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 2008UALA00970Flap · dentedLEFT WING, INBOARD FLAP, OUTBOARD LOWER TRAILING EDGE IS DENTED. PERFORMED REPAIR ON AREA.SDR SWAA080944Attach Fitting · corrodedDURING SCHEDULED 20Y CHECK, FOUND LT WING OUTBOARD FORE FLAP TRACK ATTACH FITTING CORRODED.SDR MASA200800153Flap Track · damagedREPAIR TO LEFT NR 4 FLAP TRACK.SDR MASA200800152Flap Track · damagedREPAIR TO LEFT NR 1 FLAP TRACK.SDR MASA200800151Flap Track · damagedREPAIR TO LEFT NR 5 FLAP TRACK.SDR USAA920080636Flap · delaminatedMCN - MAJOR REPAIR - C20 CHECK - LEFT WING INBOARD MIDFLAP HAS DELAMINATION, WBL 73 - WBL 82. REPAIRED LEFT WING INBOARD MIDFLAP, WBL 73 - WBL 82 IAW B737 SRM 51-70-10-2R4.SDR MASA200800158Flap Track · damagedREPAIR TO NR 3 LEFT FLAP TRACK.SDR SWAA080870Flap · delaminatedDURING SCHEDULED BRDG CHECK, FOUND LT WING OUTBOARD FOREFLAP DELAMINATED AT INBOARD END. REPAIRED FLAP PER SRM.SDR 2008UALA00918Fairing · puncturedRAMP REPORTS 5 MINS BEFORE DEPARTURE, RIGHT WING TRAILING EDGE FLAP TRACK FAIRING HAS PUNCTURE DAMAGE APPROX SIZE 5.5" BY 5.5" APROX 30 INCHES FROM T-E.SDR MASA200800146Flap Track · damagedREPAIR TO RIGHT NR 3 FLAP TRACK.SDR MASA200800145Flap Track · damagedREPAIR TO RIGHT I/B NR 2 FLAP TRACK.SDR DALA1013130186Fitting · unknownWING T/E FLAP INBD FLAP -MAIN FLAP -COLLAR FITTING REPLACEMENT FITTING. REPLACEMENT REPAIR IAW 01-073591-12 ME20 AND ME21. C/W 01-073591-12 ME20 AND ME21. (DL76L101470)SDR 08FDEA00460Skin · dentedRIGHT WING, INBOARD FLAP INBOARD LOWER SEGMENT LOWER SURFACE FOUND WITH DENT. DENT AREA FOUND OUT OF LIMIT AS PER SRM 57-10-00 FIGURE 17 VOLUME I AND REPAIR CARRIED OUT AT RT WING INBOARD FLAP INBOARD LOWER SEGMENT LOWER SURFACE AS PER SRM 57-10-00 FIGURESDR UIEA200800048Skin · corrodedLEFT OUTBOARD AFT FLAP UPPER SKIN HAS MINOR SURFACE CORROSION FOUND AFT OF OUTBOARD OF NR 2 SPINDLE. BLENDED OUT CORROSION IAW SRM 51-10-01. REPROTECTED PER 51-10-02.SDR IXXA08SMN073SFlap · dentedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT OUTBD FLAP UPPER PART SHOWS DENTS AT STATION XF 375.000 TO STA XF 404.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN, DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. SDR IXXA08SMN071SSkin · dentedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT OUTBOARD FLAP LOWER AFT SKIN HAS DENTS AT STATION XF 434.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN AND DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, SDR 08FDEA00435Skin · corrodedRT WING OUTBD T/E FLAP, LWR SURFACE OUTBD END, LIGHT SURFACE CORROSION REPAIRED RT OUTBOARD T/E FLAP LOWER SURFACE REF SRM 51-40-20 PAR 7, 8, 14, 15, 18, 20-22 AND APPLIED EXTERIOR PROTECTIVE PAINT FINISH REF MM 51-20-151-7, THIS IS CLASSIFIED AS A MINOR REPSDR 08FDEA00429Fairing · crackedLT WING, I/B FLAP, I/B TRACK AFT FAIRING SKIN CRACKED OUT ON TOP SIDE I/B OF AFT ATTACH BOLT, BOLT MOUNT CUTOUT. REPLACED FAIRING WITH SERVICEABLE UNIT. NR 4 TRACK POSITION. INSTALLATION ACCOMPLISHED ON WORK CARD NR 75C001-01. THIS IS CLASSIFIED AS A MINOR SDR 08FDEA00426Skin · delaminatedRT WING OUTBOARD AFT FLAP, LWR SURFACE 1 INCH FROM OUTBOARD END, SKIN DISBONDED. REPAIRED RT OUTBOARD AFT FLAP LOWER SURFACE 1 INCH FROM OUTBOARD END. REF 51-40-20 PAR 7, 8, 14, 15, 18, 20-22. THIS CLASSIFIED AS A MINOR REPAIR.SDR WRLA2008025Skin · debondedDURING C-CHECK INSPECTION FOUND LEFT INBOARD FLAP VANE LOWER SKIN DISBONDED TWO PLACES (20" X 23.5", 18" X 22"). REPAIRED LH FLAP VANE REF JOB CARD 038236 ITEM 1.SDR UPS08M52055Hinge Fitting · corrodedINSPECTION TYPE:C LEFT O/B TRAILING EDGE FLAP I/B WING MOUNTED HINGE PIVOT BORE HOLE AND FACE AREA FOUND RUSTY AS MARKED. (PIVOT BEARING REMOVED). LEFT FWD O/B FLAP I/B HINGE PIVOT BORE HOLE & FACE AREA CORROSION REMOVED & FOUND EXCEED LIMIT PER CMM57-44-08.SDR DLM88080274Skin · damagedDURING HMV ELONGATED HOLES WERE REPORTED ON UPPER SKIN OF LT OUTBOARD FLAP INBOARD SECTION. A NEW SKIN AND FINGER DOUBLER WERE FABRICATED AND INSTALLED IAW BOEING PRODUCTION DWG 9935954-15.SDR DLM88080273Vane · delaminatedDURING HMV, REPORTED A DELAMINATION ON UPPER SKIN OF INBOARD GUIDE VANE AT LEFT OUTBOARD FLAP. A PERMANENT REPAIR WAS PERFORMED IAW MD-80 SRM 57-03D PARAGRAPH 8A FIG 9A AND SRM 51-70-2D PARAGRAPH 6A, 6C, 10B, 10D AND 10E.SDR DLM88080268Skin · delaminatedDURING HMV, IT WAS FOUND A DELAMINATION ON UPPER SKIN OF INBOARD GUIDE VANE AT RT OUTBOARD FLAP. A PERMANENT REPAIR WAS PERFORMED IAW MD-80 SRM 57-03D PARAGRAPH 8A FIGURE 9A AND SRM 51-70-2D PARAGRAPH 6A, 6C, 10B, 10D AND 10ESDR DLM88080267Skin · erodedDURING HMV, EROSION WAS FOUND ON LOWER SKIN OF OUTBOARD GUIDE VANE OF RT INBOARD FLAP. A PERMANENT REPAIR WAS PERFORMED IAW MD-80 SRM 57-03D PARAGRAPH 8A FIG 9A.SDR DLM88080263Skin · nickedDURING HMV, SEVERAL NICKS WERE FOUND ON THE RT INBOARD FLAP LOWER SKIN P/N 9935942-6. A REPAIR WAS PERFORMED IAW ER/A 466344-14.SDR 2008UALA00823Panel · crackedRIGHT OUTBOARD FLAP OUTBOARD WRAP AROUND PANEL AT OUTBOARD SIDE UNDER AUX TRACK HAS CRACK. DURING A CHECK FOUND RH OUTBOARD FLAP OUTBOARD FLAP GUIDE BROKEN AND MISSING. SENT LEADING EDGE PANEL 666FT TO SHOP 273 FOR REPAIR. REPLACED RT OUTBOARD FLAP DEFLECTISDR SWAA080836Carriage · corrodedDURING SCHEDULED 20Y CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP NR 2 CARRIAGE LOWER SPINDLE CORRODED. REMOVED AND REPLACED CARRIAGE PER MM.SDR UPS08851654Skin · gougedRIGHT INBOARD T/E FLAP LOWER SURFACE DENT AT INBOARD LOCATION. MEASURE DENT AT 1 1/4 BY 1 3/4 .063 DEEP. FOUND .015 GOUGE IN DENT AND BLENDED TO .019 DEEP. REMOVED DAMAGE PER SRM 57-02-05. VERIFIED DAMAGED REMOVED. OK TO INSTALL DOUBLER. INSTALLED DOUBLESDR USAA920080476Skin · debondedMCN - MAJOR REPAIR - C18 CHECK - LEFT WING INBOARD FORE FLAP LOWER SURFACE HAS AREA DEBONDED, WBL 175 - WBL 178. REPAIRED AREA OF DISBOND LEFT WING INBOARD FORE FLAP LOWER SURFACE, WBL 175 - WBL 178 IAW B737 SRM 51-70-10.SDR IXXA08SMN065SSkin · dentedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT OUTBOARD FLAP LOWER SKIN FORWARD SHOWS DENTS BETWEEN STATION XF 160.000 - XF 213.000. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK NO CORROSION FOUND. PERFORMED MEASUREMENT DIA 2.00 BY 0.008" DEPTH WITHIN PERMSDR IXXA08SMN63SSkin · dentedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT OUTBOARD FLAP LOWER SKIN SHOWS DENTS AT STATION XF 434.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGE SKIN. FABRICATED NEW SKIN, AND DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED TREASDR UIEA200800037Skin · delaminatedLEFT OUTBOARD MIDFLAP LE CHIPPED AND HAS EVIDENCE OF DELAMINATION APPROX 6 INCHES LOCATED 18 INCHES OUT BOARD OF NR 1 FLAP TRACK. REPAIRED PER SRM 51-40-12 AND EO4757A418.SDR 2008UALA00743Wedge · delaminatedDURING RIGGING OF LEFT WING INBOARD SPOILER FOUND MID FLAP TRAILING EDGE LOWER SKIN DELAMINATED AND SEPARATED FROM MIDFLAP. ACCOMPLISHED REPAIR OF DELAMINATED SKIN.SDR IXXA08SMN069SLink · crackedDURING ROUTINE C CHECK INSPECTION, FOUND FLAP MECHANISM OF INNER WING FORWARD LINK CRACKED AT STATION 3.000 RIGHT. REMOVED REPLACED INNER WING FORWARD LINK OF FLAP MECHANISM IAW OHM 27-27-1 PAGE 4. PERFORMED OPS CHECK TO ALL FLIGHT CONTROLS. GOOD IAW DC8 MASDR IXXA08SMN068SDrive Link · bentDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING LINK AT FLAP DRIVE LINK BENT AT STATION 3.000. REMOVED AND REPLACED LEFT WING FLAP DRIVE LINK IAW DC8 MAINTENANCE MANUAL 20-16-0 PAGE 202. PERFORMED OPS CHECK TO ALL FLIGHT CONTROLS. OPERATIONAL CHECK GOOD SDR 08FDEA00372Skin · crackedCRACKED HOLES FOUND DURING ACCOMPLISHMENT OF EO6-5750-7-5000 AT RIB 7, INNER FLAP LT AND DAMAGED NOSE SKIN JOINT STRIP. REPAIR PERFORMED BY REAM UP UNTIL CRACK REMOVAL AT HOLE ON RIB 7 AND REMOVAL OF CRACK AT NOSE SKIN JOINT STRIP IAW RAS/FOK/015/2008 ISSUE ASDR UIEA200800036Skin · erodedLEFT OUTBOARD FOREFLAP HAS EVIDENCE OF EROSION AT 2 PLACES ON IT'S LEADING EDGE AT APPROX 12 AND 18 INCHES OUTBOARD OF NR 1 FLAP TRACK, EVIDENCE OF CONTACT BETWEEN FOREFLAP AND T/E PANEL. LT OUTBOARD FOREFLAP LEADING EDGE EROSION REPAIRED IAW SRM 51-40-12 ANDSDR G60A200800013Angle · crackedRT INBOARD FLAP INBOARD LWR CLOSE OUT PANEL HAS CRACKED ANGLE.SDR 08FDEA00364Skin · crackedDENT AND CRACK FINDING ON RT CENTER FLAP TRAILING EDGE LOWER SKIN. REPAIR PERFORMED BY INSTALLING A EXTERNAL PATCH IAW RAS/FOK/011/2008, APPROVED BY EA 6-5753-114875.SDR DL76L091890Collar · damagedWING T/E - INBD FLAP - MAIN FLAP - COLLAR FITTING REPAIR IAW 01-073591-12 ME20 AND ME21, C/W 01-073591-12 ME20 AND ME21.SDR SWAA080689Skin · delaminatedDURING SCHEDULED C2 CHECK, FOUND LT WING INBOARD T/E AFT FLAP DELAMINATED ON LOWER SURFACE. REMOVED AND REPLACED FLAP PER MM.SDR SWAA080688Skin · delaminatedDURING SCHEDULED C2 CHECK, FOUND LT WING INBOARD FOREFLAP DELAMINATED ON UPPER SURFACE. REMOVED AND REPLACED FLAP PER MM.SDR FDEA200802050350Skin · crackedLT WING INBOARD FLAP ON UPPER SKIN FOUND CRACK. REPAIRED AREA IAW SRM 57-00-01 FIG 4 SHT 2 VOL I.SDR SWAA080672Skin · delaminatedDURING SCHEDULED 20Y CHECK, FOUND LT WING INBOARD FOREFLAP UPPER SURFACE DELAMINATED. REPAIRED FLAP PER SRM.SDR SWAA080673Skin · delaminatedDURING SCHEDULED 20Y CHECK, FOUND RIGHT WING INBOARD FOREFLAP UPPER SURFACE DELAMINATED. REPAIRED FLAP PER SRM.SDR 08FDEA00350Skin · crackedLT WING INBOARD FLAP ON UPPER SKIN FOUND SCRATCH.SDR DLM88080172Skin · damagedTHE RT WING INBD MAIN FLAP LOWER REMOVEABLE TRAILING EDGE SKIN WAS SPLICED TO REMOVE NICKS.SDR 2008UALA00652Skin · gougedRT INBOARD FLAP VANE UPPER EXTERNAL SURFACE IS GOUGED AT OUTBOARD END OF VANE. ACCOMPLISHED MAJOR REPAIR AT GSO.SDR 200800028Skin · puncturedDURING A CHECK, FOUND LT WING T/E I/B MID FLAP WBL 443.83 LOWER SURFACE CRACKED AND BULLNOSE PUNCTURE, IN ADDITION LT IB AFT FLAP WBL 445 OUTBOARD EDGE WITH DELAMINATION. DISPOSITION WAS MADE TO PERFORM A WET LAY UP INTERIM REPAIR (REF BOEING SRM 57-53-01, FI
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