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 DALA2024013001345Flap Track · corrodedSHIP 3124 CORROSION ON FLAP BEARING TRACK 2 ON I/B FLAP L/H WING (1 E/A). CORRECTIVE ACTION: REPLACED FLAP BEARING TRACK #2 ON I/B FLAP L/H WING (1 E/A) PER A320 FAM AMM 57-52-21-000-001-A AND A320 FAM AMM 57-52-21-400-001-A. (0177748)SDR DALA2024013101406Rod End · excess playSHIP 3124 EXCESSIVE PLAY FLAP INTERCONNECTING STRUT ROD END BEARING ON LH WING (1 EA). CORRECTIVE ACTION: REPLACED INTERCONNECTING STRUT ON L/H WING AS PER A320 FAM AMM 27-51-44-000-001-A AND A320 FAM AMM 27-51-44-400-001-A. (0175848)SDR SWAA2024013045986Skin · delaminatedRT INBOARD MAIN FLAP DELAMINATED AFT EDGE O/B OF FLAP AT WEDGE ASSY LOWER SKIN. RT INBOARD MAIN FLAP DELAMINATED AFT EDGE O/B OF FLAP<[01] REMOVED R/H INB FLAP WEDGE PER SRM 51-40-02;[02] REMOVED AND REPLACED RT. INBOARD MAIN FLAP AFT WEDGE ASSY. PER. AMM REF.SDR SWAA2024013045987Skin · delaminatedLT INBOARD MAIN FLAP DELAMINATED AT AFT EDGE O/B OF FLAP LOWER SKIN OF TRAILING EDGE WEDGE ASSY... LT INBOARD MAIN FLAP DELAMINATED AT AFT EDGE O/B OF FLAP<[01] REMOVED THE LEFT MAIN FLAP TRAILING EDGE WEDGE;[02] REMOVED AND REPLACED LT INBOARD MAIN FLAP AFT WSDR FDEA202401280121Hinge Bracket · corrodedLEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING- WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM57-44-07.OVERSISDR FDEA202401280120Hinge Bracket · corrodedRIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING- WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM57-44- 07.OVSDR SWI2024F00274Fairing · chafedRH INBOARD FLAP HAS CHAFFING 2 AREAS WHERE CANOE FAIRING 683BB AND 686BB CONTACT LOWER SKIN (C-CHECK RO 4/3/2024) BLENDED-OUT DAMAGE AND EVALUATED LIMITATIONS ON RHS INBOARD FLAP LOWER SKIN AT FLAP-STA-74.718 AND FLAP STA-135.512, THE SUBJECT REWORKED CONDSDR SWI2024F00275Vane · chafedLH INBOARD FLAP VANE CHAFFED ON OUTBOARD LEADING EDGE (C-CHECK RO 4/3/2024) L/H I/B FLAP VANE, OUTBOARD LEADING EDGE CHAFFING BLENDED IAW CRJ 200 SRM 51-12-00 AND FOUND TO BE BEYOND LIMITS IAW CRJ 200 SRM 57-20-00 AND REO 601R-57-52-004 REV.-D, DATED 2012-SDR SWAA2024012945217Skin · delaminatedR/H OTBD AFT FLAP DELAMINATED INBD LOWER CORNER<[01] REPLACED R/H OUTBD AFT FLAP PER AMM 27-51-22. ADJUSTMENT/OPS CHECKS STILL REQUIRED.;[02] REPLACED R/H OUTBD AFT FLAP PER AMM 27-51-22. ADJUSTMENT/OPS CHECKS STILL REQUIRED.;[03] REPLACED R/H OUTBD AFT FLAP PSDR ASAA2024012648622Tab · crackedLH FLAP DEFLECTION BEAM UPPER TAB IS BROKEN OFF. GROUNDED - YES. REPAIRED DEFLECTION BEAM UPPER TAB IAW B737-900 SRM 57-51-02-2R-3.SDR AALA202403128644Bracket · wornAIRCRAFT IN BASE MAINTENANCE: RIGHT WING TRAILING EDGE INBOARD FLAP ATTACHMENT BRACKET FOR INTERCONNECTING STRUT BEARING HAS EXCESSIVE PLAY AT RIB 14. REPLACED BRACKET PER SRM 51-72-11.SDR VNAA202402290002Skin · nickedNICKS ON LOWER SKIN OF LH INBOARD FLAP FLS 15.00 TO FLS 65.5. NICKS ON LOWER SKIN OF LH INBOARD FLAP FLS 15.00 TO FLS 65.5 WERE BLENDED PER CRJ900 SRM 51-12-00-001-001-A01 AND WERE EVALUATED WITHIN LIMITS PER CRJ900 SRM 57-52-01-101-001-A01SDR VNAA202402290001Skin · dentedDENTS ON LOWER SKIN OF RH INBOARD FLAP FLS 15.00 TO FLS 65.5. DENTS ON LOWER SKIN OF RH INBOARD FLAP FLS 15.00 TO FLS 65.5 WERE MEASURED AND WERE EVALUATED WITHIN LIMITS PER CRJ-900 SRM 57-52-01-101-001-A01SDR AALA202402287874Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT WING INBOARD TRAILING EDGE FLAP INTERCONNECTING STRUT FITTING BEARING HAS EXCESSIVE PLAY. REPLACED FITTING PER SRM 51-42-11.SDR SWAA2024012945035Skin · crackedLH O/B AFT FLAP HAS DISBONDED AREA AND CRACKS ON LOWER SURFACE<[01] REMOVED AND REPLACED LH OUTBOARD AFT FLAP IN REFERENCE WITH AMM 27-51-26.;[02] RII C/W; REMOVED AND REPLACED LH OUTBOARD AFT FLAP IN REFERENCE WITH AMM 27-51-26.;[03] REMOVED AND REPLACED LH OSDR SWAA2024012945046Skin · delaminatedRH OUTBOARD TE FLAP ASSY DELAMINATING INBOARD TRAILING EDGE.<[01] REMOVED AND REPLACED RH OUTBOARD TE FLAP ASSY REF AMM 27-51-22. OPS AND RIG CHECK GOOD.;[02] REMOVED AND REPLACED RT OUTBOARD T/E; PERFORMED AFT FLAP ADJUSTMENT.<BR>REF: AMM 27-51-22. OPPS CHECKSDR SWAA2024012944807Skin · delaminatedLEFT WING OUTBOARD TRAILING EDGE FLAP DELAMINATED ON INBOARD EDGE.<[01] C/W EA 24-127-00235SDR FDEA202401260113Skin · dentedRH WING IB AFT FLAP UPR SURFACE FOUND DENT AT ITEF 340 AND 2.7 IN AWAY FROM AFT EDGE. EVALUATED RH WING IB AFT FLAP UPR SURFACE AT ITEF 340 AND 2.7 IN AWAY FROM AFT EDGE DENT WITH DISBOND DAMAGE SIZE LXW=5.1"X2.1" OUT OF ALLOWABLE LIMIT AS PER B777 SRM 57- SDR ASAA2024012549588Skin · dentedLEFT FLAP HAS MULTIPLE DENTS BEHIND MAIN WHEELS, MEASURE AND MAP ALL GROUNDED - YES. REPAIRED L/H I/B FLAP T/E WEDGE LOWER SURFACE IN ZONE 2 BY PREFORMING PERMAMENT CORE AND DOUBLER REPAIR IN 2EA AREAS. AREA 1 MEASURES 89.5" FROM I/B EDGE, REPAIR DOUBLER SIZESDR IPXA2024030237046Hinge Arm · corroded(APG) REPLACE R/H WING O/B FLAP I/B AFT HINGE DUE TO HEAVY CORROSION. REPLACED SERVICABLE R/H WING O/B FLAP I/B HINGE IN REF TO UPS MD11 CMM 57-52-04. INSTALLED LEADING EDGE UPPER AND LOWER COVER PANELS ON R/H O/B FLAP IN REF TO UPS MD11 CMM 57-52-04. REMOVE ASDR IPXA2024030236939Hinge · corroded(APG) REPLACE L/H WING O/B FLAP I/B AFT HINGE DUE TO HEAVY COORSION. REPLACED L/H WING O/B FLAP I/B AFT HINGE AND VERIFIED THE PLY WASHERS ARE NOT ROTATING IN REF TO UPS MD11 CMM 57-52-04. REINSTALLED LEADING EDGE UPPER AND LOWER COVER PANELS ON L/H O/B FLAP ISDR IPXA2024022936249Hinge · corroded(APG) REPL L/H WING O/B FLAP O/B FWD HINGE DUE TO HEAVY CORROSION. INST L/H WING O/B FLAP O/B FWD HINGE IN REF TO UPS MD11 AMM 57-53-01-400-801 TW ID: 22-1335 CAL DUE: 26-JUL-2024 TW ID: 19-1220 CAL DUE: 23-APR-2024. RE-INST 3EA BRACKETS & 1EA BELLCRANK & PUSHSDR IPXA2024022936554Hinge · corroded(APG) REPLACE L/H WING O/B FLAP I/B FWD HINGE DUE TO HEAVY CORROSION. INSTALLED L/H WING O/B FLAP I/B FWD HINGE IN REF TO UPS MD11 AMM 57-53-01-400-801 TW ID: 22-1335 CAL DUE: 26-JUL-2024 TW ID: 19-1220 CAL DUE: 23-APR-2024 TW ID: 16-88 CAL DUE: 16-MAY-2024. RSDR IPXA2024030635980Hinge · corrodedNEED TO REPLACE O/B FLAP O/B FWD HINGE DUE TO HEAVY CORROSION. REPLACED R/H WING O/B FLAP O/B FWD HINGE IN REF TO UPS MD11 AMM 57-53-01-400-801 TW ID: 19-411 CAL DUE: 14-FEB-2024 TW ID: 14-290 CAL DUE: 16-MAY-2024. REMOVE AND REPLACE HINGE BRACKET ASSEMBLY ARCSDR IPXA2024022336170Hinge · corrodedREPLACE R/H WING O/B FLAP I/B FWD HINGE DUE TOHEAVY CORROSION REMOVE AND REPLACE HINGE BRACKET ASSEMBLY ARC0502-508 PER MD11 AMM 57-53-01/401 REV 96. REINSTALLED HYD LINES AT R/H O/B FLAP I/B FWD HINGE AND PERFORMED HYD LEAK CHECK, NO LEAKS NOTED IN REF TO UPSSDR FDEA202401250110Skin · dentedRH WING OB FLAP LWR SURFACE FOUND DENT AT OTEF 234 AND 5.4 IN AWAY FROM AFT EDGE. EVALUATED RH WING OB FLAP LWR SURFACE DENT AT OTEF 234 AND 5.4 IN AWAY FROM AFT EDGE WITH DISBOND DAMAGE SIZE LXW=4.25"X2.5" OUT OF ALLOWABLE LIMIT AS PER B777 SRM 57-53-01SDR FDEA202401250109Skin · dentedLH WING OB FLAP LWR SURFACE FROM OB TO IB 233 INCHES CROSS TE TO LE 11 INCHES FOUND ONE DENT. EVALUATED LH WING OB FLAP LWR SURFACE FROM OB TO IB 233 INCHES CROSS TE TO LE 11 INCHES ONE DENT WITH DISBOND DAMAGE SIZE LXW=2.0"X1.0" OUT OF ALLOWABLE LIMIT ASSDR NACA2024012400002Skin · debondedRH WING O/B AFT FLAP DISBOND BETWEEN WBL.230.68 ~ WBL.234.68 .(L:4 INCH , W:0.3 INCH). PERFORMED CATEGORY A REPAIR OF A DISBOND AT THE EDGE OF ALUM HONEYCOMB STRUCTURE, RH WING O/B AFT FLAP BETWEEN WBL 230.68~WBL 234.68 I.A.W. B737-400 SRM 57-53-02-2R-2 & SRSDR IPXA2024012413312Fairing · puncturedL/H WING I/B FLAP, I/B AFT FLAP TRACK FAIRING O/B SIDE 30" FROM AFT END HAS 2"X2" DENT WITH 1/2" PUNCTURE. REMOVED DAMAGE AS NEEDED. FABRICATED NEW CORE PLUG AND INSTALLED WITH ADHESIVE PER SRM 57-20-35, CURED AS REQUIRED. REPAIRED PER SRM 57-20-35. CURE COMPSDR SWAA2024012944402Fairing · cracked#2 FLAP TRACK FAIRING HONEYCOMB CRACK<[01] FOUND L/H O/B FLAP I/B SUPPORT AFT FAIRING TAILCONE #2 HAS A HONEYCOMB CRACK L=4' W=.25' APROX 2.5' FROM BOTTOM CENTERLINE IN ZONE 2. OUT OF LIMITS PER SRM 57-53-70-1A-1. C/W EA 24-157-00208SDR DALA2024012501110Track · corrodedSHIP 3124 CORROSION ON FLAP BEARING TRACK 4 ON O/B FLAP R/H WING (1 E/A). CORRECTIVE ACTION: REMOVED AND INSTALLED NEW FLAP BEARING TRACK #4 ON O/B FLAP RH WING (1E/A) AS PER A320 FAM AMM 57-53-21-000-001-A AND AS PER A320 FAM AMM 57-53-21-400-001-A. (0169633)SDR SWAA2024012444279Skin · crackedLH O/B AFT FLAP HAS DISBONDED AREA AND CRACKS ON LOWER SURFACE. REFERENCE EA 24-157-00199 FOR PERMANENT REPAIR REQUIREMENTS.<[01] COMPLETED ON EA 24-157-00205.;[02] C/W INSP.;[03] C/W INSP.SDR IPXA2024030291807Hinge · corrodedSTR - R/H I/B FLAP O/B FWD HINGE #3 LUG BORE HAS CORROSION (114-60) COMPLETE SUBJECT REPAIR PER ATTACHED SUBTASK EO-89593-REQ1 (REF EA 011-5740-01-B0165 IR). BUSHING INSTALLED AND REPAIR ACCOMPLISHED ON EA#011-5740-B0165, AUDIT C/W. REVIEWED.SDR SWAA2024012943883Skin · crackedLEFT O/B AFT FLAP HAS CRACKS ON LOWER SURFACE<[01] C/W EA 24-157-00199; REPAIR REQUIRED WITHIN 5 FLIGHT CYCLES. OK TO CONTINUE ON TLD PER EA 24-157-00199. AIRCRAFT OK FOR SERVICESDR IPXA2024012493601Deflector · brokenRH WING CENTER FLAP OTBD END DEFLECTOR PLATE BROKEN REMOVED AND REPLACED DEFLECTOR PLATE ANGLE P/N A5796040221500 BATCH # 0004185041 IAW SRM 57-53-11 FIG 2.SDR IPXA2024041680192Skin · damaged*SUPPLEMENTAL SDR* DURING PDC .FOUND DAMAGE ON RT WING INBD AFT FLAP. INSTALLED SERVICEABLE RH WING INBD AFT FLAP IAW AMM 27-51€“06/201. OPS CHECK GOOD. THIS CLEARS DMI.SDR DALA2024012501157Skin · corrodedSHIP 6822 CORROSION ON LOWER INNER SKIN OF INBOARD FLAP (STA 173.43) AT LH WING. CORRECTIVE ACTION: SUMMARY OF NRC 00081 PERMANENT REPAIR ON LOWER INNER SKIN OF INBOARD FLAP (STA 173.43) AT LH WING WAS PERFORMED PER PRI NO .615248-14, REVISION 0 AND ER/A NO.61SDR FDEA202401220100Flap · delaminatedLH WING OUTBOARD FLAP BETWEEN INBOARD SIDE AND INBOARD FLAP TRACK AREA LEADING EDGE WITH DELAMINATE. LH WING OUTBOARD FLAP AT OTEF 345.75 WAS REPAIRED IAW B767 SRM 57-53-01-2R PAG 3-9 FIG 201 AND SRM 51-70-17-0G PAR 4.A PAG 24,25,48 FIG 10 REV 88 DEC 15/2SDR IPXA2024012380192Flap · damaged*SDR FILED OPEN* DURING PDC .FOUND DAMAGE ON RT WING INBD AFT FLAP. ASSIGNED EO-89280-REQ1 TO FAULT.SDR DALA2024012301014Lever · excess playSHIP 3124 EXCESSIVE PLAY ON BEARING OF ROTARY DRIVE ARM LEVER TRACK 2 ON R/H WING. CORRECTIVE ACTION: REPLACED BEARING (1 EA) ON ROTARY DRIVE ARM LEVER TRACK #2 ON RH WING PER AMDS CARD 2750-6020-RT. (0167049)SDR DALA2024012301013Lever · excess playSHIP 3124 EXCESSIVE PLAY ON BEARING OF ROTARY DRIVE ARM LEVER TRACK 3 ON L/H WING. CORRECTIVE ACTION: REPLACED BEARING (1 EA) ON ROTARY DRIVE ARM LEVER TRACK #3 ON LH WING AS PER AMDS CARD 2750-6020-LT. (0167042)SDR DALA2024012301012Lever · excess playSHIP 3124 EXCESSIVE PLAY ON BEARING OF ROTARY DRIVE ARM LEVER TRACK 2 ON L/H WING. CORRECTIVE ACTION: REPLACED BEARING (1 EA) ON ROTARY DRIVE ARM LEVER TRACK #2 ON LH WING AS PER AMDS CARD 2750-6020-LT. (0167036)SDR DALA2024012301011Lever · excess playSHIP 3124 EXCESSIVE PLAY ON BEARING OF ROTARY DRIVE ARM LEVER TRACK 4 ON R/H WING. CORRECTIVE ACTION: REPLACED BEARING (1 EA) ON ROTARY DRIVE ARM LEVER TRACK #4 ON RH WING AS PER AMDS CARD 2750-6020-RT. (0167030)SDR DALA2024012301010Lever · excess playSHIP 3124 EXCESSIVE PLAY ON BEARING OF ROTARY DRIVE ARM LEVER TRACK 1 ON L/H WING. CORRECTIVE ACTION: REPLACED BEARING (1 EA) ON ROTARY DRIVE ARM LEVER TRACK #1 ON LH WING AS PER AMDS CARD 2750-6020-LT. (0167026)SDR DALA2024012301015Lever · excess playSHIP 3124 EXCESSIVE PLAY ON BEARING OF ROTARY DRIVE ARM LEVER TRACK #3 ON R/H WING. CORRECTIVE ACTION: REPLACED BEARING (1 EA) ON ROTARY DRIVE ARM LEVER TRACK #3 ON RH WING AS PER AMDS CARD 2750-6020-RT. (0167017)SDR FDEA202401220099Hinge Bracket · corrodedLEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING- WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-07.OVERSIZESDR FDEA202401220098Hinge Bracket · corrodedRIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING- WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-07.OVERSIZED REPAIR BUSHING FABRICATSDR FDEA202401220097Hinge Bracket · corrodedLEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT LUG HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-52-03. OVERSIZED SDR FDEA202401220096Hinge Bracket · corrodedLEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-52-03. OVERSIZED SDR FDEA202401220095Hinge Bracket · corrodedRIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT LUG HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-52-03. OVERSIZE
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