JASC 5753
Service difficulty reports · 31,513
Reports filed under 5753 · Trailing Edge Flaps, 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 = '5753' 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 = '5753' 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 JJBA20240325090Angle · corrodedRH IB FLAP IB ANGLE CORRODED. OLD ANGLE REMOVED, NEW ANGLE PARTIALLY INSTALLED. INSTALLATION OF NEW BRACKET COMPLETEDSDR SWAA2024031159732Fairing · pulled# FLAP TRACK FAIRING AFT CONE HAS 3 EA PULLED FASTENERS ON OUTBD SIDE<[01] REMOVED AND REPLACED #3 FLAP TRACK FAIRING AFT CONE REF AMM 27-51-18SDR JGVR20240306001Skin · corrodedBLENDED CORRODED AREAS UNDER THE NUTPLATES COMMON TO THE LH & RH WING FLAP PANELS 523AB AND 623AB, PERFORMED NDT, AND REPORTED FOR REPAIR DISPOSITION. REPAIRED AREAS BY FABRICATING AND INSTALLING REPAIR DOUBLERS IN ACCORDANCE WITH NETJETS RFTS-110102.SDR DALA2024030603059Roller · wornSHIP 3418 LEFT WING O/B FLAP, O/B ROLLER WORN. CORRECTIVE ACTION: REMOVED AND REPLACED ROLLER W/REF A330 AMM 27-54-73. OK FOR SERVICE. (0232284)SDR SWAA2024041159046Fairing · damagedRIGHT NR 6 FLAP TRACK AFT FAIRING WITH ELONGATED HOLES AT OB MID SEAL INSTALLATION. REPAIRED DAMAGE AND RESTORED AREA AT NR 6 FLAP TRACK FAIRING O/B MID SEAL AREA IAW SRM 51-70-04-2R-9.SDR SWAA2024041159047Fairing · damagedLEFT NR 3 FLAP TRACK AFT FAIRING WITH ELONGATED HOLES AT OB MID SEAL INSTALLATION. REPAIRED DAMAGE AND RESTORED AREA AT #3 FLAP TRACK FAIRING AS PER SRM51-70-04-2R-9.SDR SWAA2024041159612Skin · delaminatedLEFT WING OTBD AFT FLAP INBD T/E LOWER SURFACE AREA DELAMINATED. REMOVED AND REPLACED LT WING OTBD FLAP AFT FLAP AND ALSO ACCOMPLISHED ADJUSTMENT IAW AMM 27-51-22-400-801,SDR SWAA2024041159616Skin · delaminatedRIGHT WING OTBD AFT FLAP INBD LOWER T/E AREA DELAMINATED. REMOVED AND REPLACED R/H WING O/B FLAP AFT FLAP AND ALSO ACCOMPLISHED ADJUSTMENT AS PER AMM 27-51-22-401-NG.SDR JJBA20240318068Angle · corrodedLH OB FLAP IB ANGLE CORRODED. AT LH OB FLAP, ANGLE BRACKET REMOVED FOR REPLACEMENT. CORROSION FOUND ON BRACKET OUTBOARD FLAP WING BLENDED. NEW LH OB ANGLE INSTALLEDSDR IPXA2024030479473Skin · damaged*SDR FILED OPEN* L/W INBD UPPER FLAP UPPER SURFACE SKIN DAMAGE FOUND ADDITIONAL DAMAGE TO INNER SKIN AT REPAIR LOCATION. STOP DRILLS THRU LOWER SKIN AT TWO LOCATIONS. PARTIALLY REMOVED LOWER FLAP SKIN FOR ACCESS.SDR ASAA2024030448792Skin · dentedLESSOR ITEM 767 RH WING TRAILING EDGE IB FLAP LOWER SURFACE I/B CLUSTER OF DENTS REQUIRES REPAIR. GROUNDED - YES. REPAIRED RH WING TRAILING EDGE IB FLAP LOWER SURFACE I/B CLUSTER. FINAL DIMENSIONS OF REPAIR ARE 12.5"W X 11.8"L LOCATED 47.5" FROM INBRD AND STOPSDR DALA2025103107962Vane · corrodedCORROSION ON LOWER SKIN OF OUTBD FLAP VANE AT RT WING. OTBD FLAP VANE AT RT WING WAS REPLACED BY ONE SERVICEABLE OTBD FLAP VANE (0228760).SDR SWAA2024040958576Panel · debondedDEBONDED IB MAIN FLAP WEDGE PANEL LOWER SURFACE O/B SIDE AT RT WING. REPAIRED IB MAIN FLAP WEDGE PANEL LOWER SURFACE O/B SIDE AT RT WING IAW B737-700 SRM 57-53-01-2R-7 REPAIR 7.SDR UIEA2024022600130Skin · delaminatedRHW O/B FORE FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA IAW SRM 51-70-07 PAR 5.C. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024022600131Skin · delaminatedLHW O/B FORE FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA IAW SRM 51-70-07 PAR 5.A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024022600132Skin · delaminatedLHW O/B FORE FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA IAW SRM 51-70-07 PAR 5.A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024022600133Skin · delaminatedRHW I/B AFT FLAP FOUND DELAMINATION. PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.C. NO FURTHER DEFECTS NOTED</P>)SDR SWI202405080360Vane · chafedRIGHT INBOARD FLAP, FLAP VANE. LEADING EDGE AT FLS72 IS CHAFED. (MARKED) (C-CHECK RO 5/6/2024) REMOVED AND INSTALLED 1EA NEW R/H INBD FLAP VANE CAP AT FLS72 PER CRJ700SRM 51-42-13-001-001-A01 AND CRJ700SRM 51-23-00-001-001-A01 AND DWG CC670-14010 REV -F. SSDR SWIA202405080302Skin · damagedLEFT INBOARD FLAP LOWER SKIN HAS A CREASE FLS 41 AND 5.5 INCHES FROM THE TRAILING EDGE. (MARKED) (C-CHECK RO 5/6/2024) L/H I/B FLAP LOWER SKIN HAS BEEN REPAIRED REF CRJ SRM 57-52-01-201-002-A01, TYPE 4, PERMANENT NON FLUSH REPAIR.. COMPLIED FULLY W/SKYCASDR AALA202404296468Skin · debondedAIRCRAFT WAS GROUNDED: LEFT WING TRAILING EDGE OUTBOARD FLAP TRAILING EDGE LOWER SURFACE EXTERNAL BONDED REPAIR HAS BECOME DISBONDED AND STARTING TO FAIL 66 INCHES FROM THE INBOARD EDGE. MAINTENANCE REPLACED THE FLAP ASSEMBLY PER TASK CARD 26L00027009.SDR JR2R20240427728Skin · crushedRH O/B FLAP FAIRING 633BB CRUSHED RH O/B AFT FLAP SKINSDR AALA202403086468Skin · debondedAIRCRAFT WAS GROUNDED: LEFT WING TRAILING EDGE OUTBOARD FLAP TRAILING EDGE LOWER SURFACE EXTERNAL BONDED REPAIR HAS BECOME DISBONDED AND STARTING TO FAIL 66 INCHES FROM THE INBOARD EDGE. **SUPPLEMENTAL REPORT WILL BE SUBMITTED ** (OPEN)SDR DALA2024030402977Bonding Plate · damagedSHIP 3128 DAMAGED BONDING PLATE FLAP TRACK FAIRING 631CB ON RH WING. CORRECTIVE ACTION: REPAIRED PER ER/A 615323-14. (0226234)SDR DALA2024030402976Bonding Plate · damagedSHIP 3128 DEBONDED BONDING PLATE FLAP TRACK FAIRING 2 (531CB) ON LH WING. CORRECTIVE ACTION: REPAIRED PER ER/A 615323-14. (0226204)SDR DALA2024030402975Bonding Plate · damagedSHIP 3128 DAMAGED BONDING PLATES WERE FOUND AT FLAP TRACK #2. CORRECTIVE ACTION: REPAIRED PER ER/A 615323-14. (0226196)SDR SWAA2024030557869Retainer · crackedAFT UPPER TRAILING EDGE SEAL RETAINER JUST O/B OF THE #3 FLAP TRACK IS CRACKED<[01] REMOVED AND REPLACED SEAL RETAINER FITTING IAW SRM 51-40-02.;[02] C/W INSPECTIONSDR YENA2024030500330Skin · debondedDURING HEAVY MAINTENANCE: DEBONDED OB FLAP SURFACE ON RH WING; REPAIRED OB FLAP LOWER SURFACE ON RH WING IAW EC# A24-129-01, EA# 57-0022-24 REVISION 0 AND EA# 57-0022-24 PART 1. TOOL USED: DIGITAL CALIPER: P/N 500-197-30, S/N A21043111, DUE DATE: JUL/20/2024. SDR IPXA2024040823808Skin · crackedTHE R/H CENTER FLAP ASSY HAS 1EA CRACK (TOTAL), AT RIB LOCATION 12 AFT. DEFECT MARKED IN RED ON THE UPPER SURFACE. REVIEWED. EMOVED FLANGE CRACKED AND FABRICATED NEW REPAIR FLANGE WITH MATERIAL 2024-T3 .056C BATCH 0004237066. TREATED AND PRIMED NEW REPAIR FLANSDR IPXA2024040823096Skin · crackedTHE L/H CENTER FLAP ASSY HAS 1EA CRACK (TOTAL), AT RIB LOCATION 26 FWD. DEFECT MARKED IN RED ON THE UPPER SURFACE. REVIEWED. REMOVED CRACKED FLANGE AT CENTER FLAP RIB 26 BETWEEN STR 2.6 TO STR 2.7 AND FABRICATED NEW REPAIR ANGLE WITH MATERIAL 2024-T3 .056C. TRSDR IPXA2024040825603Skin · crackedTHE R/H CENTER FLAP ASSY HAS 2EA CRACKS (TOTAL), AT RIB LOCATION 27 AFT. DEFECTS MARKED IN RED ON THE UPPER SURFACE. REVIEWED. REMOVED CRACKED FLANGE AND FABRICATED NEW REPAIR FLANGE WITH MATERIAL 2024-T3 .056C BATCH 0004237066 IN ACCOMPLISH WITH STEP 58 ON EASDR IPXA2024040825406Skin · crackedTHE R/H CENTER FLAP ASSY HAS 2EA CRACKS (TOTAL), AT RIB LOCATION 26 AFT. DEFECTS MARKED IN RED ON THE UPPER SURFACE. REVIEWED. ACCOMPLISH PERMANENT REPAIR PER EO-89700-REQ1 AND EA 300-5750-27-A3537.SDR IPXA2024040825155Skin · crackedTHE R/H CENTER FLAP ASSY HAS 1EA CRACK (TOTAL), AT RIB LOCATION 25 AFT. DEFECT MARKED IN RED ON THE UPPER SURFACE. REVIEWED. TREATED AND PRIMED NEW REPAIR DOUBLER IAW A300-600 SRM 51-21-10. NSTALLED NEW DOUBLER IN ACCOMPLISH WITH STED 69 ON EA 300-5750-27-A353SDR IPXA2024040824763Skin · crackedTHE R/H CENTER FLAP ASSY HAS 1EA CRACK (TOTAL), AT RIB LOCATION 18 AFT. DEFECT MARKED IN RED ON THE UPPER SURFACE. REVIEWED. REMOVED FLANGE CRACKED AND FABRICATED NEW REPAIR FLANGE WITH MATERIAL 2024-T3 .056C BATCH 0004237066. TREATED AND PRIMED IAW A300-600 SSDR IPXA2024040824243Skin · crackedTHE R/H CENTER FLAP ASSY HAS 1EA CRACK (TOTAL), AT RIB LOCATION 17 AFT. DEFECT MARKED IN RED ON THE UPPER SURFACE. REVIEWED. REMOVED FLANGE CRACKED AND FABRICATED NEW REPAIR FLANGE WITH MATERIAL 2024-T3 .056C BATCH 0004237066. TREATED AND PRIMED NEW REPAIR FLASDR IPXA2024040824047Skin · crackedHE R/H CENTER FLAP ASSY HAS 1EA CRACK (TOTAL), AT RIB LOCATION 13 AFT. ON THE UPPER SURFACE. ACCOMPLISH PERMANENT REPAIR PER EO-89700-REQ1 AND EA 300-5750-27-A3537 REV. -.SDR IPXA2024040823430Skin · crackedTHE R/H CENTER FLAP ASSY HAS 1EA CRACK (TOTAL), AT RIB LOCATION 11 AFT. DEFECT MARKED IN RED ON THE UPPER SURFACE. REVIEWED. FABRICATED NEW REPAIR FLANGE AND NEW REPAIR STIFFENER WITH MATERIAL 2024-T3 .050C BATCH 0004247654 IN ACCOMPLISH WITH STEP 6 ON EA 300-SDR IPXA2024040822772Skin · crackedTHE L/H CENTER FLAP ASSY HAS 2EA CRACKS (TOTAL), AT RIB LOCATION 26 AFT. DEFECTS MARKED IN RED ON THE UPPER SURFACE. REVIEWED. REMOVED CRACKED FLANGES AT CENTER FLAP RIB 26 BTW STR 2.7 TO REAR SPAR AND FABRICATED 02 EA NEW REPAIR ANGLES WITH MATERIAL 2024-T3 .SDR SWAA2024031557167Skin · delaminatedLH WING O/B TRAILING EDGE FLAP UPPER SURFACE DELAMINATED APPROXIMATELY 6.5' X 4.0' LOCATED AT 1.5' FROM I/B END AND 1.5' FROM TRAILING EDGE. T/E AFT FLAP (LH OTBD) (PN: 113A3700-25 SN: S1401-10)<[01] REMOVED L/H WING O/B AFT FLAP PER AMM 27-51-22.;[02] INSTALLSDR SWAA2024040356902Skin · delaminatedSKIN DELAMINATION ON L/H O/B AFT FLAP LOWER SURFACE 1.7' TO 3.0' FROM I/B END; 4.5' TO 11.0' FROM T/E.<[01] REMOVED AND REPLACED L/H O/B AFT FLAP IAW AMM 27-51-22-000-801 AND AMM 27-51-22-400-801SDR SWAA2024031556543Skin · delaminatedLH INBD MAIN FLAP OUTBD TRAILING EDGE WEDGE DELAMINATED ON LOWER SURFACE<[01] LOCATED AND DRILLED LH INBD MAIN FLAP OUTBD TRAILING EDGE WEDGE PER SRM 51-40-02;[02] 01 - REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-B00069 (GENERAL - FASTENER INSTALLATION AND REMSDR R61A2024031000106Fitting · crackedSUSPECTED CRACK IB AFT FLAP, IB SIDE EMITING FROM BOLT. REQUIRED NDT TO CONFIRM. FITTING (R/H IB AFT FLAP- IB SIDE) REPLACED IAW EMBRAER 170/175 AMM 20-10-01-910-801-A TABLE 201 AND 203 AND SRM 51-21-05.SDR FDEA202402260216Skin · delaminatedLEFT WING, OUTBOARD TRAILING EDGE FLAP AT NOSE SKIN (LEADING EDGE) BETWEEN OTEF STA 190 AND OTEF STA 265.69 WITH DELAMINATION. LEFT WING, OUTBOARD TRAILING EDGE FLAP AT NOSE SKIN (LEADING EDGE) BETWEEN OTEF STA 190 AND OTEF STA 265.69 WAS REPAIRED IAW B767SDR FDEA202402260215Skin · delaminatedLEFT WING, OUTBOARD TRAILING EDGE FLAP AT NOSE SKIN (LEADING EDGE) BETWEEN OTEF STA 3.75 AND OTEF STA 83.73 WITH DELAMINATION. LEFT WING, OUTBOARD TRAILING EDGE FLAP AT NOSE SKIN (LEADING EDGE) BETWEEN OTEF STA 3.75 AND OTEF STA 83.73 WAS REPAIRED IAW B767SDR SWIA202404250316Skin · buckledLEFT WING OUTBOARD FLAP LOWER SIDE SKIN APPROXIMATELY FLS209 BUCKLING , HN00140933 (C-CHECK RO 4/24/2024) LEFT WING OUTBOARD FLAP LOWER SIDE SKIN HAS BEEN REPAIRED REF CRJ 700 SRM 57-53-01-201-001-A01, TYPE 3, PERMANENT NON FLUSH REPAIR. REFER TO CONTISDR SWI202404250316Skin · buckledLEFT WING OUTBOARD FLAP LOWER SIDE SKIN APPROXIMATELY FLS209 BUCKLING , HN00140933 (C-CHECK RO 4/24/2024) LEFT WING OUTBOARD FLAP LOWER SIDE SKIN HAS BEEN REPAIRED REF CRJ 700 SRM 57-53-01-201-001-A01, TYPE 3, PERMANENT NON FLUSH REPAIR. REFER TO CONTISDR UIEA2024021500088Skin · delaminatedRH WING OUTBOARD FLAP LOWER SKIN EXISTING REPAIR WITH DELAMINATION (23 IN FROM L/E & 48 IN FROM LH EDGE)(<P>RH WING OUTBOARD FLAP LOWER SKIN PANEL WAS REPAIRED PER SRM 57-53-01-2R-1 & SRM 51-70-10-2R-4. NO FURTHER DEFECTS NOTED.</P>)SDR IXXA2024022202Skin · corrodedLEFT WING IB FLAP HAS CORROSION ON UPPER SURFACE.SDR SWIA2024032500221Skin · damagedRIGHT OUTBOARD FLAP HAS SMOKING RIVITS ON THE OUTTER SKIN (C-CHECK RO 3/23/2024) REMOVED AND REPLACED 10EA SMOKING FASTENERS ON RH OUTBOARD FLAP PER MHIRJ REO 670-57-53-347, REV: --, DATED 2024-02-24. ALL STEPS OF REO COMPLIED WITH IN THEIR ENTIRETY.SKYCASDR 2026FA0000337Stiffener · shearedFLAP TRACK STIFFENERS THAT KEEP THE FLAP TRACKS STRAIGHT AND TRUE WERE FOUND TO BE SHEARED OFF ON THE INBOARD LH FLAP TRACKSDR REXA2024102901114Access Panel · chafedRH FLAP L/E ACCESS PANEL 684GB IS CHAFED. FOUND DAMAGE ON PANEL BEYOND REPAIR. LOCATED AND DRILLED NEW SERVICABLE PANEL 684GB IAW CRJ-900 SRM 51-40-11-001-001-A01.
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