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 FDEA202203081172Seat Track · noneREPAIR ASSESSMENT: MAIN DECK L/H SIDE STA APROX. 1410 - 1530 LBL 47.5 HAS EXISTING SEAT TRACK REPAIR DOT 39. REPAIRED PER SRM 53-00-52 FIG.201. REPAIR 1.SDR FDEA202203081171Seat Track · noneREPAIR ASSESSMENT: MAIN DECK R/H SIDE STA APROX. 1129 - 1269 RBL 8.5 HAS EXISTING SEAT TRACK REPAIR DOT 38. REPAIRED PER SRM 53-00-02 FIG. 201, REPAIR 1.SDR FDEA202203081170Seat Track · noneREPAIR ASSESSMENT: MAIN DECK R/H SIDE STA APROX. 815 - 909 RBL 75.5 HAS EXISTING SEAT TRACK REPAIR DOT 37. REPAIRED PER SRM 53-00-52 F. 201, REP.1SDR FDEA202203081169Seat Track · noneREPAIR ASSESSMENT: MAIN DECK R/H SIDE STA APROX. 745 - 785 RBL 8.5 HAS EXISTING SEAT TRACK REPAIR. EXISTING MAJOR REPAIR PREVIOUSLY INSTALLED PER SRM 53-00-52-2R REPAIR 1, FIG. 201, SHT. 1 - 3.SDR FDEA202203070436None · none1859Z AT FL 290 ENCOUNTERED SEVERE TURBULENCE. TWO OVER SPEEDS WERE NOTED DURING THE EVENT OVER SPEED WAS APPROXIMATELY 40 KNOTS . OVERALL AIRSPEED LOSS AND GAIN APPROXIMATELY 50 KTS. ALTITUDE LOSS AND GAIN WAS 1000 . FINALLY GOT CONTROL OF THE AIRCRAFTSDR CALA2022030900610None · corrodedFLOOR SUPPORT ON OUTBOARD SIDE BY L1 DOOR HAS CORROSION BETWEEN STA 312 THRU STA 348.2 (REF AAR RFD NR REPLACED INNER CHORD & ANGLE ATTACHED TO INNER CHORD ON OUTBOARD SIDE BY L1 DOOR BETWEEN STA. 312 THRU STA. 348.2 IAW B737-900 S RM 51-40-02-0G-0 & DWG 143A5SDR GTIA2022030736311None · noneSUSPECTED FUME EVENT ON SHORT FINAL-ACCOMPLISHED TSM 05-50-00 INSPECTED APU COMPARTMENT FOR LEAKS NO LEAKS FOUND GVI ENG 1&2 DEOILER SEALS SEALS WERE GOOD RAN BOTH ENGINES AND USED SNIFFER NOFUMES FOUND IAW AMM 71-00-00 A/C OK FOR COUNITED USESDR IXXA2022060803Ceiling Panel · corrodedALC CEILING PANEL SUPPORT CORRODEDSDR YENA2022030700126None · noneFLT#399,LGA-MCO."FUMES EVENT DESCENDING THROUGH 5000 FT. NOTICED IN COCKPIT,FWD LAV AREA,AND STRONGEST AT AFT F/A JUMPSEAT;AS PRECAUTIONARY OPERATED BOTH ENGINES WITH PACKS BLD AND APU BLEED ISOLATED EACH INDIVIDUALLY NO ODOR NOTED.COMPLIED WITH INFO NOTICE 20SDR YENA2022030700125None · noneFLT#2895,BOS-PUJ.'COCKPIT SMELLED OF PLASTIC IN DESCENT F/A HAS METALLIC TASTE;COMPLIED WITH INFORMATION NOTICE 2017-T015 SECTION A(A) ISOLATED FAULT TO TYPE 10(A)1,C PER TSM 05-51-00-810-085-A. TSM 05-50-00-810-085-0D. THIS IS A LEVEL 1 TRANSIENT ODOR EVENT. SDR AC2A202208069201Flange · crackedFOUND WELDMENT ASSEMBLY CRACKED AT FLANGE.SDR IXXA2022051202Support Channel · corrodedTHE ROLLER TRAY SUPPORT IS CORRODED ON THE LOWER SURFACE, AT RBL20 FROM STA 1395 TO STA 1417SDR IXXA2022050706Frame · corrodedCORROSION ON THE LOWER SURFACE OF THE UPPER FRAME CHORD, AT STA.1175 (ALC FLOOR LEVEL) FROM LBL42 TO RBL42SDR CALA2022030300548Intercostal · cracked(AD 2019-20-10) FR16 RH DOOR STOP FITTING FRAME HOLES, FITTING # 7 UPPER AND LOWER I/B HOLES HAVE CRACK INDICATIONS. HOLES CIRCLE D IN RED. REPAIR BEFORE NEXT FLIGHT PER EA 5311-02164.() TRANSFERRED TO ELB 809638, REF THIS LOG FOR WORK ACCOMPLISHEDSDR CALA2022030300547Intercostal · cracked(AD 2019-20-10) FR 16 RH DOOR STOP FITTING FRAME HOLES. FITTING #1, LOWER I/B HOLE HAS CRACK INDICATIONS. HOLE CIRCLED IN RED. R EPAIR BEFORE NEXT FLIGHT PER EA 5311-02164. () TRANSFERRED TO ELB 809638, REF THIS LOG FOR WORK ACCOMPLISHEDSDR IXXA2022040502Panel · crackedL/H FILLET PNL 195FL HAS COMPOSITE DAMAGESDR GTIA2022030436304None · noneDIRT SOCK SMELL ON DECENT. SHUT OFF PACK 1 ALEAVED SMELL-FIND NO SMELL ON PACK 1. NO MX REQUIREDSDR IXXA2022040501Panel · crackedVERT STAB REMOVABLE L/E PANEL 321E MOST UPPER L/E COMPOSITE ERODED & CRACKEDSDR CALA2022022800511None · cracked(SUPPORT TASK) LH AFT DOOR FR68 DOOR STOP FITTING #1 I/B LOWER H OLE HAS A CRACK INDICATION, HOLE IS CIRCLED IN BLACK, NEEDS TOBE REPAIRED BEFORE NEXT FLIGHT. () NOTED IAW NTM 51-10-01, INSTALLED FREEZE PLUG. REINSTALLED #1 FROM TIME OF ADL/REPAIR EMBODIMENT 3SDR FDEA202202240929Floorbeam · corrodedCORROSION WERE FOUND ON FLOOR BEAM UPPER T-CHORD LOCATED STA 880 LBL 45-60 WORK ACCOMPLISHED IN ACCORDANCE WITH FEDEX E.A # F-5310-T0367576 B, FLOOR BEAM ASSY, STA 879, UPPER CHORD, BL 45-68 CORROSION, REPAIR. MAJOR REPAIRSDR FDEA202202240779Skin · noneUNDOCUMENTED COMPOSITE REPAIR WERE FOUND ON SKIN EMPENNAGE STA 1981.9-1941 11 O'CLOCK POSITION PERFORMED TAP TEST INSP. PER SRM 51-10-06 AND EVALUATED I.A.W CASCADE AEROSPACE WORK CARD 07765 NR0408 AND NR0407 AND NO DAMAGE OR DEVIATIONS NOTED. FOR RECORD SDR FDEA202202240778Skin · unknownUNDOCUMENTED COMPOSITE REPAIR WERE FOUND ON SKIN EMPENNSGE STA 1918.9-1941 12 O'CLOCK POSITION PERFORMED TAP TEST INSP PER SRM 51-10-06 AND EVALUATED I.A.W CASCADE AEROSPACE WORK CARD 07765 NR0408 AND NR0407 AND NO DAMAGE OR DEVIATION NOTED. FOR RECORD PUSDR FDEA202202240766Flap · noneUNDOCUMENTED COMPOSITE REPAIR ON L/H WING OUTER AFT FLAP LOWER SURFACE 11" FROM AFT EDGE 105" FROM OUTBD EDGE PERFORMED WET LAYUP REPAIR FOR MENTIONED AREA PER SRM 51-70-17, REF SRM 57-53-01- 2R-1 REPAIR 1, FIG.201 DETAIL IV TABLE II REP.DIM: 4". REP. LOCSDR FDEA202202240763Skin · unknownUNDOCUMENTED COMPOSITE REPAIR WERE FOUND ON STA 1963.8-1992.8 STR 6 O'CLOCK POSITION PERFORMED HOT BOND REPAIR PER SRM 51-70-10-2R, REF. SRM 53-80-01-2R, DETAIL 1. REP. DIM:5.5" REF. LOCATION: 6.5" FROM FWD EDGE OF PANEL AT 6 O'CLOCK. MAJOR REPAIRSDR FDEA202202240740Seat Track · crackedCRACK ON SEAT TRACK LOCATED STA1580-1600 RBL 45 WORK ACCOMPLISHED PER FEDEX E.A # F-5300-T0367320: SEAT TRACK AT STA 1580-1600 RBL 58.22, CRACK, PERMANENT REPAIR MAJOR REPAIRSDR FDEA202202240708Channel · unknownUNDOCUMENTED REPAIR WERE FOUND ON 2 CHANNEL LOCATED STA 1380-1400 RBL 11 PERFORMED NEW SRM REPAIR PER SRM 53-60-52-2R, AND PER SRM 51-70-12 TYPICAL EXTRUDED REPAIR, THIS REPAIR IS A CAT. A REPAIR AND NO SUPPLIMENTAL INSP. ARE REQUIRED. MAJOR REPAIRSDR FDEA202202240707Seat Track · corrodedCORROSION ON SEAT TRACK LOCATED STA 1540 LBL 45.5 PERFORMED SEAT TRACK REPAIR USING NEW SEAT TRACK SECTION , 2 EA ANGLES, AND STRAP PER SRM 53-00-52, FIG 201, REPAIR 1. THIS REPAIR IS A CATEGORY "A" REPAIR AND NO SUPPLEMENTARY INSP. ARE REQUIREDSDR FDEA202202240642Channel · unknownUNDOCUMENTED SPLICE REPAIR WERE FOUND ON Z-CHANNEL OF FWD CARGO FLOOR STRUCTURE LOCATED STA 560-580 RBL 29 PERFORMED DVI PER SRM 51-10-08 AND EVALUATED I.A.W SRM 51-70-12 AND NO DAMAGE OR DEVIATIONS NOTED THIS IS A MAJOR REPAIRSDR FDEA202202240641Channel · corrodedUNDOCUMENTED SPLICE REPAIR WERE FOUND ON Z-CHANNEL OF FWD CARGO FLOOR STRUCTURE LOCATED STA 560-580 LBL 8 PERFORMED DVI PER SRM 51-10-08 AND EVALUATED I.A.W SRM 51-70-12 AND NO DAMAGE OR DEVIATION NOTED. THIS IS A MAJOR REPAIRSDR FDEA202202240639None · noneMULTIPLE CORROSION ON SEAT TRACK BETWEEN STA 1280-1320 RBL 45 PERFORMED SEAT TRAK REPLACEMENT USING A NEW FABRICATED SEAT TRACK PER SRM 53- 00-52, FIG 201 REPAIR 1. AND FEDEX GMM 7-0-1001. THIS REPAIR IS A CATEGORY "A" REPAIR AND NO SUPPLEMENTARY INSP. ARSDR YENA2022030100105None · noneFLT # 54, PBI-JFK. DESCENDING THROUGH AROUND FL230 TO TOUCHDOWN THERE WAS A VERY STRONG ODOR LIKE BURNING CHEMICAL THROUGHOUT THE AIRCRSFT ISOLATION PROCEDURE ACCOMPLISHED WITH LITTLE SUCCESS.; COMPLIED WITH INFORMATION NOTICE 2017-T015, SECTION B (2),AND PERFSDR YENA2022030100104None · noneFLT # 54, PBI-JFK. DESCENDING THROUGH AROUND FL230 TO TOUCHDOWN THERE WAS A VERY STRONG ODOR LIKE BURNING CHEMICAL THROUGHOUT THE AIRCRSFT ISOLATION PROCEDURE ACCOMPLISHED WITH LITTLE SUCCESS.; COMPLIED WITH INFORMATION NOTICE 2017-T015, SECTION B (2),AND PERFSDR YENA2022022400088None · noneFLT# 795, JFK-AUS. FUME ODOR SMELLED ON DESCENT FROM 19,000 TO 12,000 CAPT SMELT ACETONE PAINT SMELL PACK 1 TURNED OFF AND MASK DONNED; COMPLIED WITH INFORMATION NOTICE 2017-T015 SECTION A (A) ISOLATED FAULT TO TYPE 10 (A) 1, C PER TSM 05-51-00-810-085-A TSM 0SDR FDEA202202210365Support · corrodedCENTER CARGO COMP: FLOOR SUPPORT AT STA 1781 LBL 8 UNDER FLOOR PANEL 183LG HAVE SIGNS OF CORROSION REMOVED AND REPLACED FLOOR SUPPORT AFA 7115-25 AT CENTER CARGO COMPARTMENT STA 1781 LBL 8 REF. SRM 51-31-01-0G AND SRM 51-33-01-0GSDR YENA2022022400087None · noneFLT # 1058, AUA-JFK. IN CRUISE C FL300 WE PASSED THRU SOME WEATHER WITH MODERATE TURBULENCE AND LIGHT RAIN. SHORTLY AFTER ENTERING THE WX, WE HAD A SMELL OF ELECTRICAL SMOKE IN THE COCKPIT. THE INFLIGHT REPORTED THE SAME SMELL IN THE FWD CABIN-STRONGEST AROUNDSDR HNAA2022022400116None · nonePDIS 635 05-50 2696123 19FEB22 CLT CLOSE
FLAP OVERSPEED AT 150 KTS FOR 1-2 SECONDS AT 2500 TO 3000FT WITH FLAPS AT 45
FACT 19FEB22 13:56 CLT
INSPECTED A/C IAW AMM 05-50-07. NO MAINTENANCE ACTION IS NEEDED AT THIS TIME.SDR HNAA2022022400115Not Reported · not reportedPDIS CLT 19FEB22 DURING FLIGHT LOST RMU 1 PFD1 NAV 1 FMS 1 AND MFD2 AND REMAINED OFF THROUGHOUT FLIGHT
FACT 19FEB22 15:11 UPON MX ARRIVAL TO A/C THE AVIONICS MASTER 1 PB WAS IN THE OFF POSITION. SUSPECT SWITCH FAILURE FROM TURBULENCE IN SEQ 1 TSDR HNAA2022022400114Not Reported · not reportedPDIS 635 05-50 2606121 19FEB22 CLT CLOSE
DURING DESCENT A/C EXPERIENCED SEVERE TURBULENCE
FACT 19FEB22 14:48 CLT
PERFORMED SEVERE TURBULENCE INSP/ CHECK IAW AMM 05-50-27NO DAMAGE FOUNDSDR GTIA2022022136293Not Reported · not reportedAFTER T.O. POWER REDUCTION THE OIL QUANTITY WENT DOWN TO APPROX 6.2 QT. WE GOT THE ADVISORY AND FLASHING INDICATION. IT SHOWED 8.5 DURING THE APPROACH AND LANDING-SRVCD ENG #2 IAW AMM 12-13-79 W/9QTS OF OILSDR 2022FA0000092Skin · scratchedDURING OVERNIGHT INSPECTION AT HEBRON, KY (CVG) THE FUSELAGE SKIN ON L/H SIDE WAS FOUND WITH A SCRATCH. THE SCRATCH IS LOCATED BETWEEN FS 881 AND FS897 ALONG STRINGER 15L LINE AND MEASURES .4915" LONG X 0.0201" WIDE X 0.0075" DEEP (NOT INCLUDING PAINT LAYER). SDR GTIA2022022136290None · noneDURING DESCENT THROUGH 40000' F/A REPORTED "DIRTY SOCK" SMELL IN AFT CABIN. APU WAS OFF. CHECK-LIST PERFORMED. SMELL WAS THEN REPORTED AS VERY FAINT-TROUBLESHOT IAW TSM 05-50-00-810-831-A. FOUND APU TO BE SORCE OF AIR QUALITY EVENT. SEE LP 2810952-02 FOR APU DSDR FDEA202202150302Frame · crackedBS 1640 S-14R I/B BOTTOM HOLE HAS CRACK INDICATIONS AT 4 & 9 O'CLOCK LOOKING AFT // BS 1640 S-14R O/B BOTTOM HOLE HAS A CRACK INDICATION AT 5 O'CLOCK LOOKING AFT. ACCOMPLISHED FRAME REPAIR AT STA. 1640 BTW STR. 9 & STR 20 IAW EA # F-5310- T0366462 "FUSELAGSDR FDEA202202140450None · noneCENTER CARGO, STA 1801-1821, LONGERON 46R, AT SLPICE AREA, AFT OUTBOARD VERTICLE SIDE OF LONGERON HAS A CRACK. REPLACED CRACKED LONGERON 46R FROM STA 1811 TO 1828 AND FABRICATED NEW SPLICE REF SRM 53-00-05-2R REPAIR 1 FIGURE 201 AND 202 SHEET 1, 2, AND 3 ASDR FDEA202202120363Skin · corrodedR/H EMPENAGE FUSELAGE SKIN COMMON TO LOWER AFT FUSELAGE FAIRING NUTPLATE HOLES AT STA. 2140 TO 2160 HAS SURFACE CORROSION. MARKED RED. TRIMMED OUT CORRODED SKIN AND APPLIED DOUBLER REPAIR IAW SRM 53-70-01-2R REP3 FIG 201SDR EVCA021222Compressor · leakingVISIBLE WHITE SMOKE NOTED FROM VENTS WHEN PILOT TURNED ON ANTI ICE.SDR ASAA2022021137494None · corrodedAFT CARGO LH TRANSITION HAS CARROSION FROM STA 727C TO 727F. GROUNDED - YES. BLENDED CORROSION FOUND TO BE OUT OF LIMITS IAW B737-900 SRM 53-00-53-1A-2 REPAIRED TRANSITION IAW B737-900 SRM 53-00-53-2R-5W=1.0 O=.040 R=.034 L=3.00 D=.006.SDR FDEA202202110276None · failedPDIS 615 05-50 1092 10FEB22 MEM FACT U REJECT AT 65 KNOTS DUE TO MASTER CAUTION. ALERT APPEARED WITH MASTER CAUTION BUT CLEARED WHEN THROTTLES REDUCED BEFORE WE HAD TIME TO READ. OAT 18 C. GROSS WEIGHT 408.0 UPDT 11FEB22 03:00 MEM U SINCE SDR FDEA202202100813Seat Track · corrodedMAIN DECK - SEAT TRACK LOBES/NUTPLATE HOLES HAVE SURFACE CORROSION AT STA 760, LBL 47. ENTERED IN ERROR.SDR FDEA202202100976Seat Track · corrodedMAIN DECK - SEAT TRACK HAS CORROSION AT STATION 1791 RBL 50 SEAT-TRACK ATTACH LOBE REPAIR PER SRM#53-00-52-2R FIG-201 SHT-1 PG-26SDR FDEA202202100535Seat Track · corrodedMAIN DECK- SEAT TRACK AT STA 5-11 - 5-52 AND THE 10 LBL HAS 2 LOCATIONS WITH PITTING CORROSION. REPAIRED SEAT TRACK BETWEEN STA 1371-1510, LBL8 AT EXISTING SPLICES LOCATIONS REF SRM 53-00-52-2R FIG 201 REPAIR 1 SHEET 1. ALONG WITH JPF ITEMS 1-7.
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