JASC 5753
Service difficulty reports · 31,515
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 SWIA200718680Structure · deformedFOUND DENT ON RT INBD FLAP BETWEEN FLAP STATION 64.00 AND 67.00, FOUND AT C-CHECK. INSTALLED INNER DOUBLER, FLUSH PLATE AND SUPPORT BRACKET IAW CRJ700 SRM 51-42-06-001-001-A01, CRJ700/900 SRM 57-52-01 PG 201-212 AND 51-42-13 PG 2 AND REO 670-51-52-009 SHEET SDR UPS07850345Doubler · puncturedINSPECTION TYPE:C2 LEFT WING INBOARD FLAP STA 110 UPPER SURFACE SKIN DENT AND EXISTING DOUBLER PUNCTURED. REMOVED DAMAGED DOUBLER ON LEFT WING INBOARD FLAP STA 110 UPPER SURFACE IAW SRM 51-01-21-0. FABRICATED AND INSTALLED REPAIR DOUBLER AT LEFT WING UPPER SSDR SWAA073554Skin · crackedDURING SCHEDULED BRDG CHECK, FOUND LEFT WING OUTBOARD MID FLAP CRACKED AT NR 2 CARRIAGE CUTOUT. REPAIRED FLAP PER SRM.SDR SWAA073531Skin · delaminatedDURING SCHEDULED A1 CHECK, FOUND LEFT WING OUTBOARD FORE FLAP T/E DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.SDR UIEA200700270Skin · crackedSMALL AREA OF CHAFING/CRACK AND DELAMINATION TO RT O/B FOREFLAP.SDR S9BA1407Arm · corrodedLEFT HAND I/B FORE FLAP O/B HINGE ARM CORRODED. REMOVED AND REPLACED FORE FLAPSDR 07FDEA02505Vane · delaminatedRIGHT WING OUTBOARD FLAP VANE UPPER SURFACE FOUND DELAMINATED. [07-30-07] COMPLIED WITH FEDEX E.A. 1-5750-112356. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR DU4R2007160Rib · crackedFOUND LT INBB FLAP MAIN FLAP RIB (3RD FROM I/B END) CRACKED. REPAIRED BY REMOVING RIB AND INSTALLING RIB FABRICATED (ON N/R 25000)16.780 BY 8.550 FROM 7050-T7457 IAW B757 SRM 51-40-02, BOEING DWG NR 113N2352 REV C, AND B757 SRM 51-20-01.SDR DHL2007804529Skin · misrepairedRT OUTBD FLAP T/E UPPER PANEL HAS A NON-STANDARD REPAIR AT STA XF 375.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW BOEING MSG NR 1-405802434-2 DATED 06-07-07. REMOVED PANEL PLATING WITH EXISTING NON-STANDARD REPAIR IAW SRM 57-1-0 PG 1, SRM 51-1-21. FABRICSDR 2007UALA02731Flap · damagedLEFT OUTBOARD MID TRAILING EDGE FLAP HAS A DEFLECTION IN ITS TRAILING EDGE OF 1 INCH OVER A LENGTH OF 38 INCHES. [08-14-07] EXISTING FLAP IS NOT DELAMINATED AND IS STRUCTURALLY SOUND. HOWEVER, REPLACED THE LT OUTBOARD FLAP PER MM-27-51-04. AIRCRAFT TEST FLSDR DHL2007753001Skin · delaminatedSMALL AREA OF DELAMINATION ON RT I/B MID FLAP T/E. CUT OUT DELAMINATED AREA ON RT I/B MID FLAP, APPROX 4 1/4" BY 5". FABBED FILLER APPROX 4 1/4" BY 5" AND DOUBLER APPROX 3" BY 4 1/4" FROM 7075-T6 .016" PO NR 9003988. CLEANED, PREPPED, PRIMED, BONDED, CLEANSDR DHL2007753500Structure · chafedRIGHT WING INBD FORE FLAP HAS O/B OF L/E DEEP CHAFE. REMOVED RT INBD FORE FLAP TO FOM IAW B727 MM 27-51-1. CUT OUT DAMAGED AREA I/B FORE FLAP R/WING. DIM CUT OUT 3/4" BY 3/4" AS REQUIRED IAW B727 SRM 57-50-4 FIG 1. FABBED DOUBLER REPAIR FROM P/N 2024-T3 .SDR 07FDEA02467Rib · crackedLEFT OB MID FLAP OB END RIB WEDGE CLIP AND SEAL RETAINER ANGLE ALL CRACKED AT AFT REAR CORNER OF FLAP. REMOVED LT, O/B MIDFLAP, REPLACED WITH SERVICABLE UNIT, REINSTALLED ON NON-ROUTINE #N00234.SDR AWXA200700876Skin · delaminatedMCN - MAJOR REPAIR - C-20 CHECK - NR 5961981, LEFT WING MID FLAP OUTBOARD END DELAMINATED, WS 184.275, INSIDE PANEL 722D. REPAIRED LEFT WING MID FLAP OUT BOARD END, WS 184.275, INSIDE PANEL 722D IAW B737-300 SRM 51-70-10-2R4.SDR UPS07M50815Hinge · corrodedINSPECTION TYPE:C LEFT O/B FLAP I/B HINGE (FLAP MOUNTED) PIVOT LUG I/B BORE & SPOT FACES FOUND CORROSION AS MARKED. CORROSION REMVD FROM AFFECTED AREAS & FOUND EXCEED LIMITS PER CMM57-52-0 4 PG 621-622 R58. ORG DIA 1.139" THK 0.497" FINAL DIA 1.189" THK 0.49SDR UPS07M50562Hinge · corrodedINSPECTION TYPE:C RT O/B FLAP I/B HINGE (WING MOUNTED) LOWER ATTACHMENT LUG I/B FOUND BORE AND SPOT FACES CORROSION AS MARKED. BORE AND SPOTFACE CORROSION REMOVED, EXCEED LIMIT CMM 57-44-08 PG 602-607 R58 ORG DIA 0.644" THK 0.460" FINAL DIA 0.707" THK 0.441" SDR UPS07M50561Hinge · corrodedINSPECTION TYPE:C RT O/B FLAP I/B HINGE (WING MOUNTED) LOWER ATTACHMENT LUG O/B FOUND BORE AND SPOT FACES CORROSION AS MARKED. BORE AND SPOTFACE CORROSION REMOVED, EXCEED LIMIT CMM 57-44-08 PG 602-607 R58. ORG DIA 0.644" THK 0.461" FINAL DIA 0.706" THK 0.435"SDR 07FDEA02789Skin · misrepairedPREVIOUS REPAIR LOCATED ON LT OUTBD FLAP, RIB 2/3 (UPPER SKIN). REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN SRM REPAIR. NEW REPAIR WASSDR 07FDEA02777Skin · misrepairedPREVIOUS REPAIR FOUND LOCATED ON INBD FLAP, RIB 2/4 (UPPER SKIN, TRALING EDGE). REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT CONFORM TO SRM. NEW REPAIR ACCOMPLISHED SDR SWAA073386Flap · delaminatedDURING SCHEDULED C3 CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REMOVED AND REPLACED FLAP PER MM.SDR DHL2007784511Skin · delaminatedRT INBD MID FLAP, OUTBD T/E DELAMINATED UPPER AND LOWER SURFACE, RWBL 239 TO 243.93. REMOVED DAMAGED AREA 3.5 BY 3.6, CLEANED AND PREPPED AREA TO BE REPAIRED IAW B727 SRM 51-40-20, PARA 7, FIG 3. FABRICATED FILLER 3.5 BY 3.6 AND DOUBLER 6.5 BY 5.1 FROM .012,SDR DHL2007784507Skin · crackedLT INBD AFT FLAP LE CRACKED AT NR 2 TRACK CUTOUT PREVIOUS DOUBLER, LWBL 60. REMOVED PREVIOUS REPAIR DOUBLER IAW B727 SRM 51-10-2, 51-30-2. HFEC IAW B727 NDTM PT.6 51-00-00, FIG.23, NO CRACKS INDICATED. FABRICATED REPAIR DOUBLER, MATERIAL USED 7075T6, 050, 3SDR DHL2007784502Skin · crackedLT INBD AFT FLAP LE CRACKED AT NR 3 TRACK CUTOUT, LWBL 112. STOP DRILLED CRACK AT LT INBD AFT FLAP AT NR 3 TRACK CUTOUT, LWBL 112 IAW B727 SRM 57-50-4, FIG 1. HFEC VERIFIED CRACK STOPPED IAW B727 NDTM 51-00-00 PT 6, FIG 23. FABRICATED REPAIR DOUBLER, MATERISDR AWXA200700850Wedge · debondedMCN - MAJOR REPAIR - C-20 CHECK - NR 5962306, RIGHT WING INBOARD MID FLAP TRAILING EDGE WEDGE LOWER SURFACE HAS AREA OF DISBOND, WS 161.5 - WS 167.5. REPAIRED RIGHT WING INBOARD MID FLAP TRAILING EDGE WEDGE LOWER SURFACE, WS 161.5 - WS 167.5 IAW B737-300 SRM SDR CALA0700348Flap Track · corrodedINSPECTION FOUND CORROSION INSIDE THE AFT TRANSMISSION MOUNT HOLE OF THE NR 8 FLAP TRACK, RT WING, WS 289-511. THE CORROSION IN THE BORE WAS REAMED, SHOT PEENED, PLATED AND A SLEEVE BUSHING WAS INSTALLED IAW CMM 57-53-15, PAGE 16, FIGURE 6 AND SOPM 20-42-10 ASDR QXEA200701186Flap Track · corrodedC4 PDX -LEFT WING NR 4 FLAP TRACK UPPER SURFACE OF OUTBOARD LOWER TRACK HAS PITTING AT FORWARD END. REPAIRED IAW RD8/4-57-988.SDR QXEA200701181Structure · damagedC4 PDX - LEFT NR4 FLAP, HAS TWO DIVOTS ON OUTBOARD CENTER SURFACE. REPAIRED IAW RD8/4-57-988.SDR QXEA200701180Flap Track · damagedC4 PDX - LEFT NR 4 FLAP TRACK, TOP SURFACE HAS TWO DIVOTS. REPAIRED IAW RD8/4-57-988.SDR SWAA073358Wedge · delaminatedDURING SCHEDULED 18Y CHECK, FOUND RIGHT WING INBOARD MID FLAP T/E WEDGE DELAMINATED AT OUTBOARD LOWER SURFACE. REPAIRED FLAP PER SRM.SDR SWAA073352Flap · delaminatedDURING SCHEDULED MV1 CHECK, FOUND RIGHT WING INBOARD FORE FLAP DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED FORE FLAP PER MM.SDR MWEA070154Structure · damagedLEFT WING FLAP TRAILING EDGE FIBER SHAPE IS DAMAGED. REMOVED AND REPLACED REPAIR SEGMENT.SDR QXEA200701179Flap Track · wornC4 PDX - LEFT INBOARD FLAP INBOARD LOWER TRACK HAS SEVERAL AREAS OF WEAR ON UPPER CONTACT SURFACE AT 4", 8", AND 20" AFT OF FORWARD END. REPAIRED IAW RD8/4-57-985.SDR QXEA200701178Flap Track · wornC4 PDX - LEFT INBOARD FLAP INBOARD UPPER TRACK HAS AREA OF WEAR ON LOWER CONTACT SURFACE AT 10" AFT OF FORWARD END. REPAIRED IAW RD8/4-57-985.SDR QXEA200701177Flap Track · wornC4 PDX - LEFT INBOARD FLAP OUTBOARD LOWER TRACK HAS SEVERAL AREAS OF WEAR ON UPPER CONTACT SURFACE AT 8" AND 20" AFT OF FORWARD END. REPAIRED IAW RD8/4-57-986.SDR QXEA200701136Doubler · chafedC4 PDX - LEFT OUTBOARD FLAP HAS CHAFE DAMAGE ON INBOARD UPPER SIDE ON THE DOUBLER. REPAIRED IAW RD8/4-57-1022.SDR IXXA07SMN193SPanel · deformedDURING ROUTINE C CHECK INSPECTION; FOUND RIGHT WING INBOARD FLAP LEADING EDGE UPPER PANEL DEFORMED BETWEEN STATION XW 123.000 AND STATION XW 136.000. REMOVED DAMAGED AREA. FABRICATED NEW SKIN AND DOUBLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. SDR ASAA0781862Skin · gougedRIGHT WING O/B FLAP I/B VANE GOUGED ON L/E 7 INCHES FROM I/B END. PREPARED DAMAGED AREA. FABRICATED DOUBLER AND INSTALLED IAW SRM 51-70-2 PG 59.SDR ASAA0781856Skin · gougedRIGHT WING O/B FLAP O/B VANE GOUGED ON UPPER SURFACE 68 INCHES FROM O/B END. PREPAIRED DAMAGED AREA, FABRICATED DOUBLER AND INSTALLED IAW SRM 51-70-2 PG 23 PARA 18B AND 51-70-2 FIG 12.SDR ASAA0781855Skin · gougedRIGHT WING O/B FLAP I/B VANE GOUGED ON LEADING EDGE 7 INCHES FROM I/B END. PREPAIRED DAMAGED AREA, FABRICATED DOUBLER AND INSTALLED IAW SRM 51-70-2 PG 59.SDR ASAA0781854Skin · dentedLT WING I/B FLAP I/B VANE DENTED ON LWR SURFACE NEXT TO PREVIOUS REPAIR EDGE. REMOVED EXISTING REPAIR, PREPAIRED SURFACE, FABRICATED DOUBLER AND INSTALLED IAW SRM 57-03 FIG 9A AND 51-70-2 FIG 12.SDR 07FDEA02371Skin · dentedRIGHT WING I/B FLAP LOWER SURFACE FOUND DENT. REPAIR CARRIED OUT AT RIGHT HAND WING I/B FLAP LOWER SURFACE AS PER SRM 57-10-00 FIGURE 38 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR CA070717017Nut · loose(CAN) ON APPROACH, CREW SELECTED FLAPS FROM 2 TO 5 AND HAD AN AMBER LIGHT INDICATION FOR THE NR 1 KRUGER FLAP INDICATING STILL RETRACTED. FELT MODERATE VIBRATION AND DECLARED AN EMERGENCY. UNEVENTFUL LANDING. MAINTENANCE CYCLED SYSTEM AND COULD NOT FAULT. FUSDR UPS07M50355Skin · canningINSPECTION TYPE:C LEFT I/B FLAP UPPER SURFACE FOUND OIL CANNING AT 4.75 INCHES FROM O/B END AND 33.75 INCHES FROM T/E AS MARKED. DAMAGES / AFFECTED AREA TRIM OUT SRM 57-10-00 FIG 34 VI R38. REWORKED AREA REPROTECTED SRM 51-21-01VII R38. HFEC INSP C/O NDTSPMSDR UPS07M50354Skin · dentedINSPECTION TYPE:C LEFT I/B FLAP LOWER SURFACE FOUND WITH SEVERAL SMALL DENTS AT 63 INCHES FROM O/B END AS MARKED. LEFT WING I/B FLAP LWR O/B SEGMENT LWR SKIN REMOVED PER SRM 51-35-01VII R38. NEW SKIN FAB PER BOEING DWG ARC2443, USE MATL 2024T3-0.040". HOLESSDR UPS07M50353Skin · dentedINSPECTION TYPE:C LEFT I/B FLAP LOWER SURFACE FOUND WITH SEVERAL DENTS AT 64 INCHES FROM I/B END AS MARKED. LEFT WING I/B FLAP LOWER I/B SEGMENT LOWER SKIN REMOVED SRM 51-35-01VII R38. NEW SKIN FAB BOEING DWG ARC2736, USE MATL 2024T3-0.040". HOLES PICK UP PSDR 07FDEA02355Flap · delaminatedRT WING, I/B FLAPS, AFT FLAP O/B END T/E IS DELAMINATED. REMOVED, REPAIRED, AND REINSTALLED RT WING I/B FLAP, AFT FLAP ASSY REF'S MM 27-51-002-4 AND SRM 51-40-20. THIS IS CLASSIFIED AS A MAJOR REPAIR. PLAY AND POSITION CHECK TO BE PERFORMED ON ROUTINE CARD SDR 07FDEA02357Wedge · debondedLT I/B MID FLAP AFT WEDGE HAS DISBONDED JUST O/B OF THE AFT FLAP TRACK. REMOVED LT I/B AFT FLAP REF M/M 27-51-001-4 REPAIRED MID FLAP REF SRM 51-40-21 PARA 4D AND 4E AND SRM 51-40-20 PARA 7, 14, 15, 18, 20, 21, 22 LT I/B AFT FLAP ASSY INSTALLED ON SNRM N00328.SDR 07FDEA02356Flap · delaminatedRT WING, I/B FLAPS, AFT FLAP O/B END T/E IS DELAMINATED. REMOVED, REPAIRED, AND REINSTALLED RT WING I/B FLAP, AFT FLAP ASSY REF'S MM 27-51-002-4 AND SRM 51-40-20 THIS IS CLASSIFIED AS A MAJOR REPAIR. PLAY AND POSITION CHECK TO BE PERFORMED ON ROUTINE CARD W/SDR IXXA07SMN173SVane · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING INTERIM HAD IMPROPER REPAIR AT OUTBOARD VANE SLOT XOLDO 067 AT STATION XFS 566.250. REMOVED EXISTING REPAIR. CUT DAMAGED AREA.PERFORMED NDT INSPECTION. NO CRACK OR CORROSION AFTER CUT. FABRICATED REPAIR PSDR WRNA200700055Rib · unserviceableDURING M96 COMPLY WITH S/B A300-57-0245, REPLACEMENT OF LT INBOARD FLAP RIB NR 7. REMOVED LEFT WING INBOARD FLAP, RIB NR 7, PERFORMED HFEC INSPECTION IAW A300-57-0245, NO DEFECTS NOTED. INSTALLED NEW NR 7 RIB P/N A5796005000400 IAW S/B A300-57-0245.
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