JASC 5753
Service difficulty reports · 31,506
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 FDEA202408281184Skin · delaminatedLH WING, L/E OUTBD FLAP BETWEEN WS 543.00/ 597.00 WITH DELAMINATION LH WING, L/E OUTBD FLAP BETWEEN WS 543.00/ 597.00 WAS REPAIRED IAW B767 SRM 57-53-01-2R TABLE I AND 51-70-03-0G PAR 5.A FIG 5 REV 89 APR 15/2024SDR IPXA2024100975064Skin · damagedRH INBOARD FLAP - DAMAGE / EROSION ON OUTBOARD TRAILING EDGE (REPAIR). REMOVE DAMAGE AREA AND SURFACE MOISTURE AND CLEAN THE DAMAGED AREA I.A.W. 747-8F SRM 57-53-01-2R-1 REFER TO SRM 51-70-04-2R-1 PARAGRAPH 5.A.(1), (2) REV.43. REMOVE THE DAMAGE AND TAPER SANDSDR IPXA2024100974933Skin · damagedFAULT - ITEMS IDENTIFIED BY BUYER - LOWER SURFACES OF BOTH INBOARD FLAPS HAVE IMPACT DAMAGE (REPAIR). REMOVE DAMAGE AREA AND SURFACE MOISTURE AND CLEAN I.A.W. 747-8F SRM 57-53-01-2R-1 REFER TO SRM 51-70-05-2R-1 PARAGRAPH 5.A.(1), (2) REV.43. REMOVE THE DAMAGE SDR IPXA2024100974805Skin · damagedFAULT - ITEMS IDENTIFIED BY BUYER - LEFT INBD AFT FLAP - MULTIPLE IMPACT DAMAGES (REPAIR). REMOVE DAMAGE AREA AND SURFACE MOISTURE AND CLEAN THE DAMAGE AREA I.A.W. 747-8F SRM 57-53-01-2R-1 REFER TO SRM 51-70-05-2R-1 PARAGRAPH 5.A.(1), (2) REV.43. REMOVE THE DASDR IXXA20241002010Skin Panel · wornRH WING OTBD FLAP LOWER SURFACE SKIN IS WORN AT THE CONTACT POINT OF THE OTBD TRACK AFT FAIRING INBD BULB SEAL. HAECO WO 320008 NON ROUTINE 40490SDR SWAA2024092331396Wedge · delaminatedL/H WING I/B MAIN FLAP T/E WEDGE DELAMINATION OUT OF LIMITS<[01] REMOVED L/H WING I/B MAIN FLAP T/E WEDGE .;[02] LOCATED AND DRILLED L/H WING I/B MAIN FLAP T/E WEDGE PER SRM 51-40-02.;[03] LOCATED AND DRILLED L/H WING I/B MAIN FLAP T/E WEDGE PER SRM 51-40-02.ISDR UIEA2024083000876Structure · tornLHW #7 V/C FLAP LSA FOUND TORN.(<P><SPAN>PERFORMED REPAIR AT LSA TORN AREA IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.</SPAN></P>)SDR UIEA2024083000875Structure · tornLHW #8 V/C FLAP LSA FOUND TORN.(<P><SPAN>PERFORMED REPAIR AT LSA TORN AREA IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.</SPAN></P>)SDR UIEA2024083000874Structure · tornLHW #9 V/C FLAP LSA FOUND TORN.(<P><SPAN>PERFORMED REPAIR AT LSA TORN AREA IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.</SPAN></P>)SDR UIEA2024083000873Structure · tornRHW #18 V/C FLAP LSA FOUND TORN.(<P><SPAN>PERFORMED REPAIR AT LSA TORN AREA IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.</SPAN></P>)SDR UIEA2024083000872Structure · tornRHW #19 V/C FLAP LSA FOUND TORN.(<P><SPAN>PERFORMED REPAIR AT LSA TORN AREA IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.</SPAN></P>)SDR UIEA2024083000871Structure · tornRHW #20 V/C FLAP LSA FOUND TORN.(<P><SPAN>PERFORMED REPAIR AT LSA TORN AREA IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.</SPAN></P>)SDR UIEA2024083000870Structure · tornRHW #21 V/C FLAP LSA FOUND TORN.(<P><SPAN>PERFORMED REPAIR AT LSA TORN AREA IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.</SPAN></P>)SDR UIEA2024083000869Panel · damagedLHW I/B MAIN FLAP MOST O/B SEAL PAN PANEL SCREW HOLE FOUND ELONGATED.(<P><SPAN>PERFORMED PERMANENT REPAIR AS PER SRM 51-70-05 REPAIR 7. NO FURTHER DEFECTS NOTED.</SPAN></P>)SDR NACA2024082600001Spar · corrodedFOUND RH WING IB FWD FLAP REAR SPAR LOWER CHORD CORROSION AT 30 INCHES TO OB EDGE. REMOVED CORROSION, REWORKED AREA AND REPLACED DAMAGED PART IAW SRM 51-40-02SDR SWAA2024092330633Skin · delaminatedL/H OUTBOARD AFT FLAP INBOARD CORNER IS DELAMINATED.<[01] OK TO INSTALL REPLACEMENT O/B FLAP S/N 000176;[02] REMOVED AND REPLACED L/H O/B AFT FLAP PER AMM 27-51-22;[03] 02 - INSPECTED PER [AMM 27-51-22-401-NG (OUTBOARD AFT FLAP - REMOVAL/INSTALLATION - PERMANESDR CALA2024083000521Seal · missingPDA 2 RH OB FLAP IB CUSHION SEAL AND PLATE MISSING FROM AIRCRAFT UPON ARRIVAL. 55SQ IN. UPDATED SDR INFORMATION.SDR SWIA202412240825Skin · dentedLH WING OTBD FLAP HAS A DENT ON LOWER INBOARD EXTERNAL SKIN, MARKED (C-CHECK RO 12/21/2024) (FILED OPEN)L/H WING O/B FLAP, AFT I/B LWR SKIN HAS BEEN REPAIRED REF CRJ 700 SRM 57-53-01-201-001-A01, TYPE 3 REPAIR. COMPLIED FULLY W/SKYCARD 51-900-1002-SKY. SEE CONSDR SWAA2024082830219Skin · crackedDURING MV 1 CHECK FOUND DAMAGE TO RH AFT FLAP LOWER SKIN INBOARD SECTION 23 1/4 FROM I/B END AND 10.5 FROM TRAILING EDGE. DAMAGE IS .750 L X .750 W WITH SKIN CRACKS.<[01] COMPLIED WITH EA24-157-02331 TIME LIMITED REPAIR. RH AFT FLAP I/B TRAILING EDGE DAMAGE TOSDR CALA2024082802300Skin · damagedLEFT WING AFT OUTBOARD FLAP LOST A PART OF ITS FIBER TOP LAYER EXPOSING COMPOSITE INNER CORE. DAMAGE OUTSIDE OF ALLOWABLE LIMIT. REMOVED LT WING OUTBOARD AFT FLAP IAW AMM 27-51-22-000-801. C/W RII STEPS AND INSPECTED HARDWARE AND ATTACHED POINTS ON LEFT DIMSDR SWAA2024082630193Skin · delaminatedLH OB AFT FLAP PREVIOUS REPAIR DELAM<[01] REMOVED LH OB AFT FLAP IAW AMM 27-51-22;[02] OK TO INSTALL LH OB AFT FLAP.SN 000856.;[03] INSTALLED L/H AFT .OUTBOARD FLAP PER M/M 27-51-22;[04] REMOVED AND REPLACED L/H AFT. OUTBOARD FLAP PER M/M 27-51-22;[05] C/W RIISDR SWAA2024100729773Skin · debondedCUSTOMER REQUEST - DEBONDED IB MAIN FLAP TRAILING EDGE WEDGE PANEL LOWER SURFACE AT RT WING 2024-533342<[01] TOOL USED CALIPER PN: 500-197-30; SN: A18229508; DUE DATE: 14/JAN/25.;[02] THE REPLACE OF IB MAIN FLAP TRAILING EDGE WEDGE PANEL LOWER SURFACE AT RT WISDR SWAA2024100729774Skin · debondedCUSTOMER REQUEST - DEBONDED IB MAIN FLAP TRAILING EDGE WEDGE PANEL LOWER SKIN AT LT WING 2024-533345<[01] TOOL USED CALIPER PN: 500-197-30; SN: A18229508; DUE DATE: 14/JAN/25.;[02] THE REPLACE OF IB MAIN FLAP TRAILING EDGE WEDGE PANEL LOWER SURFACE AT RT WING SDR SWI2024F01214Fitting · damagedL/H I/B FLAP- I/B WING LUG FITTING- CENTER INBOARD LUG IS DAMAGED (ROLLED METAL) (C-CHECK RO 10/28/2024) (FILED CLOSED)EVALUATED AND REPAIRED DAMAGE ON LH INBD FLAP-INBD WING LUG FITTING-CENTER INBD LUG IAW CRJ700 SRM 57-21-27, 51-12-00. NDT PERFORMED BY BARONSDR SWI2024F01213Fitting · damagedL/H I/B FLAP- I/B WING LUG FITTING- CENTER OUTBOARD LUG IS DAMAGED-(ROLLED METAL) (C-CHECK RO 10/28/2024) (FILED CLOSED)REPAIRED DAMAGE ON LH IB FLAP, IB WING LUG FITTING, CENTER OTBD LUG IAW CRJ700 SRM 51-21-27, SRM 51-12-00, AND REO 670-57-21-993 REV-- DATE SDR SWI2024F01212Fitting · damagedR/H I/B FLAP- IB WING LUG FITTING- CENTER OUTBOARD FITTING IS DAMAGED (ROLLED OVER METAL ON EDGE) (C-CHECK RO 10/28/2024) (FILED CLOSED)PERFORMED REPAIR ON R/H IB FLAP IB WING LUG FITTING CENTER OB FITTING PER MHIRJ REO 670-57-21-992. REV.--. DATE: 2024-09-16SDR SWIA2024F01071Lug · damagedL/H I/B FLAP- I/B WING LUG FITTING- CENTER INBOARD LUG IS DAMAGED (ROLLED METAL) (C-CHECK RO 10/28/2024) (FILED OPEN)EVALUATED AND REPAIRED DAMAGE ON LH INBD FLAP-INBD WING LUG FITTING-CENTER INBD LUG IAW CRJ700 SRM 57-21-27, 51-12-00. NDT PERFORMED BY BARON NSDR SWIA20241029822Lug · damagedR/H I/B FLAP- IB WING LUG FITTING- CENTER OUTBOARD FITTING IS DAMAGED (ROLLED OVER METAL ON EDGE) (C-CHECK RO 10/28/2024) (FILED OPEN)PERFORMED REPAIR ON R/H IB FLAP IB WING LUG FITTING CENTER OB FITTING PER MHIRJ REO 670-57-21-992. REV.--. DATE: 2024-09-16 ASDR SWAA2024091128739Skin · debonded#4 AFT FLAP LOWER SKIN IS DISBONDED ON I/B SIDE.<[01] CORRECTED SUB-STEP 4;[02] REMOVED AND REPLACED R/H O/B AFT FLAP IAW AMM 27-51-22-400-801 AND AMM 27-51-22-000-801.;[03] VERIFIED CORRECTIVE ACTION 2SDR SWAA2024082629015Skin · delaminatedLEFT WING OB TE FLAP HAS DELAM ON TE APPR 16 FROM IB END<[01] REPLACED LEFT WING OUTBOARD AFT FLAP REF <BR>01 - REMOVED AND REPLACED PER [AMM 27-51-22-400-801-NG (OUTBOARD AFT FLAP INSTALLATION - PERMANENT)]SDR SWAA2024091328685Fairing · delaminatedL/H WING #3 CANOE HAS MULTIPLE AREAS OF LARGE DELAMINATIONS ON O/B SIDE<[01] REMOVED #3 TRAILING EDGE SUPPORT FAIRING 'CANOE' FROM AIRCRAFT INVENTORY AND REPLACED WITH NEW SERVICEABLE #3 TRAILING EDGE SUPPORT FAIRING. TRAILING EDGE SUPPORT FAIRING TO BE INSTALSDR SWAA2024091328682Skin · delaminatedL/H WING O/B AFT FLAP HAS AREA OF DELAMINATION ON LOWER I/B SURFACE<[01] REMOVED AND REPLACED L/H O/B AFT FLAP IAW AMM 27-51-21;[02] LINE #1 INSPECTED AS REQUIRED;[03] CORRECTIVE ACTION #1 SIGNED OFF USING INCORRECT REFERENCE. CORRECTIVE ACTION SHOULD READ; RESDR SWAA2024091328687Skin · delaminatedL/H WING I/B MAIN FLAP HAS LARGE AREA OF DELAMINATION ON FIXED TRAILING EDGE WEDGE.<[01] REMOVED TRAILING EDGE WEDGE F.O.M.;[02] DRILLED NEW WEDGE ASSY 113A2550-603 PER SRM 51-10-02.;[03] INSPECTED AS REQUIRED. CORRECTIVE ACTION #1 AND #2;[04] PAINTED EXTERIORSDR SWAA2024091228686Skin · delaminatedR/H WING O/B AFT FLAP HAS LARGE AREA OF DELAMINATION ON LOWER I/B SURFACE<[01] OK TO INSTALL O/B AFT FLAP.;[02] REMOVED AND REPLACED R/H OUTBD AFT FLAP PER AMM 27-51-22.;[03] INSPECTED WORK PERFORMED ON C/A #2.;[04] REMOVED AND REPLACED R/H OUTBD AFT FLAP PER SDR AALA202408235435Wedge · missingAIRCRAFT WAS GROUNDED: NOTICED MISSING FLAP REPAIR ON RIGHT HAND WING TRAILING EDGE FLAP. INSTALLED NEW WEDGE ASSEMBLY ON RIGHT HAND INBOARD. PER AMM 27-51-22.SDR IXXA20241003003Retainer · gougedL WING LFAP FAIRING 571AB SEAL RETAINER HAS EDGE DAMAGE. HAECO WO 320008 NON ROUTINE 40147SDR SWAA2024092428149Retainer · corrodedCORROSION RETAINER SEAL ANGLE OUTBOARD TRAILING EDGE AT LEVEL SPOILER 10 AT RT WING 2024-512511<[01] REPLACED RETAINER SEAL ANGLE OUTBOARD TRAILING EDGE AT LEVEL SPOILER 10 AT RT WING IAW B737-800 SRM 51-40-02 AND DWG: 115A3551; SHEET: 5; REV: -;[02] CERTIFIEDSDR SWAA2024092428369Retainer · corrodedCORROSION RETAINER SEAL ANGLE OUTBOARD TRAILING EDGE AT LEVEL SPOILER 3 LT WING 2024-512513<[01] REPLACED RETAINER SEAL ANGLE OUTBOARD TRAILING EDGE AT LEVEL SPOILER 3 LT WING I.A.W B737-800 SRM 51-40-02-0G-0 AND DWG# 115A3551; SHEET 5; REV.-.;[02] CERTIFIED CSDR YENA2024082601159Flap Track · wornDURING HEAVY MAINTENANCE: WEAR ON FLANGE FLAP TRACK #3 LOCATED ON LOWER INBOARD SIDE ON LH WING; REFERENCE AEROMAN W.O. 2024 131/1 NR 336716 - PERFORMED REWORK ON WEAR AREA AND EVALUATED DAMAGE LOC AT FLAP TRACK BEAM 3 ON LH WING AND FOUND WITHIN LIMITS IAW A3SDR YENA2024082601158Flap Track · wornDURING HEAVY MAINTENANCE: WEAR ON LOWER FLANGE FLAP TRACK #2 IB AND OB ON LH WING; REFERENCE AEROMAN W.O. 2024 131/1 NR 336753 - REWORKED AREAS AND EVALUATED DAMAGES LOCATED ON FLAP TRACK 2 BEAM LOWER AREA ON LH WING AND FOUND ALLOWABLE WITHIN LIMITS IAW A32SDR FDEA202408201154Skin · noneAIRCRAFT REPAIR ASSESSMENT : EXISTING DOUBLER REPAIR FOUND ON LH CENTER FLAP LOWER SKIN AT RIB20 ~ 21, TRAILING EDGE-14.5" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKSDR UIEA2024081500831Skin · dentedDENT AT RH WING FLAP LOWER SURFACE 58" FROM INBD END(<P>INSTALLED FABRICATED DOUBLER AT RH WING FLAP LOWER SURFACE 58" FROM INBD END AND 27" FROM LOWER T/E IAW SRM 51-70-10-2R-0. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024081500830Skin · dentedSEVERAL DENTS AT LH WING INBD MID FLAP LOWER SURFACE(<P>INSTALLED, FABRICATED DOUBLER ON LH WING MID FLAP IAW SRM 51-70-10-212-0 PAR 20B TABLE 208. NO FURTHER DEFECTS NOTED</P>)SDR SWAA2024082926891Fairing · delaminatedL/H WING #3 CANOE FAIRING; AFT CONE; OUTBOARD SIDE; HAS SEVERAL AREAS OF DELAMINATION INDICATED BY BULGING FACE SHEET.<[01] REMOVED AND REPLACED THE #3 CANOE FAIRING; AFT FAIRING ASSEMBLY PER AMM 27-51-18;[02] C/W INSPECTIONSDR IPXA2024082298500Roller · wornAGING A/C INSPECTION: FOUND NO.1 FLAP TRACK GENEVA CAM SUPPORT ROLLER WORN OUT 1EA. (REPLACE). REPLACED WORN CAM ROLLER. AMM 27-51-00.SDR IPXA2024082298753Roller · wornAGING A/C INSPECTION: FOUND NO.2 FLAP TRACK GENEVA CAM SUPPORT ROLLER WORN OUT 1EA. (REPLACE). REPLACED WORN CAM SUPPORT ROLLER PER AMM 27-51-00.SDR LR7A2024081603444Skin · damagedDURING SCHEDULED C-15 CHECK UNDER JOB CARD HC5712, FOUND RH OUTBOARD WING FLAP LOWER SKIN DAMAGED AT WOFS176-182R. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. NR# 1001134849. / PSE# 57-50-16, AD 2012-06-09SDR UIEA2024081600834Fairing · delaminatedLHW I/B MID FLAP I/B L/E FAIRING FOUND DELAMINATION(<P><SPAN>PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5A. NO FURTHER DEFECTS NOTED.</SPAN></P>)SDR FDEA202408161137Rib · crackedRH WING CENTER FLAP RIB UPPER FLANGE FOUND 1EA CRACK AT RIB5 BETWEEN STGR2.7 AND STGR2.8 COMPLIED WITH EA: 6-5750-T0380295 P1 REPAIRED THE RH WING CENTER FLAP CRACKED RIB UPR FLANGE AT RIB5 BETWEEN STGR2.7 AND STGR2.8. TITLE: WING - FLIGHT SURFACES - RH SDR FDEA202408161136Rib · crackedRH WING CENTER FLAP RIB UPPER FLANGE FOUND 1EA CRACK AT RIB17 BETWEEN REAR SPAR AND STGR2.8 COMPLIED WITH EA: 6-5750-T0380295 P1 REPAIRED THE RH WING CENTER FLAP CRACKED RIB UPR FLANGE AT RIB17 BETWEEN REAR SPAR AND STGR2.8. TITLE: WING - FLIGHT SURFACES
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