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 SWAA2024022749082Fairing · damagedLEFT WING #3 FLAP CANOE HAS FASTENER HOLES ELONGATED ON OUTBOARD SIDE<[01] APPLIED REPAIR TO DAMAGED FASTENER HOLES PER SRM 57-53-70-2R-2 ALTERNATIVE 2.;[02] KEVIN HOWE (TECHNICIAN); 14-FEB-2024 20:34 UTC<BR>APPLIED REPAIR TO DAMAGED FASTENER HOLES PER SRM 57-SDR SWAA2024022049542Fairing · delaminatedRIGHT WING # 7 FLAP TRACK AFT CANOE FAIRING IS DELAMINATED ON UPPER AFT SURFACE (MARKED)<[01] REMOVED DALAMINATED #7 FLAP TRACK AFT FAIRING AND INSTALLED NEW FAIRING PER AMM 27-51-28.;[02] REMOVED DALAMINATED #7 FLAP TRACK AFT FAIRING AND INSTALLED NEW FAIRINGSDR SWAA2024020948902Fairing · delaminatedR/H WING; #6 FLAP TRACK AFT FAIRING HAS A .25' HOLE PUNCTURED CAUSING A .75' AREA OF DELAMINATION ON THE LOWER OUTBOARD SIDE. (MARKED)<[01] R&R AFT FAIRING PER AMM 27-51-18.SDR EE4Y2023122819078Bearing · wornRIGHT WING TRAILING EDGE, DURING REMOVAL OF FLAP FAIRING #2 FOR ACCESS, IT WAS FOUND WITH EXCESSIVE MOVEMENT. NOTE: THE FLAP #2 MOVABLE FAIRING FWD HINGE POINT BEARING WAS REPLACED IN ACCORDANCE WITH ERJ-190 AMM TASK 57-58-23-000-801-A PARAGRAPH 1H(13) STEP (SDR SWIA20240514205Vane · chafedR/H I/B FLAP VANE EXISTING REPAIR IN MIDDLE CHAFFED (C-CHECK RO 5/13/2024) REPAIRED R/H I/B FLAP VANE SKIN IAW CRJ200 SRM 57-52-00,57-52-00 REPAIR #1,51-21-11,51-25-06 AND 51-25-16 AMM 27-54-10.CALIBRATED TOOLS USED: DEPTH GUAGE AV-7277 CAL DUE: AUG 2024,SDR DALA2024020901754Skin · dentedSHIP 1604 R/H WING I/B AFT FLAP FOUND DENT 9.5INCH FROM T/E 23INCH FROM I/B. DAMAGED AREA REPAIRED PER PER B767-300 SRM 57 -53-01-2R-1 & 51-70-10-2R-4 & SRM 51-70-10 (0187471)SDR UIEA2024012500024Skin · damagedLHW I/B FORE FLAP LWR SURFACE FOUND DAMAGED AS MARK (156" FROM O/B TO I/B).(<P>LHW I/B FORE FLAP LWR SURFACE 156" FROM O/B TO I/B DAMAGED AREA. PERFORMED HOT BOND REPAIR AS PER SRM 51-70-07 PAR 5.A.(1) AND FIG 5. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024012500025Skin · delaminatedL/H I/B FLAP MID FLAP MOST O/B LWR SURFACE FOUND DELAMINATION AS MARK (15" TO O/B EDGE).(<P>L/H I/B FLAP MID FLAP MOST O/B LOWER SURFACE (15" TO O/B EDGE) DELAMINATION AREA. PERFORMED HOT BOND REPAIR AS PER SRM 51-70-07 PAR 5.A.(1) AND FIG 5. NO FURTHER DEFECTSDR UIEA2024012500026Skin · delaminatedLHW T/E I/B AFT FLAP L/E 66" FOUND DELAMINATION AS MARKED (COUNT FROM O/B).(<P>LHW T/E I/B AFT FLAP L/E 66" (COUNT FROM O/B) DELAMINATION AREA. PERFORMED HOT BOND REPAIR AS PER SRM 51-70-07 PAR 5.A.(1) AND FIG 5. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024012500028Skin · dentedLHW I/B AFT FLAP LWR T/E SURFACE AT MID AREA FOUND 1EA DENT AS MARK (155" FROM I/B TO O/B).(<P>LHW I/B AFT FLAP LWR T/E SURFACE 155" FROM I/B DENT AREA. PERFORMED HOT BOND REPAIR AS PER SRM 51-70-07 PAR 5.A.(1) AND FIG 5. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024012500029Skin · puncturedL/H I/B FLAP AFT FLAP T/E UPPER SURFACE FOUND 1EA PUNCH DAMAGED AS MARK.(<P>LH I/B FLAP AFT FLAP T/E UPPER SURFACE PUNCH DAMAGED AREA. PERFORMED HOT BOND REPAIR AS PER SRM 51-70-07 PAR 5.A.(1) AND FIG 5. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024012500030Skin · dentedLHW I/B AFT FLAP O/B LWR SURFACE FOUND 1EA DENT AS MARK (146" FROM I/B TO O/B).(<P>LHW I/B AFT FLAP O/B LWR SURFACE (146" FROM I/B TO O/B) DENT AREA. PERFORMED HOT BOND REPAIR AS PER SRM 51-70-07 PAR 5.A.(1) AND FIG 5. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024012500031Skin · delaminatedLHW T/E I/B AFT FLAP LOWER SURFACE T/E 130" FOUND DELAMINATION AS MARK. (COUNT FROM I/B TO O/B)(<P>LHW T/E I/B AFT FLAP LOWER SURFACE T/E 130" (COUNT FROM I/B TO O/B) DELAMINATION AREA. PERFORMED HOT BOND REPAIR AS PER SRM 51-70-07 PAR 5.A.(1) AND FIGURE 5. NOSDR UIEA2024012500032Skin · delaminatedLHW T/E I/B FLAP FLAP LOWER SURFACE L/E 47" (COUNT FROM I/B) FOUND DELAMINATION AS MARKED.(<P>LHW T/E I/B AFT FLAP LOWER SURFACE L/E 47" (COUNT FROM I/B) DELAMINATION AREA. PERFORMED HOT BOND REPAIR AS PER SRM 51-70-07 PAR 5.A.(1) AND FIG 5. NO FURTHER DEFECTSSDR UIEA2024012500033Panel · delaminatedL/H O/B FLAP MID FLAP O/B CARRIAGE ASSY COVER PANEL FOUND DELAMINATION AS MARK.(<P>L/H O/B FLAP MID O/B CARRIAGE ASSY COVER PANEL DELAMINATION AREA. PERFORMED HOT BOND REPAIR AS PER SRM 51-70-07 PAR 5.A.(1) AND FIG 5. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024012500034Skin · delaminatedRHW T/E I/B AFT FLAP LOWER SURFACE T/E 100" FOUND DELAMINATION AS MARKED (COUNT FROM I/B).(<P>RHW T/E I/B AFT FLAP LOWER SURFACE T/E 100" (COUNT FROM I/B) DELAMINATION AREA. PERFORMED REPAIR AS PER SRM 51-70-07 PAR 5.A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024012500035Skin · delaminatedRHW T/E I/B AFT FLAP LOWER SURFACE T/E 122" FOUND DELAMINATION AS MARKED (COUNT FROM I/B).(<P>RHW T/E I/B AFT FLAP LOWER SURFACE T/E 122" (COUNT FROM I/B) DELAMINATION AREA. PERFORMED REPAIR AS PER SRM 51-70-07 PAR 5.A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024012500036Skin · delaminatedRHW T/E I/B MID FLAP LOWER SURFACE L/E 124" FOUND DELAMINATION AS MARKED (COUNT FROM TO I/B).(<P>RHW T/E I/B MID FLAP LOWER SURFACE L/E 124" (COUNT FROM TO I/B) DELAMINATION AREA. PERFORMED REPAIR AS PER SRM 51-70-07 PAR 5.A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024012500038Skin · delaminatedRHW T/E I/B AFT FLAP LOWER SURFACE T/E 48" FOUND DELAMINATION AS MARKED (COUNT FROM I/B).(<P>RHW T/E I/B AFT FLAP LOWER SURFACE T/E 48" (COUNT FROM I/B) DELAMINATION AREA. PERFORMED REPAIR AS PER SRM 51-70-07 PAR 5.A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024012500039Skin · delaminatedRHW T/E I/B MID FLAP L/E 2" (COUNT FROM I/B) FOUND DELAMINATION AS MARK.(<P>RHW T/E I/B MID FLAP L/E 2" (COUNT FROM I/B) DELAMINATION AREA PERFORMED REPAIR AS PER SRM 51-70-07 PAR 5.A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024012500040Panel · delaminatedR/H I/B T/E FLAP MID FLAP O/B CARRIAGE ASSY UPPER COVER APNEL FOUND DELAMINATION AS MARK.(<P>R/H I/B T/E FLAP MID FLAP O/B CARRIAGE ASSY UPPER COVER PANEL DELAMINATION AREA. PERFORMED REPAIR AS PER SRM 51-70-07 PAR 5.A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024012500041Skin · delaminatedRHW T/E I/B AFT FLAP LOWER SURFACE T/E 155" FOUND DELAMINATION AS MARKED (COUNT FROM I/B).(<P>RHW T/E I/B AFT FLAP LOWER SURFACE T/E 155" (COUNT FROM I/B) DELAMINATION AREA. PERFORMED REPAIR AS PER SRM 51-70-07 PAR 5.A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024012500042Fairing · delaminatedRHW O/B FWD FLAP FWD FAIRING 48" FOUND DELAMINATION AS MARKED (COUNT FROM O/B).(<P>RHW O/B FWD FLAP FWD FAIRING 48" (COUNT FROM O/B) DELAMINATION AREA. PERFORMED REPAIR AS PER SRM 51-70-07 PAR 5.A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024012900052Skin · corrodedLHW I/B AFT FLAP FOUNDÂ BULGE UP(<P>PERFORMED REPAIR AT BULGE UP AREA IAW RI-57-53-16705. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024013000053Skin · dentedLHW O/B T/E AFT FLAP O/B PANEL UPPER SURFACE FOUND SEVERAL AREA DENT MARK AS MARKED.(<P>METAL HOT BOND REPAIR CARRIED OUT AS PER RI-57-51-16699 REV.A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024013000054Skin · dentedRHW O/B T/E AFT FLAP O/B PANEL UPPER SURFACE FOUND SEVERAL AREA DENT MARK AS MARKED.(<P>METAL HOT BOND REPAIR CARRIED OUT AS PER RI-57-51-16700 REV.A. NO FURTHER DEFECTS NOTED.</P>)SDR DALA2024020601607Nut · corrodedSHIP 3124 CORROSION ON NUT OF FLAP CARRIAGE BOLT OF TRACK #4 O/B FLAP (1 E/A) L/H WING. CORRECTIVE ACTION: REPLACED NUT OF FLAP CARRIAGE BOLT OF TRACK #4 (1 E/A) L/H WING INSTALLATION IS TO BE ACCOMPLISHED AS PER AMDS CARD 2750-6020-LT. (0188571)SDR SWAA2024022655345Skin · delaminatedLEFT OUTBOARD AFT FLAP INBOARD SIDE UPPER AND LOWER SURFACE DELAMINATED.<[01] REMOVED AND REPLACED LEFT OUTBOARD AFT FLAP REF AMM 27-51-11. REQUIRES OPS CHECK.;[02] REMOVED AND REPLACED LEFT OB AFT FLAP REF AMM 27-51-22-400-801; THRU STEP F.(5)(G). OB AFT FLAPSDR DALA2024020601603Bushing · corrodedSHIP 3124 CORROSION ON BUSHING OF O/B FLAP DRIVE ARM O/B POSITION AFT SIDE 2E/A ON LH WING. CORRECTIVE ACTION: REPLACED BUSHINGS (2EA) ON O/B FLAP DRIVE ARM O/B SIDE AFT POSITION LH WING AS PER AIRBUS CMM 57-53-21, A319 SRM 51-21-00-801 AND A319 SRM 51-74-00-8SDR DALA2024020601602Bushing · corrodedSHIP 3124 CORROSION ON BUSHING OF O/B FLAP DRIVE ARM I/B POSITION AFT SIDE 2E/A ON LH WING. CORRECTIVE ACTION: REPLACED BUSHINGS (2E/A) OF O/B FLAP DRIVE ARM I/B POSITION AFT SIDE L/H PER AIRBUS CMM 57-53-21. (0185487)SDR DALA2024020501535Link · corrodedSHIP 3313 CORROSION ON FLAP TRACK 2 REAR LINK ON LOWER POSITION ON LH WING. CORRECTIVE ACTION: REMOVED AND REPLACED LOWER BEARING ON FLAP TRACK LINK #2 ON L/H WING AS PER A330 CMM 57-51-36-000-801-A01 AND CMM 57-51-36-400-801-A01. (0185853)SDR FDEA202402030134Skin · dentedLEFT INBOARD FLAP, AFT FLAP, LOWER SURFACE, BTW FLAP TRACK FAIRINGS, DENTS. LEFT INBOARD FLAP, AFT FLAP, LOWER SURFACE, BTW FLAP TRACK FAIRINGS WAS REPAIRED IAW B767 SRM 57-53-01-2R REP 1 AND SRM 51-70-03-0G PAR 5.L FIG 16 PAG 27,52 REV 88 DEC 15/2023SDR ASAA2024020247752Skin · dentedL/H INBD. FLAP LOWER TRAILING EDGE WEDGE, MIDDLE CLUSTER REQUIRES REPAIR. GROUNDED - YES. REMOVED 9.4" X 10.5" DAMAGED LH INBD FLAP LWR SKIN & CORE 83" FROM INBD EDGE / 5.5" FROM TE IDENTIFIED AS MIDDLE CLUSTER & REPAIRED IAW A320-200 SRM 57-52-00-300-093 REV.SDR DALA2024020201490Trunnion · out of limitsSHIP 3271 DISC: REWORK WAS FOUND OUT OF LIMITS ON UPPER STRUCTURE FLAP TRUNNION INBOARD FLAP ON LH WING MEASURE OF MAXIMUN DEPTH 0.298IN AND TRUNNION SHAFT DIAMETER 3.086IN CONTAC LIAISON ENGINEERING. ADDITIONAL ENGINEERING D OCUMENTATION IS REQUIRED PRIOR TO SDR REXA2024102901158Vane · chafed"R/H I/B FLAP VANE IS CHAFED ON THE LEADING EDGE APPROX 8 INCHES FROM O/B EDGE. BLENDED DAMAGE IAW CRJ900 SRM 57-52-01-101-001-A01 TABLE 1 AND CRJ900 SRM 51-12-00-001-001-A01 PARAGRAPH 7, EVALUATED AND FOUND TO BE OUT OF LIMITS IAW CRJ-900 SRM 57-52-01-101-001SDR SWIA20240201Skin · dentedDENT NOTED AT R/H INBD FLAP EXTERNAL LOWER SKIN AT APPROX. 2" FROM T/E AND 5" FROM INBD EDGE (MARKED) (C-CHECK RO 4/3/2024) R/H I/B FLAP EXTERNAL LOWER SKIN DENT HAS BEEN REPAIRED REF CRJ 200 SRM 57-52-00. SEE CONTINUATION SHEET FOR DETAILS. COMPLIED FULLSDR SWIA20240619201Rivet · looseTWO AREAS OF SMOKING RIVETS ON LH OB FLAP UPPER SURFACE, APPRX 30 FASTNERS.( MARKED) (C-CHECK RO 3/19/2024) REPLACED NOTED SMOKING RIVETS ON LH OB FLAP UPPER SURFACE, APPROX. 30 FASTENERS REF MHIRJ REO--601R-57-53-1290 REV -- DATE 2024-02-03.COMPLIED WITH SDR SWAA2024022047056Skin · delaminatedRH OB AFT FLAP IB LOWER CORNER; UPPER SURFACE HAS AREA OF DELAMINATION.<[01] REMOVED RT OUTBOARD AFT FLAP PER 27-51-22;[02] OK TO INSTALL NEW FLAP S/N 00789;[03] INSTALLED RH OB AFT FLAP PER AMM 27-51-22;[04] RII INSPECTED AS REQUIRED. CORRECTIVE ACTION #3.;[0SDR SWAA2024020546763Skin · delaminatedRIGHT WING O/B AFT FLAP I/B TE DELAMINATED 14 BY 9 INCH. REMEASURE RIGHT WING O/B AFT FLAP FOUND FLAP DELAMINATED 20.6BY 9.5 INCH.<[01] R AND R RIGHT WING O/B AFT FLAP PER AMM 27-51-22.SDR DALA2024020101438Nut · corrodedSHIP 3124 CORROSION ON NUT OF FLAP CARRIAGE BOLT OF TRACK 3 (1 E/A) L/H WING. CORRECTIVE ACTION: REPLACED NUT OF FLAP CARRIAGE BOLT OF TRACK #3 (1 E/A) L/H WING PER AMDS CARD 2750-6020-LT. (0180548)SDR DALA2024020101437Bearing · excess playSHIP 3124 EXCESSIVE PLAY ON O/B FLAP BEARING O/B SIDE LH WING. CORRECTIVE ACTION: REPLACED BEARING TRACK #4 ON O/B FLAP L/H WING (1 E/A) AS PER A320 FAM AMM 57-53-21-000-001-A AND AMM 57-53-21-400-001-A. (0180541)SDR DALA2024020101436Bearing · excess playSHIP 3124 EXCESSIVE PLAY ON O/B FLAP BEARING I/B SIDE LH WING. CORRECTIVE ACTION: REPLACED FLAP BEARING LOC. AT TRACK #3 ON O/B FLAP L/H WING AS PER A320 FAM AMM 57-53-21-000-001-A AND AMM 57-53-21-400-001-A. (0180521)SDR ASAA2024013048790Skin · delaminatedLESSOR ITEM 799: (77751) RH WING TRAILING EDGE, FLAP TRACK #3 AREA, BROKEN FILLER COMPOUND AND EVIDENCE OF WATER INGRESS, ABRASION RESISTANT PAINT BROKEN AND MISSING GROUNDED - YES. REPAIRED R/H WING TRAILING EDGE FLAP TRACK #3 AREA WITH CAT. A PERMANENT REPAISDR ASAA2024013048786Skin · delaminatedLH WING TRAILING EDGE, FLAP TRACK #3 AREA, BROKEN FILLER COMPOUND AND EVIDENCE OF WATER INGRESS, ABRASION RESISTANT PAINT BROKEN AND MISSING GROUNDED - YES. EVALUATED LESSOR ITEM 800. LH WING TRAILING EDGE, FLAP TRACK #3 AREA, P/N D5757420200600, NSN(SN) DAMAGSDR AALA202402268175Strut · corrodedAIRCRAFT WAS IN BASE MAINTENANCE: L/H WING INTERCONNECT STRUT DAS CORROSION. RECEIVED SERVICEABLE COMPONENT INSTALLED.SDR AALA202402263332Strut · corrodedAIRCRAFT WAS IN BASE MAINTENANCE: R/H WING INTERCONNECT STRUT HAS CORROSION. EVALUATED CORROSION AND FOUND OUT OF LIMITS NO SRM REFERENCE PART REPLACED.SDR SWAA2024022046649Skin · delaminatedR/H O/B AFT FLAP REQUIRES REPLACEMENT DUE TO DELAMINATION ON I/B LOWER CORNER (MARKED )<[01] OK TO INSTALL R/H OB FLAP.;[02] REMOVAL AND REPLACEMENT OF R/H OUTBOARD AFT FLAP PARTS IS ACCOMPLISHED ON TTG8Q00R7YCX;[03] VERIFIED R/H OUTBOARD AFT FLAP PARTS IS ACCSDR DALA2024020901766Bearing · excess playSHIP 3124 EXCESSIVE PLAY ON FLAP BEARING LOC. AT TRACK 3 ON O/B FLAP R/H WING (1 E/A). CORRECTIVE ACTION: REPLACED FLAP BEARING LOC. AT TRACK #3 ON O/B FLAP R/H WING (1 E /A) FOR REMOVE AS PER A320 FAM AMM 57-53-21-000-001-A. (0179408).SDR ASAA2024012948783Skin · delaminatedGENERATED FROM CUSTOMER CARD # G1871683 LESSOR 731, DB#10 ; LEFT WING INBOARD FLAP LOWER SKIN, OB CLUSTER OF DENTS REQUIRES REPAIR GROUNDED - YES. REPAIRED LEFT WING INBOARD FLAP LOWER SKIN OUTBOARD CLUSTER OF DENTS LOCATED 84" FROM INBOARD TO OUTBOARD AND STSDR SWAA2024022046148Skin · delaminatedRIGHT WING OUTBOARD TRAILING EDGE AFT FLAP DELAMINATED; INBOARD UPPER SURFACE.<[01] PARTS UPDATE;[02] REMOVAL AND REPLACEMENT TO BE ACCOMPLISHED ON NON-ROUTINE CARD # TTG8Q00R8PNW;[03] VERIFIED REMOVAL AND REPLACEMENT TO BE ACCOMPLISHED ON NON-ROUTINE CARD # T
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