REPAIRED IAW EI T2018A53M-6110, AND SRM 51-40-02, REV 41.SDR AALA201812049016Hinge Fitting · excess playEXCESSIVE PLAY ON THE HINGE FITTING BEARING. REPLACED THE HINGE FITTING IAW SRM 51-72-11 AND AMM 55-36-41-400-001-A.SDR VNAA2018110699901Pulley · separatedPAX DOOR RETRACT PULLEY SEPERATING FROM DOOR FRAME. CA REPAIRED IAW BOMBARDIER REOSDR CALA2018110502282Structure · corrodedAAR NR 9878413 - FORWARD AND REPLACED CORRODED INNER CHORD AND F WD WET AREA BETWEEH STA 294 AND STA 328, RBL 53 PER REF B737 SRM 51-40-02 REMOVED AND REPLACED CORRODED INNER CHORD AND FWD WET AREA BETWE EN STA 294 AND STA 328 RBL 53 PER REF B737 SRM 51-40-02SDR Q2SA2019222700118Shear Web · corrodedCORROSION FOUND ON SHEAR WEB JUST INBD AND AFT OF R2 DOOR AT BS 986.5 TO 1016.SDR SWIA2018110545237Panel · corrodedSTRAP LOCATED ON PANEL 196DR IS CORRODED. (C-CHECK) RO: 11/1/2018. REPLACED STRAP ON PANEL 196DR REF SRM 51-42-13-001-001-A01. COMPLIED WITH 51-900-1002-SKY (CL600-2C10) STRUCTURAL MAJOR REPAIR (**RII**).SDR SWIA2018110545236Panel · corrodedFWD UNDERWING FAIRING PANEL 193AB HAS CORROSION. (C-CHECK) RO: 11/1/2018. REMOVED AND INSTALLED (2) NEW STRAPS REF SRM 51-42-06-001-001-A01.SDR SWIA2018110245223Structure · dentedLEFT SIDE OF FUSELAGE, BS 515 WAS DENTED. REPAIRED .SDR FOTR20180829022Skin · gougedGOUGE ON INTERNAL DOUBLER AT B.S. 298, UNDER STR .20RSDR DALA2018082805343Not Reported · damagedDURING INSPECTION FOUND OUT OF LIMITS DURING REWORK ON CORRODED AEAS FROM NRC 00523. STA 360 TO 500I CRACK WAS FOUND IN STATION 500A +5. OUT OF LIMIT AREAS ON STA 360 TO 500I AND CRACK IN STA 500 A+5 WERE REPLACED. PER B737-800 SRM 53-00-53 REPAIR 6.SDR AALA201808285001Unknown · vibrationDURING CLIMB AT 37000 FT, HEARD AND FELT LOW RUMBLING IN THE AIRFRAME. POSSIBLELY A LT ENGINE COMPRESSOR STALL. LEFT ENGINE EXHAUST GAS TEMPERATURE ROSE. AMBER LIGHT ON ENGINE GAS TERMPERATURE INDICATOR. ODOR OF ACRID FUMES NOTICED IN THE COCKPIT AND A RESDR ASOA201808105174Tripler · chafedTRIPLER AT BS 985, BL 0 WAS CHAFED. REPAIRED TRIPLER IAW REO 670-53-00-552 REV -, AND EC/TC REO 670-53-00-552.SDR FDEA2018121891977Seat Track · corrodedMAIN DECK COMPARTMENT FRAME 41-44, SEAT TRACK Y0 HAS CORROSION AS MAKED 7 PLACES. SEAT TRACK FOUND TO BE CORRODED OUT OF LIMITS IAW SRM 53-10-16 FIG 103. TRACK REMOVED AND REPLACED IAW SRM 51-40-21 FR41-44 MAJOR REPAIRSDR SWIA2018081745005Not Reported · damagedTWO OVERSIZED HOLES IN LHS AIRCRAFT STRUCTURE FOUND. REPAIRED IAW REO.SDR SIMA201806132003Unknown · unknownAFTER TAKEOFF, A LOUD BANGING SOUND WAS HEARD AND FELT ON THE LEFT FORWARD SIDE OF THE NOSE. DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. NORMAL LANDING. INSPECTED IAW 51-10-02, NO AREAS OF DAMAGE FOUND, THE DOOR OPERATED NORMAL.SDR N6WA20180608702Not Reported · crackedA CRACK WAS FOUND AT BS 280. BL 0. R & R THE INTERCOSTAL & BS 280 FLOORBEAM IAW SRM 53-11-41, ANDSRM 51-42-06SDR N6WA20180608701Not Reported · crackedCRACK FOUND AT BS 280, BL 0. R & R THE INBD & OTBD INTERCOSTALS & THE FLOORBEAM IAW SRM 53-11-41, AND SRM 51-42-06SDR UIEA2018060701057Not Reported · corrodedCORROSION LOCATIONS FOUND DURING SB 747-53A-878. REPAIR THE DAMAGE AREA IAW EI T2018 AS3M-2232 REV.3SDR V0XD20180608002Structure · crackedFWD EQUIPMENT COMPARTMENT LOWER STUCTURE CRACKED JUST OTBD OF ADG STOWING MANIFOLD. REPAIRED IAW REO 670-53-11-509, REV D, AND REO 670-53-11-1397, REV-.SDR R61A201806040646Profile · corrodedCORROSION WAS FOUND ON THREE PROFILES ON PANEL 1441FR. REMOVED AND REPLACED THE PROFILES.SDR R61A201806040645Profile · corrodedCORROSION WAS FOUND ON THREE PROFILES ON PANEL 1431DL. REMOVED AND REPLACED THE PROFILES.
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