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 FDEA202110082498None · damagedZONE 220 FLOOR BOARD 222MDF IS DAMAGED. FABRICATED ZONE 220 FLOOR BOARD 222MDF ON VT MAE TRAVELER T21/1575353 IAW DWG SRZ 25-005 REVISION R. MAJOR REPAIRSDR FDEA202110082497None · damagedEDGE DAMAGE NOTED ON FLOOR PANEL 242MEF BOTTOM SIDE. FABRICATED FLOOR BOARD 242MEF ON VT MAE TRAVELER T21/1577548 IAW DWG SRZ-25-005 REVISION R. MAJOR REPAIRSDR FDEA202110082496None · damagedZONE 220 FLOOR BOARD 222MAF IS DAMAGED. FABRICATED ZONE 220 FLOOR BOARD 222MAF ON VT MAE TRAVELER T21/1575476 IAW DWG SRZ- 25-005 REVISION R. MAJOR REPAIRSDR FDEA202110082495None · damagedZONE 220 FLOOR BOARD 221MBF IS DAMAGED. FABRICATED ZONE 220 FLOOR BOARD 221MBF ON VT MAE TRAVELER T21/1575357 IAW DWG SRZ-25-005 REVISION R. MAJOR REPAIRSDR FDEA202110082494None · damagedZONE 220 FLOOR BOARD 222MEF IS DAMAGED. FABRICATED ZONE 220 FLOOR BOARD 222MEF ON VT MAE TRAVELER T21/1575352 IAW DWG SRZ-25-005 REVISION R. MAJOR REPAIRSDR FDEA202110082493None · damagedZONE 220 FLOOR BOARD 221AF IS DAMAGED. FABRICATED ZONE 220 FLOOR BOARD 221AF ON VT MAE TRAVELER T21/1575471 IAW DWG SRZ- 25-005 REVISION R. MAJOR REPAIRSDR FDEA202110082492None · damagedZONE 220 FLOOR BOARD 222BF IS DAMAGED. FABRICATED ZONE 220 FLOOR BOARD 222BF ON VT MAE TRAVELER T21/1575359 IAW DWG SRZ- 25-005 REVISION R MAJOR REPAIRSDR ABXA2021108098None · noneMAIN CARGO DOOR LIGHT CAME ON AT 400 AGL DURING TAKEOFF. AIR TURNBACK TO CVG. UNEVENTFUL LANDING AND GROUNDED BY MAINTENANCE. T/S PER IAI SUPP MM 52-71-09. FOUND S9021 OUT OF LIMITS. ADJUSTED PER 52-71-09. R+R MCD DOOR CENTRAL PANEL IAW B767 IAI SUPPLEMENT AMMSDR MASA20211008466None · bentLOWER STRIKER WAS FOUND TO BE BENT / DEFORMED FROM CONTOUR. PERFORMED PERMANENT REPAIR IAW SRM 53-21-23-001-001-A01, EA 83-2021-043.SDR MASA20211008464None · noneFUSELAGE SKIN AT FS 1051.30 AND STR 21L WAS FOUND TO HAVE DENT DAMAGE. PERFORMED PERMANENT REPAIR IAW SRM 51-24-21, EA 69-2021-095.SDR MASA20211008462None · noneFWD BAGGAGE BAY DOOR OUTER SKIN WAS DISCOVERED WITH NICKS. PERFORMED PERMANENT REPAIR IAW SRM 52-35-01-001-001-A01, FIGURE 52-35-01-991-801, ITEM 1, EA 79-2021-234SDR MASA20211008461None · noneCORROSION AFFECTING THE FLOOR BEAM AT FS1015, LBL 9.00. PERFORMED PERMANENT REPAIR IAW SRM 53-61-43-991-801, ITEM 1B, EA 80-2021-136.SDR 2021FA0000281Bracket · crackedPART NUMBER 55006610401 FOUND ON LONG BEACH AIRPORT RUNWAY 30 DURING INSPECTION BY AIRPORT OPERATIONS. TRACING OF PART NUMBER IDENTIFIED A EMBRAER 545 NOSE LANDING GEAR UPLOCK BRACKET. IT IS CRACKED AT BOTH ENDS. THE ORIGINATING AIRCRAFT IS UNKNOWN.SDR IPXA2021101975115Angle · corrodedINSPECTION TYPE:3C#2 PYLON SPAR ANGLE IS CORRODED AT STA. YID= 380.310 & ZID= 54.5.REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG. AVB7510 AND SRM 51-33-01. (MINOR)SDR GTIA2021100436030None · noneR3 DOOR EMERGENCY ASSIST BOTTLE REQ SERVICE. -SERVICED R3 DOOR EMER ASSIST BOTTLE IAW AMM 52-10-00.SDR FDEA202110022447None · noneMDIS 854 05-50 1962 02OCT21 KIX REPORTED FOR CAPTAIN EE# 216581 REF WRI 05-50-1960 KIX RWY 06L WIND 060 AT 5 KT MANUAL LANDING FROM RIGHT SEAT, HIGH SINK RATE LATE FLARE NO SIDE SLIP, NO DRIFT GENTLE NOSE GEAR LANDONG TOUCHDOWN FACT 02OCT2SDR CALA2021100401768None · damaged(AD 2019-20-10) DURING ROTO PROBE INSPECTION OF THE RH DOOR STOP FITTING #1 AT FR16. REJECTABLE DAMAGE INDICATION WAS NOTED IN UP PER I/B AND O/B HOLES DUE TO THREAD DAMAGE. () REPAIRED RH #1 DOOR STOP FITTING HOLES/AREA IAW EC/RA 5311-02639 VT MAE FINAL EA 32SDR FDEA202110012549Seat Track · unknownAIRCRAFT REPAIR ASSESSMENT:EXISTING REPAIR FOUND ON MAIN DECK SEAT TRACK BTW FR36 TO FR37,-Y450 POSITION. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, INSPECTION OF REPAIR DETERMINED IT TO BE CURRENT WITH FAA APPROVED DATA A300-600F SRM 53-10SDR FDEA202110012548Seat Track · unknownAIRCRAFT REPAIR ASSESSMENT:EXISTING REPAIR FOUND ON MAIN DECK SEAT TRACK BTW FR30 TO FR31,-Y1456 POSITION. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, INSPECTION OF REPAIR DETERMINED IT TO BE CURRENT WITH FAA APPROVED DATA A300-600F SRM 53-1SDR FDEA202110012547Seat Track · unknownAIRCRAFT REPAIR ASSESSMENT:EXISTING REPAIR FOUND ON MAIN DECK SEAT TRACK BTW FR29 TO FR30,-Y953 POSITION. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, INSPECTION OF REPAIR DETERMINED IT TO BE CURRENT WITH FAA APPROVED DATA A300-600F SRM 53-10SDR ASMF202110000023None · noneDURING TRANSIT CHECK, IT WAS DETECTED SEVERAL LIGHTNING STRIKE ON FUSELAGE SKIN. MAINTENANCE PERSONNEL PERFORMED A LIGHTNING STRIKE CONDITIONAL INSPECTION PHASE 1A, LEVEL EXAMINATION AND PHASE 1B AND II, GENERAL VISUAL INSPECTION AND SYSTEM COMPONENTS IAW AMM SDR SWIA202162721None · crackedREPLACE THE CRACKED RH AFT DRAG ANGLE FOR VERTICAL STABILIZER REAR SPAR. (C-CHECK RO 11-20-2021) REPAIRED THE RH AFT DRAG ANGLE FOR THE VERTICAL STABILIZER BY CUTTING AWAY DAMAGE, FABRICATING AND INSTALLING REPAIR PARTS REF CRJ700 SRM 55-31-00-201-001-A01SDR CALA2021100101730Stringer · corrodedA3NB-05-3-6022:BULK CARGO COMPT FR 64-65 STRINGER 44 HAS CORROSI ON DOT 116-66 () SPLICE AND STRINGER IAW SRM 51-42-11 FROM FR 63 TO FR 67, CUT SECTION OUT OF DAN50B08 BATCH #2478344, D5348003020700 AND SPLICE, FACTORY SPLICE AND STRINGER REPAIR SECTION IAW SRSDR CALA2021100101729Stringer · corrodedA3NB-05-3-6022: BULK CARGO COMPT FR 63-64 STRINGER 42R HAS CORRO SION. DOT 116-65 () 283-002. REPAIRED STRINGER SECTION 42 BETWEEN FR63 TO FR64 IAW INSPECTION THRESHOLD FROM TIME OF ADL/REPAIR EMBODIMENT IS SRM 53-00-13-300-001, FIG 001, SHT 1. DIM CUT OUT LIMSDR GTIA2021093036018None · noneL2 DOOR ASSIST BOTTLE REQ SERVICE-SERVICED L2 DOOR ASSIST BOTTLE IAW AMM 52-10-00SDR IPXA2021092974396Floorbeam · corrodedINSPECTION TYPE:SEG4MAIN CABIN FLOOR BEAM BETWEEN 24.75 RBL - 45.5 STA 1200 SHOWING SIGNS OF CORROSION.REPAIR PER EA# 757-5360-27-A2671 REV-.SDR IPXA2021101374900Floor Panel · damagedINSPECTION TYPE:A300PNL 231LG BROKEN.FABBED IAW SREO A300-5320-40552-B.SDR IPXA2021100774692Floor Panel · noneINSPECTION TYPE:CFWD MAIN CABIN L/H SIDE FLOOR PANEL 231PH JUST INSIDE MAIN CARGO DOOR HAS DAMAGE TO LOWER SURFACE AS MARKEDCOMPLIED WITH SREO A300-5320-42722-FSDR IPXA2021100874733Floor Panel · noneINSPECTION TYPE:CFWD L/H MAIN CABIN FLOOR 231MJ JUST INSIDE MAIN CARGO DOOR HAS BROKEN CORNER INSERT AS MARKEDCOMPLIED WITH SREO A300-5320-42722-FSDR IXXA20211018078Stiffener · crackedWEB ON STIFFENER AT STATION 971 LBL 90 HAS DAMAGED HOLE. REMOVED, FABRICATED AND REPLACED NEW STIFFNER AT STATION 971 LBL 90 IAW ENGINEERING ORDER 74783FAB01.SDR FDEA202109272551Skin · unknownAIRCRAFT REPAIR ASSESSMENT :EXISTING EXTERNAL DOUBLER FOUND ON FUSELAGE SKIN BTW FR101 TO FR103 AND STR-2L TO STR-5L POSITION. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, INSPECTION OF REPAIR DETERMINED IT TO BE CURRENT WITH FAA APPROVED DATSDR FDEA202109272550None · unknownAIRCRAFT REPAIR ASSESSMENT :EXISTING EXTERNAL DOUBLER FOUND ON RUDDER TRAILING EDGE APEX AREA LOCATED BTW T/E SCREW LINE NO.20 AND NO.21 FASTENER COUNTED FROM LOWER SIDE. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, INSPECTION OF REPAIR DETERSDR GTIA2021092736012None · noneL1 DOOR ASSIST BOTTLE REQUIRES SERVICE -SERVICED L1 DOOR ASSIST BOTTLE IAW AMM 52-10-00SDR GTIA2021092736009None · noneL2 DOOR ASSIST BOTTLE REQUIRES SERVICE -SERVICED L2 DOOR ASSIST BOTTLE IAW AMM 52-10-00SDR MASA20211004453Skin · damagedFUSELAGE SKIN AT FS 1051.30 AND STR 21L WAS DELIVERED WITH DENT DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 51-21-11, 51-25-06, 51-25-16, 51-21-11, EA 69-2021-159SDR FDEA202109242462Beam · corrodedAFT CARGO AT ABOVE LOWER LATCH SPOOLS-CLOSE OUT WEB FITTING SHOWS EVIDENCE OF EXFOLIATED CORROSION.(AREA MARKED) REMOVED CORROSION ON BEAM P/N: AGA7216-1 REF MD11 SRM 53-00-15-2R PG 22-24 REPAIR 6, DAC DWG AGA7216SDR IXXA20211018077Failsafe · crackedRIGHT FAILSAFE STRAP AT STA 955 HAS A CRACK INDICATION ON ULTRASOUND NDT INSPECTION. REPAIRED FAILSAFE STRAP AT STATION 955 IAW AMES ENGINEERING ORDER 472070RD04.SDR IXXA20211018075Flap · delaminatedLEFT WING TRAILING EDGE INBOUND TRAILING EDGE PLAP HAS DELAM AREA ON INBOUND EDGE. LAYED UP AND CURED IAW B767 SRM 51-70-10.SDR IXXA20211018074Beam · crackedINBOUND HYD BAY LATCH CHANNEL IS CRACKED AT #3 LATCH MOUNT AREA. REMOVED AND REPLACED BEAM IAW B767 SRM 51-40-02.SDR IXXA20211018069Skin · delaminatedRIGHT SIDE VERTICAL BETWEEN THE AUX SPAR AND FRONT SPAR THE COMPOSITE SKIN PANEL IS DELAMINATED. REPAIRED RIGHT SIDE VERT STAB PANEL BETWEEN THE AUX SPAR AND FT SPAR IAW B767 SRM 51-70-10 R4.SDR GTIA2021092736004None · noneDURING INITIAL CLIMB - VERY LARGE SINGLE BIRD STRIKE TO AN UNKNOWN AREA OF THE AIRCRAFT. RETURNED SAP FOR INSPECTION CORRETION - JL - LEFT WINGLET.-PERFORMED INSP OF AIR FRAME AFTER BIRD STRIKE NO DAMAGE FOUND TO FUSELAGE, PYLON AND NACELLS, NO EVIDENCE OF BIRSDR IXXA20211018067Web · crackedFWD DOUBLER ON FAIRING SUPPORT WEB AT TA 1081 CRACKED, FABRICATED AND REPLACED NEW DOUBLER IAW B767 SRM 51-10-02.SDR IXXA20211017066Doubler · crackedAFT DOUBLER ON FAIRING SUPPORT WEB AT STA 1081 CRACKED. FABRICATED AND REPLACED NEW DOUBLER IAW B767 SRM 51-10-02.SDR HNAA2021101800516None · noneL/H WING RIB 21 INSIDE 551CB CRACKED .... PERFORMED REPAIR ON L/H WING RIB 21 INSIDE 551CB PNL IAW EMB 145 SRM 57-20-07 ITEM 4 FIGURE 203 DET C AND PIEDMONT EO1-57-21-0280SDR IPXA2021092374183Floorbeam · corrodedINSPECTION TYPE:SEG4MAIN CABIN FLOOR BEAM BETWEEN 24.75 RBL - 24.75 LBL STA 110 SHOWING SIGNS OF CORROSIONREPAIRED PER EA# 757-5340-27-A2673 REV-SDR 2021FA0000263None · noneTHE START BATTERY CONTACTOR WAS IMPROPERLY INSTALLED ON MULTIPLE AIRCRAFT DURING PRODUCTION. THIS ALLOWS THE CONTACTOR TO RETAIN MOISTURE AND SHORT OUT ELECTRICAL CIRCUITS. THIS CAN IN FLIGHT LOSS OF POWER AND HIGH AMPERAGE SHORTING.SDR JJBA20210922034None · noneCORROSION FOUND ON CENTER AISLE LH OMEGA BEAM LOCATED BETWEEN FR 23- FR 29. REMOVED AND REPLACED LH OMEGA BEAM, LOCATED BETWEEN FR 23-FR29SDR SWIA202162859None · corrodedPAX DOOR UPPER SILL ANGLE IS CORRODED BETWEEN F.S. 310 TO F.S. 349. (C-CHECK RO 11/28/2021) PAX DOOR SILL ANGLE WAS REMOVED AND A NEW PART SH670-31825-9 WAS INSTALLED IAW CRJ 700 SRM 51-41-04-01-001-A01 ALL OPS CHECKS GOODSDR IXXA20211018076Former · crackedNOSE FORMER IS CRACKED BY #9 SLAT INBOUND AUX TRACK AT WING LEADING STATION 562. REMOVED AND REPLACED DAMAGE NOSE FORMER IAW B767 SRM 51-40-02.SDR IXXA2021100018075Rib · crackedLEFT WING LEADING EDGE AT APPROXIMATELY LES 563.0 HAS CRACKED NOSE RIB. REMOVED AND REPLACED NOSE RIB ON LEFT WING LEADING EDGE AT WS STA 565.9 IAW B767 51-40-02.
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