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 08FDEA02507None · noneFOUND A REPAIR LOCATED AT STA 1517-1527; STRINGER 46R THAT REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS INSTALLED USING FAA APPROVED DATA. EVALUATED REPAIR AND FOUND NO APPROVED FAA DATA. REPAIRED IAW FEDEX EA 8-5310-118524 "FUSELAGE SDR UPS08152573None · noneCRACK MAIN CARGO PIT DOOR. EVALUATED DAMAGE TO BE WITHIN LIMITS OF A300 SRM CH 53-10-20 FIG 104. C/W TEMPORARY AND OPEN DEFERRAL FOR PERMANENT REPAIR WITHIN 350 FLIGHT HRS.SDR QXEA200800667None · noneGEG - FLIGHT 2378 - ODOR PRESENT IN FWD CABIN DURING DESCENT. SMELLED LIKE SOLVENT. MAINTENANCE FOUND IT TO BE FROM THE GARBAGE CAN. REMOVED TRASH AND WASHED TRASH CAN. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. NOT AN SDRSDR VNAA0806011None · noneCREW REPORTED A BIRD STRIKE TO THE RT WINDSHIELD. MAINTENANCE INSPECTED AND FOUND NO DEFECTS. ACFT WAS RELEASED FOR SERVICE. (S)SDR 08FDEA02346None · noneACCOMPLISHED BOEING SB 757-54-0035, R2, PARA. 3, PART 3, STRUCTURE CHANGES FOR THE NR 2 STRUT, EXCEPT STEO Q, PANEL 5, PER FEDEX EA F-5450-108907, DATED 11 OCT 2007. COMPLIED WITH FEDEX EA F-5450-108907A, DATED 28 MAY 2008 ON W/C T F-5450-108907A, WRI 5450017SDR 08FDEA02345None · noneACCOMPLISH SB 757-54-0035, R2, PARA 3, PART 2; WING STRUCTURE CHANGES FOR THE NR 2 STRUT AND RT WING PER EA F-5450-108907, DATED 11 OCT 2007. ACCOMPLISHED SB 757-54-0035, PART 2, ON NR 2 STRUT, AS PER EA F-5450-108907A, DATED 28 MAY 2008. PER EA, SCHEDULE EOSDR UPS08853000None · noneINSPECTION TYPE-C2, COMPLY WITH MPI 19584 REGARDING REPLACEMENT OF EXISTING REPAIR AT AT L28R IAW WAN3 1369154 AND EO DC8-5330-20248-E APPX.E FABBED AND INSTALLED REPAIR DOUBLER IAW, EA NR 008-5330-01-A1449, SRO 853 0032. NOT AN SDR.SDR VNAA0806010None · noneCREW REPORTED A BIRD STRIKE TO THE CAPTAIN`S WINDSHIELD. MAINTENANCE INSPECTED AND FOUND NO DEFECTS. ACFT WAS RELEASED FOR SERVICE. (S)SDR ZZDA2008123None · noneEMERGENCY LIGHT SYSTEM INOPERATIVE. FOUND ON F/A PANEL SWITCH IN ON POSITION. RESET SWITCH, SYSTEM OPS NORMAL AS REQUIRED.SDR TRAX200800756None · noneCORROSION AT SUBFRAMES BETWEEN S26L/R AND S27 JUST FWD OF FS 364.00 AT AFT CORNER. UPON FURTHER INSPECTION NO CORROSION FOUND AT FS 346.00 S26L-26R. (B)SDR 08FDEA02167None · noneREJECTED TAKEOFF FOR WINDSHEAR AURAL ALERT 80 KTS,34 DEG C ,386K FACT 05 JUN08 21:47 AFW U CHECKED PER AMM 05-56-00 AND 05-57-00, ACFT OK FOR SERVICE CHECKED PER AMM 05-56-00 AND 05-57-00, ACFT OK FOR SERVICE.SDR 08FDEA02166None · noneREJECTED TAKEOFF AT IND AT 100 KTS OAT 31C WEIGHT 386,200. REJECTED FOR PREDICITIVE WINDSHEAR ALERT. NO OBSERVED OR REPORTED WINDSHEAR. PERFORMED BRAKE INSPECTION PER AMM 32-57-00-6. NO DEFECTS NOTED. ACN RELEASED FOR SERVICE PER MEL/CDL: 34-41-01-01-A CASDR 08FDEA02126None · noneCENTER CARGO, STA 1791 LEFT LONGERON 37 FOUND WITH EXISTING SPLICE REPAIR. CENTER CARGO STA 1791 LEFT LONGERON 37 FOUND WITH EXISTING SPLICE REPAIR EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED AS PER SRM 53-10-00 FIGURE 2 VOLUME I FEDEX EO NR 1-5100-7-5001 A3 SDR 08FDEA02125None · noneLOWER AFT FUSELAGE BELLY AT STA 1711 TO STA 1751 FOUND WITH EXISTING REPAIR. EXISTING SKIN SPLICE REPAIR AT LOWER AFT FUSELAGE BELLY STA 1711 TO STA 1751 EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED AS PER SRM 53-20-00 FIGURE 10 VOLUME I FEDEX EO NR 1-5100-7-5SDR 08FDEA02124None · noneMAIN DECK, EXISTING TRANSVERSE FRAME REPAIR AT STA 1681 LONGERON 12L. EXISTING TRANSVERSE FRAME REPAIR AT STA 1681 LONGERON 12L EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED AS PER SRM 53-30-00 FIGURE 1 VOLUME I. FEDEX EO NR 1-5100-7-5001 A3 PART 1, TITLE: REPSDR 08FDEA02123None · noneMAIN DECK, EXISTING TRANSVERSE FRAME REPAIR AT STA 1641 LONGERON 12L. EXISTING REPAIR AT MAIN DECK TRANSVERSE FRAME STA 1641 LONGERON 12L EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED AS PER SRM 53-30-00 FIGURE 1 VOLUME I. FEDEX EO NR 1-5100-7-5001 A3 PART 1, SDR 08FDEA02122None · noneEXISTING REPAIR, MAIN DECK EXISTING TRANSVERSE FRAME REPAIR FOUND AT STA 1761 LONGERON 12L. EXISTING REPAIR AT MAIN DECK EXISTING TRANSVERSE FRAME STA 1761 LONGERON 12L EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED AS PER SRM 53-30-00 FIGURE 1 VOLUME I FEDEX EOSDR 08FDEA02113None · noneLEFT WING LEADING EDGE NR 3 SLAT UNDER SURFACE INBOARD FOUND EXISTING REPAIR. LEFT WING LEADING EDGE NR 3 SLAT UNDER SURFACE INBOARD EXISTING REPAIR EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED AS PER SRM 57-10-00 FIGURE 10 VOLUME I FEDEX EO NR 1-5100-7-5001SDR 08FDEA02112None · noneLEFT WING LEADING EDGE AT APPROX STA XOS 484 TO XOS 549 FOUND EXISTING REPAIR. LEFT WING LEADING EDGE AT APPROX STA XOS 484 TO XOS 549 EXISTING REPAIR EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED AS PER SRM 57-10-00 FIGURE 7 VOLUME I FEDEX EO NR 1- 5100-7-50SDR 08FDEA02111None · noneLEFT WING LEADING EDGE AT APPROX STA XIS 247 FOUND EXISTING REPAIR. LEFT WING LEADING EDGE AT APPROX STA XIS 247 EXISTING REPAIR EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED AS PER SRM 57-10-00 FIGURE 24 VOLUME I. FEDEX EO NR1-5100-7-5001 A3 PART 1, TITLE: RSDR 08FDEA02110None · noneEXISTING REPAIR, MAIN DECK EXISTING SEAT TRACK SPLICE REPAIR FOUND AT STA 1235, X = - 47.5. EXISTING REPAIR AT MAIN DECK SEAT TRACK SPLICE REPAIR AT STA 1235, X = -47.5 EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED AS PER SRM 53-70-00 FIGURE 1 VOLUME I FEDEX EOSDR 08FDEA02109None · noneEXISTING REPAIR, MAIN DECK EXISTING SEAT TRACK SPLICE REPAIR FOUND AT STA 1235, X = - 27.5. EXISTING REPAIR AT MAIN DECK SEAT TRACK SPLICE REPAIR AT STA 1235, X = -27.5 EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED AS PER SRM 53-70-00 FIGURE 1 VOLUME I. FEDEX ESDR 08FDEA02108None · noneEXISTING REPAIR, RIGHT WING INBOARD FLAP UPPER SURFACE AT XIFH 186 FOUND REPAIR DOUBLER. EXISTING REPAIR AT RIGHT WING INBOARD FLAP UPPER SURFACE AT XIFH 186 EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED AS PER SRM 57-10-00 FIGURE 38 VOLUME I. FEDEX EO NR 1-510SDR 08FDEA02107None · noneEXISTING REPAIR, RIGHT WING INBOARD FLAP UPPER SURFACE AT XIFH 225 FOUND REPAIR DOUBLER. EXISTING REPAIR AT RIGHT WING INBOARD FLAP UPPER SURFACE AT XIFH 225 EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED AS PER SRM 57-10-00 FIGURE 38 VOLUME I. FEDEX EO NR 1-510SDR 08FDEA02106None · noneEXISTING REPAIR, RIGHT WING FIXED LEADING EDGE UPPER SURFACE BETWEEN NR 1 AND NR 2 LEADING EDGE SLATS FOUND REPAIR DOUBLER. EXISTING REPAIR AT RIGHT WING FIXED LEADING EDGE UPPER SURFACE BETWEEN NR 1 AND NR 2 LEADING EDGE SLATS EVALUATED AND FOUND PREVIOUSLY SDR 08FDEA02105None · noneEXISTING REPAIR, RIGHT WING NR 3 LEADING EDGE SLAT LOWER SURFACE FOUND REPAIR DOUBLER. EXISTING REPAIR AT RIGHT WING NR 3 LEADING EDGE SLAT LOWER SURFACE EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED AS PER SRM 57-10-00 FIGURE 10 VOLUME I FEDEX EO NR 1-5100-7-5SDR 08FDEA02104None · noneEXISTING REPAIR, RIGHT WING NR 3 LEADING EDGE SLAT UPPER SURFACE LEADING EDGE FOUND REPAIR DOUBLER. EXISTING REPAIR AT RIGHT WING NR 3 LEADING EDGE SLAT UPPER SURFACE LEADING EDGE EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED AS PER SRM 57-10-00 FIGURE 5 VOLUMESDR 08FDEA02103None · noneEXISTING DOUBLER REPAIR AT LEFT FUSELAGE APPROX STA 999 TO STA 979, STRINGER 41 TO 43. EXISTING DOUBLER REPAIR AT LEFT FUSELAGE APPROX STA 999 TO STA 979, STRINGER 41 TO 43 EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED AS PER SRM 53-50-00 FIGURE 17 VOLUME I. SDR 08FDEA02102None · noneEXISTING DOUBLER REPAIR AT CENTER CARGO FORWARD CUT-OUT APPROX STRINGER 40 TO 42. EXISTING DOUBLER REPAIR AT CENTER CARGO FORWARD CUT-OUT APPROX STRINGER 40 TO 42 EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED AS PER SRM 53-50-00 FIGURE 17 VOLUME I FEDEX EO NR 1SDR 08FDEA02101None · noneEXISTING DOUBLER REPAIR AT CENTER CARGO DOOR FORWARD CUT-OUT APPROX STRINGER 37 TO 40. EXISTING DOUBLER REPAIR AT CENTER CARGO DOOR FORWARD CUT-OUT APPROX STRINGER 37 TO 40. EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED AS PER SRM 53-50-00 FIGURE 17, VOLUME I.SDR 08FDEA02100None · noneEXISTING DOUBLER REPAIR AT CENTER CARGO DOOR AFT CUT-OUT APPROX STRINGER 38 TO 42. EXISTING DOUBLER REPAIR AT CENTER CARGO DOOR AFT CUT-OUT APPROX STRINGER 38 TO 42 EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED AS PER SRM 53-50-00 FIGURE 17 VOLUME I FEDEX EO NRSDR 08FDEA02099None · noneEXISTING DOUBLER REPAIR AT FORWARD CARGO DOOR FORWARD CUT-OUT APPROX STRINGER 38 TO 42. EXISTING DOUBLER REPAIR AT FORWARD CARGO DOOR FORWARD CUT-OUT APPROX. STRINGER 38 TO 42 EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED AS PER SRM 53-50-00 FIGURE 17 VOLUME ISDR 08FDEA02098None · noneEXISTING DOUBLER REPAIR AT RIGHT FUSELAGE APPROX STA 1019 TO STA 1039, STRINGER 40 TO 43. EXISTING DOUBLER REPAIR AT RIGHT FUSELAGE APPROX STA 1019 TO STA 1039, STRINGER 40 TO 43 EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED AS PER SRM 53-20-00 FIGURE 10 VOLUMESDR 08FDEA02097None · noneEXISTING DOUBLER REPAIR AT RIGHT FUSELAGE APPROX STA 2003 TO STA 2004, STRINGER 38 TO 41. EXISTING DOUBLER REPAIR AT RIGHT FUSELAGE APPROX STA 2003 TO STA 2004, STRINGER 38 TO 41 EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED PER SRM 53-20-00 FIGURE 2 VOLUME ISDR 08FDEA02050None · noneUNRECORDED PREVIOUS REPAIR FOUND ON RT APU COWLING LOCATED AT MIDDLE HINGE. REPAIR TO BE EVALUATED. EXISTING REPAIR FOUND TO BE IAW B757-200 SRM 52-40-01 FIG 201, REPAIR 5, BASED ON EXTERNAL VISUAL EVALUATION ON THE SHAPE, LOCATION, SIZE, MATERIAL THICKNESS,SDR 08FDEA02037None · noneFOUND OLD DOUBLER REPAIR ON FUSELAGE C 73, P45-46 RT DOUBLER REPAIR RENEWED IAW SRM 53-10-12 FIG 228.SDR C2XA08RI079None · noneFLIGHT 1245 - EWR - FLIGHT CREW REPORTED SPS FAIL DURING PRE-FLIGHT TEST AND SMELLED SMOKE AFTER TEST. EWR MX PERFORMED OPERATIONAL CHECK OF SPS SYSTEM AND NO ABNORMALITIES WERE FOUND. FURTHER TROUBLESHOOTING FOUND EXTERNAL AIR CONDITIONING CART BAD. MX THESDR 08FDEA02019None · nonePATCH REPAIR ON OUTBOARD LEADING EDGE OF LH WING OUTBOARD FLAP TO BE EVALUATED. EXISTING REPAIR EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED IAW SRM 57-53-01 FIG.202. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA. NOT AN SDRSDR CA080528007Shroud · chafed(CAN) OPERATOR REPORTED A MAIN ROTOR TRANSMISSION OIL LINE FAILURE. INSP REVEALED CHAFING DAMAGE TO THE OIL-LINE SHROUD ASSY FROM THE FIREWALL CLOSEOUT METAL EDGE.SDR 08FDEA01966None · noneEXTERNAL PATCH REPAIR ON AFT CARGO DOOR LOWER CENTER EDGE BEAM TO BE EVALUATED. EXISTING REPAIR FOUND PREVIOUSLY ACCOMPLISHED IAW B757-200 SRM 52-30-01 FIG 205. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA.SDR 08FDEA01963None · noneEXTERNAL PATCH REPAIR ON FUSELAGE FROM BS 1701 TO BS 1708, BETWEEN S-17L AND S-19L TO BE EVALUATED. EXISTING REPAIR EVALUATED AS PER EO F-5100-7-5001 PT1 ATTACHMENT B, FOUND PREVIOUSLY ACCOMPLISHED BY ENGINEERING LIMITED REPAIR NO: MON/757/53-252/REP/502 ISSUSDR 08FDEA01961None · noneEXTERNAL PATCH REPAIR ON FUSELAGE BS 1717, BETWEEN S-20L AND S-21L, TO BE EVALUATED. EXISTING REPAIR EVALUATED AS PER EO F-5100-7-5001 PT.1 ATTACHMENT B, FOUND PREVIOUSLY ACCOMPLISHED IAW MESSAGE 1-730176994-3, WITH FAA FORM 8110-3. SUPPLEMENTAL INSPECTIONSDR 08FDEA02589None · nonePREVIOUS REPAIR FOUND LOCATED ON RUDDER RT STA270-869 RIB BR2-7, OUTER SKIN. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PERMANENT REPAIR WAS PERFORMED IAW FEDEX EA 6-5540-118158R. NOT SDR ASAA0843136None · noneCARRY OUT PREVENT MOD ON BS 348.2 TO BS 360 STR 16 PER EM 5310 02389 STEP 4. CARRY OUT PREVENT MOD ON BS 348.2 TO BS 360 STR 16 PER EM 5310 02389 STEP 4.SDR DHL2008807527None · noneREMOVED AND REPLACED EXISTING REPAIR AT FUSELAGE STA 320 LT SIDE L-28L WITH PERMANENT TYPE REPAIR PER SRM. INDICATE TYPE OF REPAIR, RE-INSPECTION INTERVAL AND NEXT REQUIRED INSPECTION (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-1 FIG 7 SHEET 1,4. RESDR HNAA0800149Tape · loosePAX AND F/A REPORTED SMALL FIRE COMING FROM NR 1 NACELLE , CENTER GEAR DOOR AREA. CREW PULLED FUEL OFF HANDLE, NO INDICATION ON FIRE LOOP. F/A POINTED OUT TO MX WHERE FIRE WAS REPORTED, MX FOUND A 4 INCH PIECE OF EROSION TAPE LOOSE ON STRUT, WHICH WAS A YELLOWSDR DHL2008807522None · noneREMOVE AND REPLACE EXISTING REPAIR AT FUSELAGE STA 1260 LONGERON 31L TO 29L WITH A PERMANENT TYPE REPAIR PER SRM OR APPROVED DATA. INDICATE TYPE OF REPAIR, REINSPECTION INTERVAL AND NEXT REQUIRED INSPECTION (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2SDR HALA0800554Unknown · unknownETOPS SIGNIFICANT SYSTEM, LEFT THROTTLE MUST BE ADVANCED ONE INCH FURTHER THAN LEFT TO SYNCHRONIZE ENGINES IN CRUSE. PERFORMED FIM 71-PIMIJ NO MSG FOUND LOOKED FOR ANY AUTO EVENTS NONE FOUND AND NO EICAS MSG. RAN BOTH ENG AT 80 PERCENT. NO THROTTLE SPLIT ANSDR 2008FA0000320Bearing · failedWHERE THE ROD END BEARING ATTACHES TO THE LATERAL BOLT, FWD. THIS BEARING (S34691 FAILED AT THE BEARING END. THIS BEARING IS UNDER EXTREEM TENSION LOAD AND WAS ORIGINAL. AGE WAS A FACTOR IN FAILING. REPLACING THIS BEARING AT 1000 HR INTERVALS IS NECESSARY.SDR QXEA200800395None · nonePDX- FLIGHT 2282 - FLIGHT ATTENDANT REPORTS THAT THE REAR PASSENGER DOOR (L2)IS HARD TO OPEN. MAINTENANCE OPERATED THE DOOR SEVERAL TIMES WITH NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE, NO PARTS REPLACED.
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