JASC 5100
Service difficulty reports · 4,244
Reports filed under 5100 · Standard Practices/Structures, 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 = '5100' 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 = '5100' 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 2004UALA00480Unknown · unknownDURING CLIMBOUT COULD NOT MAINTAIN NORMAL AIRSPEED AND PITCH ATTITUDE. FLIGHT LEVEL 300-340 MAX EPR 1.45. FLIGHT DATA RECORDER INDICATED AIRCRAFT WAS OPERATING WITHIN THE NORMAL FLIGHT ENVELOPE PARAMETERS.SDR MTNA20043Fire · detectedDURING FLIGHT FDX7145 EZE-POA THE CARGO SMOKE WARNING LIGHT ILLUMINATED. THE THIRD CREW MEMBER OCCUPYING THE JUMP SEAT CHECKED THE CARGO COMPARTMENT AND OBSERVED FLAMES IN THE REAR OF THE AIRCRAFT. THE CREW DECLARED AN EMERGENCY AND THE JUMPSEAT CREW MEMBER SDR QXEA200700367Unknown · unknownPDX FLIGHT NR 2325: AFTER CONTROL WHEEL CHECK, WHEEL TILTED 25 DEGREES TO THE RIGHT. AIRCRAFT RETURNED TO GATE. MAINTENANCE INSPECTED LEFT AND RIGHT AILERONS. NO DEFECTS NOTED. C/W TRAVEL OPS CHECK OF AILERON TRIM. CHECKS GOOD. C/W OPS TEST OF AILERON COSDR LR7A03106Repair · noneDURING SCHEDULED C4 INSPECTION PER JOBCARD HC3213 NOTED LMLG WHEEL WELL BULKHEAD WEB PREVIOUS REPAIR IN WEB AREA OF FS 528 - 577, WL 142 - 150, LBL 62. SCHEDULE REPLACEMENT TO ELIMINATE REPAIR. REPLACED WEB FS 528 - 577 IAW SRM SMP 583 51-60 & 51-70.SDR LR7A03101Repair · noneDURING SCHEDULED C4 INSPECTION PER JOBCARD HC5321 NOTED LT AILERON UPPER SURFACE NON-FLUSH REPAIR AT AS 40-55. REPLACED AILERON UPPER SURFACE SKIN IAW SRM SMP 583 51-60 & 51-70.SDR LR7A03098Repair · noneDURING SCHEDULED C4 INSPECTION PER JOBCARD HC5511 NOTED RT ELEVATOR NON-FLUSH REPAIR AT HSS 164. REPAIRED IAW SRM SMP 583 51-140-10.SDR LR7A03097Floorbeam · scheduled maintDURING SCHEDULED C4 INSPECTION PER JOBCARD HC5321 FOUND RT CENTER FUSELAGE FS 737E-817E CHINE ANGLE WITH NUMEROUS REPAIRS, RBL 61, WL 142. REPLACED CHINE ANGLE FS 737E-817E IAW SRM SMP 583 51-60 & 51-70.SDR ASAA02402EEDoor · chafedDURING C-CHECK, FOUND AFT GALLEY SERVICE DOOR UPPER AFT INNER CORNER CHAFED. REPAIRED IAW SRM. (M)SDR ASAA02402BBSkin · dentedDURING C-CHECK, FOUND LEFT HORIZONTAL STAB LE HAS DENT AT 91 IN OUTBOARD FROM REMOVEABLE LE SKIN INBOARD END. REPAIRED IAW SRM. (M)SDR ASAA02402AASupport · corrodedPAE - DURING C-CHECK, FOUND FLOOR TO SIDEWALL SUPPORT FROM BS 727E PLUS 14, 835 IS CORRODED. REPAIRED IAW SRM. (M)SDR C2XA037TYGusset · gougedDURING A SCHEDULED 3C INSPECTION, A GOUGE WAS FOUND ON THE TOP CAP LOCATED IN THE GALLEY AREA AFT OF THE FWD. DIGITAL. THE AFT GUSSET WAS REMOVED AND REPLACED IAW THE EMB 135/145 SRM 51-70-02. THE ACFT. WAS RELEASED FOR SERVICE FOLLOING THE COMPLETION OF THE SSDR ASAA2004AAAStrap · corrodedPAE - DURING C-CHECK, FOUND CORROSION ON STRAP AT BS 794, RBL 20 AND WL 148. REPAIRED IAW SRM. (M)SDR C2XA037Gusset · gougedDURING A SCHEDULED 3C INSPECTION, A GOUGE WAS DISCOVERED ON THE TOP CAP LOCATED IN THE GALLEY AREA, JUST AFT OF THE FWD. DIGITAL. THE AFT GUSSET WAS REMOVED AND REPLACED IAW THE EMB 135/145 SRM 5170-02. ACFT. WAS RELEASED FOR SERVICE AFTER THE COMPLETION OF THSDR C2XA03TY033Support · corrodedTYS DURING A SCHEDULED 1C INSPECTION THE TOP CAP ANGLE BEAM WAS CORRODED.MAINT.REPLACED RAMP ANGLE BEAM FOR TOP CAP IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE REL. UPON COMPLETION OF ALL WORK.SDR ASAA0340109Beam · corrodedPAE - DURING C-CHECK, FOUND CORROSION ON THRESHOLD BEAM FROM BS 795-846 RBL 21 AND WL 153. REPAIRED IAW SRM. (M)SDR NSVA200300010Skin Panel · wornDetail inspection: Captains partition lug receptacle (in cabin area) elongated and cracked. MX - Removed damaged area and installed doubler repair IAW Field repair FR-CO-00816 REV, dated 02/13/03.SDR C2XA03TY019Beam · corrodedTYS DURING A SCHEDULED 2-C INSPECTION THE FORWARD FLOOR SUPPORT BEAM FOR PANEL 242AF WAS FOUND CORRODED. MAINT. CLEANED AREA,FAB.,ALLODINED AND PRIMED A DOUBLER AND INSTALL IAW EMB 135/145 SRM-51-10-02 AND CMP-51-21-04/05/06.ALL WORK WAS ACCOMPLISHED AND WILLSDR TSAA0251248Window Frame · crackedTRIMMED AREA AND VERIFIED CRACK REMOVED USING HFEC. FABRICATED 3 EACH FILLERS AND A REPAIR DOUBLER FROM 2024-T3 AS SHOWN IN PHOTO 1, MAINTAINING 2D EDGE MARGIN AND 5D-6D SPACING AT NEW FASTENER LOCATIONS. FINISH ALL BARE ALUMINUM WITH ALODINE AND TWO COATS OSDR ASAA0240186Flange · corrodedPAE - DURING SI CHECK, FOUND CORROSION ON UPPER FLANGE AT BS 492, RBL 24 AND WL 156 FWD CARGO DOOR. REPAIRED IAW SRM. (M)SDR C2XA02TY160Channel · corrodedTYS During a scheduled inspection the aft galley floor step-up channel was found to be corroded at frame 23. Maintenance removed and replaced the channel IAW EMB-145 SRM 51-40-02, the repair was satisfactory. The aircraft will be released upon completion oSDR NSVA200200003StringerDiscovered during "A", "B" check. Stringer R 10 is cracked at FS 451SDR NSVA200200002Stringer · crackedNom-routine work card inspection- frame at FS 456 has a crack that runs through a rivit hole to the "cutout" where stringer #10 intersects.SDR C2XA02TY134Doubler · corrodedTYS During a scheduled inspection, corrosion was found on a doubler at the right hand beam hat section at frame 20. Maintenance accomplished a blend-out repair IAW EMB GST #1927/02A and EMB145 CPM 51-21-04,05 and 06. The repair was satisfactory, the aircrafSDR SIMA200222107Sill · corrodedTHIS IS LEVEL TWO FINDING ON CRIC NR 23854. LEFT SILL IN GALLEY AREA HAS CORROSION. C/A: INSTALLED SERVICEABLE SILL IAW SRM.SDR C2XA02TY110Doubler · corrodedTYS During a scheduled inspection corrosion was found on fairing 191 leading edge doublers. Maintenance removed and replaced the leading edge doublers IAW EMB-145 SRM 51-10-02, 51-20-03,04, 05 and 06. The repair was satisfactory, the aircraft will be releaSDR RYN2002F00033Panel · corrodedAT (C) CHECK, FOUND FORWARD PIT TRANSISTION PANEL WITH CORRODED AREAS, STATION 620 TO 720D, RBL 20 TO 26, ON UPPER AND LOWER SURFACES.SDR SIMA200216305Crossbeam · corrodedTHIS IS A LEVEL 2 FINDING ON CRIC NR 36200. GALLEY CROSSBEAM AND PROFILE HAS CORROSION AT FRAME 23. C/A- INSTALLED NEW CROSSBEAM AND PROFILE IAW SRM.SDR RYN2002F00031Web · corrodedAT (C) CHECK, FOUND CABIN SHEAR WEB SEVERAL AREAS OF CORROSION AT STATION 1148 TO 1183, RBL 24 TO 48.SDR RYN2002F00029Fitting · corrodedAT (C) CHECK, FOUND NOSE WHEEL WELL FORWARD BULKHEAD DOOR LINKAGE FITTING CORRODED, AT STATION 227.8, LEFT SIDE.SDR SIMA200215105Stringer · chafedDURING AN IMBV INSPECTION, FOUND STRINGER 19R, CHAFED. BLENDED CHAFE. PERFORMED AN NDT INSPECTION NO DEFECTS. TWO DOUBLERS AND FOUR SHIMS. REPAIR DONE IAW STANDARD SRM PRACTICES.SDR SIMA200215104Stringer · damagedDURING AN IMBV INSPECTION, ONE RIVET HOLES WAS MISDRILLED ON STRINGER 19L, AT FRAME 52. REAMED HOLE, INSTALLED A HST10BJ-8-6, AND HST79CK-8 FASTERNS. REPAIR DONE IAW STANDARD SRM PRACTICES.SDR ABXA010772Angle · crackedOUTBOARD LOWER FASTENER HOLE ON ATTACH ANGLE CRACKED WHERE WING TO FUSELAGE FAIRING ATTACHES AT F.S. 585. REPLACED ANGLE IAW DC-9 SRM 51-30-1 AND DC-9 DWG 9915547.SDR ABXA010569Doubler · crackedSKIN DOUBLER WAS CRACKED AND EXFOLIATED IN TWO PLACES, FORWARD SIDE OF F.S. 617 AND LONGERON 30, AND FUSELAGE DRAIN AT F.S. 632. REPLACED KIDNEY DOUBLER.SDR COMA0160700DoorFLIGHT #5512. DURING CRUISE FLIGHT EXPERIENCED INTERMITTENT LOW FREQUENCY VIBRATION FROM COCKPIT FLOOR, AIRCRAFT RETURNED TO ORIGINATION CITY CVG AND LANDED SAFELY.PERFORMED STATIC GEAR SWING, INSPECTED GEAR DOORS AND PERFORMED FLIGHT CHECK, DISCREPANCY COULDSDR COMA0160681Vane · wornL/H AND R/H INBD FLAP VANES CHAFFED ON INBD LEADING EDGES.REMOVED AND REPLACED L/H AND R/H INBD INBD FLAP VANE, INBD LEADING EDGES I/A/W AERODESIGN REPORT #1266-1 REV IR DATED 9/27/94.SDR UPS01236810Skin · corrodedINSPECTION TYPE:C ON REMOVAL OF FWD FUSELAGE HINGE FROM MAIN CARGO DOOR, CORROSION FOU ND ON FUSELAGE SKIN REPAIRED IAW SMRO EO 2001-039-004SDR RYN2002F00004Stringer · corrodedSTRINGER EXFOLIATED BETWEEN BS 1148 TO BS 1166 BETWEEN STRINGER 3L AND 4L IN THE AFT CABIN CROWN AREA. ACCOMPLISHED FUSELAGE STRINGER REPAIR BS 1148 TO 1166 BETWEEN STRINGER 3L AND 4L. DUE TO CORROSION IAW SRM. (MATERIAL USED 301 CRESS .5000 HARD .050 INCH,SDR UPS01236685Intercostal · crackedINSPECTION TYPE:C INTERCOSTAL CRACKED ABOVE DRAG BRACE FITTING SUPPORT INTERCOSTAL REPLACED IAW DRWG 65-18417SDR AALA20011621Intercostal · crackedTUL - FOUND INTERCOSTAL STATION 1291 BL0 CRACKED. REPLACED INTERCOSTAL PER SRM 51-01. (M)SDR RYN2002F00003Skin · corrodedBULGING SKIN/DISHED FASTENER AT BS 1176 THRU BS 1183, STRINGER 20L THRU 21L UNDER AFT LAV SERVICE VALVE. ACCOMPLISHED FUSELAGE SKIN REPAIR FROM BS 1176 TO BS 1183 STRINGER 20L TO STRINGER 21L DUE TO CORROSION. (MATERIAL USED 2024-T3. 071, 28 INCHES X 30 INSDR RYN2002F00002Skin · damagedBULGING AND PILLOWING SKIN AT BS 1085 THRU BS 1110 ALONG FASTENER ROWS AT STRINGER 17R THRU 19R ON EXTERNAL FUSELAGE. ACCOMPLISHED FUSELAGE SKIN REPAIR FROM BS 1085 TO BS 1110 BETWEEN STRINGER 17R AND 19R DUE TO CORROSION IAW MFG ENGINEERING RO. (MATERIAL USSDR RYN2002F00001Skin · damagedBULGING/PILLOWING SKIN ALONG STRINGER 4L AT LAP JOINT BS 1130 THRU BS 1183. ACCOMPLISHED FUSELAGE SKIN REPAIR FROM BS 1130 TO BS 1183 STRINGER 4L DUE TO CORROSION IAW SRM. (MATERIAL USED 2024-T3 .050 INCH, 98 INCHES X 9.1250 INCHES)SDR AALA20011579Web · crackedTUL - FOUND LEFT PRESSURE WALL IS CRACKED JUST BELOW DOOR CABLE QUAD. INSTALLED DOUBLER PER ESO 11697 7/30/01. (M)SDR AALA20011606Stiffener · corrodedTUL - FOUND STIFFENER CORRODED ON 870 BULKHEAD 1ST STIFFENER OUTBOARD OF KEEL BEAM, ON OUTBOARD SIDE APPROX MIDDLE OF STIFFENER. DAMAGE, REMOVED HFEC INDICATED NO CRACK AROUND ELONGATED BLENDED HOLE, DOUBLER INSTALLED PER ESO11697 DATED 7-24-01. (M)SDR AALA20011518SparTUL - FOUND INTERIM REPAIR ACCOMPLISHED ON RIB AFT FLANGE FRONT SPAR BETWEEN SLAT TRACKS NR 5 AND NR 6 RIGHT WING. REPLCED REAR HALF WITH NEW, FRONT SPAR, BETWEEN SLAT TRACKS 5 AND 6, SRM 51-01. (M)SDR SIMA200120013Support · corrodedSBP - FOUND LEFT FORWARD FLOOR SUPPORT AT STATION BL 34 IS CORRODED ON THE LOWER PORTION. REMOVED AND REPLACED FLOOR SUPPORT IAW SAAB SRM 51-40-21. (M)SDR SIMA200120009Floor Support · corrodedSBP - RIGHT FLOOR SUPPORT ANGLE AT BL 34 IS CORRODED AT FORWARD END. REMOVED AND REPLACED FLOOR SUPPORT IAW SAAB SRM 51-40-21. (M)SDR SIMA200120008Track · corrodedSBP - FOUND SEAT TRACK AT BL 36 RIGHT IS CORRODED AT LEG ATTACH POINTS. REMOVED AND REPLACED TRACK ASSEMBLY IAW SAAB SRM 51-20-43, AND 51-70-40. (M)SDR SIMA200120007Web · corrodedSBP - WEB REINFORCEMENT IS CORRODED AT STATION 294. REMOVED AND REPLACED WEB REINFORCEMENT IAW SAAB SRM 51-40-21. (M)SDR SIMA200120006Angle · corrodedSBP - LEFT ANGLE CORRODED FROM STATION 272 AND 288. REMOVED AND REPLACED ANGLE IAW SAAB SRM 51-40-21. (M)
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