JASC 5753
Service difficulty reports · 31,521
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 DU4R0507141Skin · dentedRIGHT WING INBOARD FORE FLAP LOWER SKIN SURFACE HAS NUMEROUS DENTS.SDR 138Skin · gougedRT WING OB FORE FLAP GOUGED ON OB END. S/O 269008, OPS NR 24931.SDR DU4R0507001Skin · dentedLT WING IB FWD FLAP LWR SIDE HAS 8 DENTS AT STA. WBL 85 TO 95 AT VARIOUS LOCATIONS.SDR IXXA05SMN133SAngle · crackedDURING ROUTINE C CHECK INSPECTION, RT IB FLAP INTERNAL ANGLE CRACKED 3 INCH, STA XW 129.000. REMOVED CRACKED ANGLE IAW SRM 51-1-21. FABRICATED NEW ANGLE (A EXTRUSION S-1656396) IAW SRM 57-2-0 PAGE 1. CLEANED, TREATED AND PRIMED AREA + NEW ANGLE IAW SRM 51-SDR AWXA200500798Bolt · corrodedMCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED GALVANIC CORROSION ON 4 BOLTS LOCATED AT THE LT INBOARD MID FLAP OUTBOARD CARRIAGE. THERE ARE NO LIMITS ON CORRODED BOLTS. MAINTENANCE REMOVED AND REPLACED THE 4 BOLTS FOR THE LT INBOARD MID FLAP, OUTBOARD CARSDR 05FDEA01735Hinge · corrodedLT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) AFT HINGE FITTING FORWARD BOLT HOLE FOUND CORRODED. REMOVED AND REPLACED PER AMM 27-50-30-4.SDR 05FDEA01734Hinge · corrodedLT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) FORWARD HINGE FITTING INBOARD MID BOLT HOLE FOUND CORRODED. REMOVED AND REPLACED PER AMM 27-50-30-4.SDR 05FDEA01733Hinge · corrodedLT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) AFT HINGE FITTING AFT BOLT HOLE FOUND CORRODED. REMOVED AND REPLACED PER AMM 27-50-30-4.SDR 05FDEA01731Hinge · corrodedDURING ACCOMPLISHMENT OF EA 1-5750-87541. LT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) OUTBOARD MID BOLT HOLE FOUND CORRODED. REMOVED AND REPLACED PER AMM 27-50-30-4. (CLOSED)SDR 05FDEA01719Hinge Fitting · crackedAFT FLAP RT INBD AT HINGE FITTING 111.0 FROM INBD, LE LWR SKIN CRACKED (.450 LONG) REPLACED FLAP ON W/C 76C071-00SDR 05FDEA01712Hinge · corrodedLT WING, OUTBOARD FLAP INBOARD HINGE AFT HINGE FITTING AFT HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-87551.SDR 05FDEA01711Hinge · corrodedRT WING, OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) FORWARD HINGE. COMPLIED WITH FEDEX EA 1-5750-87546.SDR 05FDEA01710Hinge Fitting · corrodedRT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) AFT HINGE FITTING FORWARD STRUT HOLE FOUND CORRODED STRUT. COMPLIED WITH FEDEX EA 1-5750-87545. (CLOSED)SDR IXXA05SMN116SFlap · improperDURING ROUTINE C CHECK INSPECTION, LT OB FLAP L/E REPAIR IMPROPER, XF 333.000 (UPPER PART) PERFORMED MAJOR REPAIR IAW NR 05259 DATE 06-24-05, DWG NR ED 3988, EO NR 2005855 DATE 06-24-05. REMOVED FASTENERS IAW SRM. REMOVED DAMAGED PLATING SEGMENT IAW DWG ED 39SDR DHL2005802502Skin · crackedRT OUTBD FLAP UPPER SKIN CRACKED 0.500 APPROX. AT STA XF 304.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG.1, SRM 57-7-1 FIG. 4, TR 57-94. REMOVED CRACKED PLATING IAW SRM 51-1-21 PG.1. FABRICATED NEW PLATING IAW SRM 57-7-1 FIG. 4, TR 57-94 ITESDR DHL2005802501Skin · damagedRT INBD FLAP UPPER EXTERNAL SKIN INTERIM REPAIR, STA XW 104.000-110.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG.1, SRM 57-7-1 FIG. 1. REMOVED PLATING WITH EXISTING INTERIM REPAIR IAW SRM 51-1-21 PG.1. FABRICATED NEW PLATING (AL2024Y3 0.040) ISDR USAA050801Skin · gougedCLT - Q5 - FLAP SKIN, .500 X 3 INCH GOUGE, I/H OB MID FLAP BOTTOM SKIN 53 INCHES FROM IB END. REPAIRED DAMAGED SKIN IAW SRM. (K)SDR USAA050800Skin · wornMID FLAP SKIN, .500 WIDE X 4 INCHES LONG, WORN AREA, LT OB MID FLAP BOTTOM SIDE 68 INCH FROM IB END. REMOVED DAMAGE AND INSTALLED NEW TRIPLER DOUBLER IAW SRM. (K)SDR SWAA051883Bolt · brokenBROKEN BOLT AND MISSING FLAP TRACK ROLLER FOUND AT LT WING OUTBOARD T/E FLAP, OUTBOARD ROLLER. INSTALLED BOLT & ROLLER PER MM.SDR SWAA051881Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REPAIRED FLAP PER SRM.SDR ASAA0540321Wedge · dentedOKC - FOUND LEFT INBOARD MID FLAP T/E WEDGE HAS TWO EACH SHARP DENTS. REMOVED DAMAGE, FABRICATED SKIN AND DOUBLER AND INSTALLED REPAIR PIECES IAW 737-400 SRM 51-70-10. (M)SDR ASAA0540308Skin · puncturedOKC - FOUND RIGHT OUTBOARD AFT FLAP INBOARD END HAS A PUNCTURE IN THE LOWER SURFACE. REMOVED DAMAGE AREA, FABRICATED FILLER AND DOUBLER AND INSTALLED REPAIR PIECES IAW B737-400 SRM 51-70-1 REPAIR 22. (M)SDR ASAA0540303Skin · delaminatedOKC - FOUND RT OB AFT FLAP DELAMINATED AT IB AFT CORNER.SDR ASAA0540302Skin · chafedOKC - FOUND RIGHT INBOARD FORE FLAP UPPER SURFACE CHAFED. REPAIRED IAW 737-400 SRM 51-70-10 REPAIR. (M)SDR 05FDEA01669Support Fitting · crackedRT WING, WHILE ACCOMPLISHING EA NR 1-5750-87541, OUTBOARD FLAP INBOARD HINGE SUPPORT FITTING FOUND CRACKED. REMOVED AND REPLACED PER AMM 27-50-30-4. FLAP RIGGING CARRIED OUT PER AMM 27-50-30-5.SDR SWAA051865Skin · delaminatedDURING SCHEDULED C2 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR MWEA050055Vane · gougedLEFT WING FIXED VANE HAS A 2 INCH GOUGE ON UPPER VANE SURFACE, AFT OF INBOARD FLIGHT SPOILER ACTUATOR, WING STATION 214. FABRICATED AND INSTALLED WING VANE.SDR ASAA0580355Vane · puncturedOKC - DURING HV-CHECK, FOUND LEFT INBOARD FLAP INBOARD FLAP VANE PUNCTURED AND DELAMINATED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER AND FILLER. (M)SDR SWAA051825Skin · delaminatedLT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.SDR COMA0570073Vane · crackedRT OUTBOARD FLAP VANE IS CRACKED. REPAIRED RT OUTBOARD FLAP VANE UPPER SKIN IAW BRAS EO 601R-52-6696.SDR COMA0570071Vane · crackedRT OUTBOARD FLAP VANE HAS 0.5 INCH CRACK ON UPPER SKIN APPROX 24 INCHES FROM INBOARD EDGE. CUT OFF INBOARD END OF SKIN PANEL TO REMOVE DAMAGE. FABRICATED AND INSTALLED REPAIR SKIN AND INTERNAL SPLICE DOUBLER (2024-13-040) IAW BRAS EO 601R-52-6696.SDR 05FDEA01615Tee Fitting · wornLT WING I/B FLAP ASSY I/B SEGMENT APPROX ALONG STA XIFH 207.30 FOUND TEE FITTING WORN. REMOVED AND REPLACED AS PER SRM 51-35-01 VOL II & DRAWING ARC 2482 FABRICATE NEW TEE SUPPORT.SDR USAA050773Skin · gougedCLT - FOUND SKIN GOUGED .125 INCH BY 1 INCH BY .060 INCH, LEADING EDGE RADIUS OF LEFT FOR FLAP .22 INCH FROM INBOARD END. REMOVED DAMAGED AREA, 2.5 INCH BY 1 INCH, INSTALLED EXTERNAL DOUBLER 7.5 INCH BY 6 INCHES IAW SRM 57-53-01 FIG 201. (M)SDR UPS05444836Rib · crackedINSPECTION TYPE:C, RHW NR 22 VC FLAP I/B ARM I/B SUPPORT RIB CRACKED AT D HOLE AREA. CRACK LENGTH 0.4375 IN. SUPPORT RIB LINKAGE ATT BOSS TIME LIMITED REPAIRED CARRIED OUT AS PER RS NR R57-41-35323 AND UPS EO NR B747-5740-22465-A.SDR 05FDEA01609Flap Track · corrodedNR 3 FLAP TRACK HAS CORROSION EMINATING FROM AFT ATTACH AREA. REPLACED NR 3 FLAP TRACK PER MM 27-51-031-4SDR ASAA0510159Skin · damagedYXX - IMPACT DAMAGE ON OUTBOARD T/E O RIGHT INBOARD MID FLAP. RIGHT INBOARD MID FLAP IMPACT DAMAGE LOCATION REPAIRED IAW B737-200 SRM 51-40-20 REPAIR NR 2. (M)SDR ASAA0510147Skin · dentedYXX - FOUND RIGHT INBOARD FLORE FLAP DENTED AND DELAMINATED AT OLD REPAIR AT BL 118. RIGHT INBOARD FORE FLAP AT WBL 118 DENTED AND DELAMINATED LOCATIONS REPAIRED IAW 737-200SRM. (M)SDR ASAA0510144Skin · damagedYXX - IMPACT DAMAGE ON OUTBOARD TRAILING EDGE OF RIGHT INBOARD MID FLAP. RIGHT INBOARD MID FLAP IMPACT DAMAGE LOCATION REPAIRED IAW B737-200 SRM 51-40-20 REPAIR 1. (M)SDR ASAA0510136Skin · chafedYXX - FOUND RIGHT INBOARD FORE FLAP CHAFE DAMAGE ON OUTBOARD TOP SURFACE AT WBL 181. RIGHT OUTBOARD FORE FLAP OUTBOARD TOP SURFACE AT WBL 181 CHAFED LOCATION REPAIRED IAW B737-200 SRM 51-40-20 REPAIR 4 FIG 13 WBL 181. (M)SDR ASAA0510135Skin · chafedYXX - FOUND RIGHT INBOARD FORE FLAP CHAFED ON INBOARD TOP SURFACE AT WBL 83. RIGHT INBOARD FORE FLAP INBOARD TOP SURFACE CHAFED LOCATION REPAIRED IAW B737-200 SRM 51-40-20 REPAIR 7 FIG 16 WBL 83. (M)SDR ASAA0510134Skin · damagedYXX - FOUND IMPACT DAMAGE ON OUTBOARD T/E OF RIGHT INBOARD MID FLAP. RIGHT INBOARD MID FLAP IMPACT DAMAGE LOCATION REPAIRED IAW B737-200 SRM. (M)SDR ASAA0510133Ramp · damagedYXX - LEFT WING OUTBOARD FORE FLAP OUTBOARD RAMP DAMAGED. LEFT WING OUTBOARD FORE FLAP OUTBOARD RAMP REPLACED WITH NEW PART PER IAW B737-200 SRM. (M)SDR ASAA0540288Skin · puncturedRT OB AFT FLAP IB END HAS A PUNCTURE IN THE LWR SURFACE. REMOVED DAMAGED AREA FABRICATED AND INSTALLED FILLER AND DOUBLER AND INSTALLED REPAIR PIECES IAW SRM. (K)SDR ASAA0540285Skin · chafedRT IB FORE UPPER SURFACE CHAFED. REPAIRED IAW SRM. (K)SDR ASAA0540284Skin · delaminatedRT OB AFT FLAP DELAMINATED AT IB AFT CORNER. REPAIRED IAW SRM. (K)SDR ASAA0540281Skin · dentedRT OB FORE FLAP HAS 4 EACH DENTS ON UPPER AFT SURFACE. REPAIRED RT OB FORE FLAP UPPER SURFACE IAW SRM. (K)SDR SWAA051698Skin · delaminatedDURING SCHEDULED C1 CHECK, FOUND LT WING INBOARD T/E FOREFLAP DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM.SDR SWAA051692Skin · delaminatedDURING SCHEDULED C2 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR SWAA051691Skin · delaminatedDURING SCHEDULED C2 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR ASAA0510124Skin · chafedYXX - FOUND RIGHT INBOARD FORE FLAP CHAFED DAMAGED ON OUTBOARD TOP SURFACE AT WBL 83. RIGHT INBOARD FORE FLAP, OUTBOARD TOP SURFACE AT WBL 83 CHAFED LOCATIONS REPAIRED IAW B737-200 SRM CHAPTER 51-40-20 REPAIR 7 FIGURE 16. (M)
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