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 UIEA2017081701499Panel · delaminatedLT I/B MID FLAP UPPER ECENTER SECTION PANEL HAS DELAMINATION. REPLACED LT I/B MID FLAP UPPER CENTER SECTION PANEL IAW EA 747-5753-28-A6917 AND EO1957A317.SDR LR7A2017081901185Skin · crackedDURING SCHEDULED B-3 CHECK, FOUND THE LT INBOARD FLAP LOWER SKIN WITH A 4 INCH CRACK AT CWS 136L. REPAIRED IAW SRM 57-70-10 AND 51-140-12.SDR SWIA201743762Plate · chafedRIGHT WING AFT FLAP HINGE ARM UNDER PANEL 683BB CHAFED ON THE INBD & OTBD GUIDE PLATE. REPLACED THE GUIDE PLATES IAW SRM.SDR SWIA201743761Plate · gougedRIGHT WING AFT FLAP HINGE ARM LOCATED UNDER PANEL 686BB HAS GOUGE INBD GUIDE PLATE. REPLACED OUT OF LIMITS ATTACHMENT BRACKET IAW SRM.SDR SWIA201743760Hinge Arm · gougedRIGHT WING FLAP AFT HINGE ARM LOCATED UNDER PANEL 695BB HAS A GOUGE AND HAS A WORN INBD GUIDE PLATE. REMOVED AND REPLACED BRACKET WITH SERVICEABLE BRACKET IAW SRM.SDR SWAA2022013131870Flap · delaminatedLH WING; O/B AFT FALP; I/B LOWER SURFACE IS DELAMINATED. DELAM IS APROX 11' X 11' / REMOVED & REPLACED LH O/B AFT FLAP; RIG & OPS CHECKED OK PER M/M 27-51-22. P/N OFF 113A3700-25; S/N OFF 3964; P/N ON 113A3700-23; S/N ON 002458.SDR FDEA201708172251Bracket · looseFLAP FAIRING BRACKET FOR 573HB IS LOOSE. REPAIRED THE LT, INBD MAIN FLAP IAW SRM 57-53-02-2R, REPAIR 3, AND EA F-5750-T0334988, PI.SDR AALA20170817004Hinge Fitting · corrodedCORROSION ON LEFT WING OUTBOARD FORWARD FLAP CENTER HINGE FITTING AT LOWER OUTBOARD STUD ATTACH POINT. REMOVED AND REPLACED HINGE FITTING IAW AMM 57-40-01-201SDR AALA20170817003Hinge Fitting · corrodedCORROSION ON RIGHT WING OUTBOARD FLAP CENTER HINGE FITTING AT UPPER AND LOWER STUDS. REMOVED AND REPLACED HINGE FITTING PER AMM 57-40-01-201SDR SWAA2017081815798Skin · delaminatedLEFT WING OUTBOARD AFT FLAP INBOARD LOWER SURFACE DELAMINATED. R & R AFT FLAP IAW MM.SDR IXXA20170906282Support · damagedRIGHT WING TRAILING EDGE FLAP SUPPORT HAS A DAMAGED FASTENER HOLES. SPOT FACED.SDR ASOA201708151867Doubler · gougedRT INBOARD FLAP INTERNAL DOUBLER GOUGED UNDER OUTBOARD MOST VANE ACTUATOR. COMPLIED WITH EC/TC REO 670-57-52-352 AND REO 670-57-52-352 REV - DATED 03/28/2017 AS WRITTEN.SDR FQAR20170815079Angle · crackedDURING ROUTINE INSPECTION, AN ANGLE INSTALLED AGAINST RIGHT WING INBOARDMOST FLAP SUPPORT WAS FOUND CRACKED. CRACKING EXTENDED THROUGH RIVET HOLES TO MATERIAL EDGE.SDR FQAR20170815077Angle · crackedDURING ROUTINE INSPECTION, AN ANGLE INSTALLED AGAINST LEFT WING INBOARD MOST FLAP SUPPORT WAS FOUND CRACKED. CRACKING EXTENDED THROUGH RIVET HOLES TO MATERIAL EDGE.SDR SWAA2022013041331Flap · delaminatedREMOVE AND REPLACE RT WING O/B AFT FLAP DUE DELAMINATION IS OUT OF LIMITS. / REMOVED UNSERVIABCLE R/H O/B AFT FLAP ASSY IAW AMM 27-51-22-000-801 AND REPLACED WITH NEW INSTALLED IAW AMM 27-51-22-400-801 POS:R/H O/B AFT TAG NO:271994; P/N OFF:113A3700-20; S/N OFSDR SWIA2017092943798Skin · dentedLEFT INBOARD FLAP TOP AND BOTTOM SKIN DENTED. TOP DENT APPROX 1.5" X .5" X .10". BOTTOM DENT APPROX 4" X 1.5" X .10". REPAIRED THE SKIN IAW SRM.SDR FDEA201708102171Hinge Bracket · corrodedRIGHT WING INBOARD FLAP OUTBOARD AFT HINGE BRACKET (FLAP SIDE) PIVOT OUTBOARD BORE FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-03. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-132256 G, PART 5, STEPS 2 AND 3. THE REPAIR WASSDR FDEA201708102167Hinge Fitting · corrodedLEFT WING INBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) PIVOT OUTBOARD BORE FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-03. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-152244 H, PART 6, STEPS 2 AND 3. THE REPAIR CLASSIFIED ASDR FDEA201708102166Hinge Fitting · corrodedLEFT WING INBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) PIVOT INBOARD BORE FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-03. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-132244 H, PART 6, STEPS 2 AND 3. REPAIR CLASSIFIED AS SDR DALA2017081106134Attach Bolt · corrodedRUSTED RT FLAP HINGE FITTING ATTACH BOLT STA XW= 251 AT RT WING. RUST WAS REMOVED PER SRM 51-10-03 PARA 26 VOL II AND SERVICEABLE FLAP HINGE AT RT WING STA 251 WAS INSTALLED PER AMM 57-40-01-201.SDR DALA2017081106132Support Fitting · corrodedCORROSION ON FLAP HINGE SUPPORT STA XW 251 AT LEFT WING REAR SPAR. LT WING FLAP HINGE SUPPORT FITTING WAS REPAIRED, BUSHING WERE FABRICATED AND INSTALLED PER CMM 27-50-5 PAR 2 I AND HINGE WAS INSTALLED PER AMM 57-40-01-201.SDR FDEA201708092156Vane · dentedRIGHT INBD FLAP VANE LOWER SURFACE HAS IMPACT DAMAGED .300" X .300" AT THE CENTER TRACK. REPAIRED THE VANE IAW SRM 57-00-01, FIG 4, VOL I, PAGE 11.SDR SWIA2017092943799Skin · dentedLEFT INBD FLAP HAS A DENT ON UNDERSIDE JUST INBD OF WS 120.382. REPAIRED THE FLAP SKIN IAW SRM.SDR A6WA2017082945237Skin · damagedLEFT INBD FLAP LOWER SKIN DAMAGED. REPLACED THE SKIN IAW SRM 51-42-13, 57-52-00, AND 51-40-11.SDR SWIA201743667Skin · dentedLEFT WING INBD FLAP HAS TWO DENTD ON THE UPPER SURFACE. REPAIRED THE DAMAGE IAW REO.SDR SWIA201743666Skin · dentedLEFT WING OTBD FLAP HAS ONE DENT ON THE ON THE UPPER SURFACE. COMPLIED WITH REPAIR IAW SRM.SDR DALA2017080806039Hinge · corrodedCORROSION AROUND STUD HOLES ON RT WING FLAP HINGE SUPPORT NR 3. DUE TO EXCESSIVE DAMAGE ON HINGE. THE HINGE WAS REPLACED.SDR A6WA201745203Skin · chafedLEFT I/B FLAP VANE HAS A CHAFE AT THE I/B STOP. REPLACED FLAP VANE LEADING EDGE IAW SRM 51-42-13.SDR CALA2017080802508Spar · corrodedLEFT WING INBD MAIN FLAP AFT SPAR LOWER SURFACE HAS CORROSION. APPROXIMATELY 28 INCHES FROM INBD EDGE. ACCOMPLISHED EC/RA 5750-04988.SDR FDEA201708062125Spar · corrodedLT WING O/B FLAP MID AREA INTERIOR FRONT SPAR LOWER CHORD FOUND HEAVY CORROSION. COMPLIED WITH EA F-5750-T0334766 P1, REPAIRED LT WING O/B FLAP MID AREA INTERIOR FRONT SPAR LOWER CHORD. MAJOR REPAIR IAW GMM 6-2-100.SDR SWIA201743751Skin · dentedLEFT INBD FLAP HAS ONE SMALL DENT ON UPPER SURFACE, TWO INCHES FORWARD OF TRAILING EDGE AND 21.3 INCHES FROM I/B EDGE. REPAIRED IAW SRM.SDR AALA201708079014Tab · delaminatedAIRCRAFT WAS GROUNDED. DISBOND (DELAMINATION) ON LEFT HAND OUTBOARD FLAP TAB APPROXIMATELY 10 INCH ON TOP SIDE AT APPROXIMATELY 30-36 INCHES FROM OUTBOARD EDGE. REPAIRED FLAP TAB ASSEMBLY PER EA 272301.SDR A6WA201745159Skin · damagedLEFT INBD FLAP HAD AN OVERSIZED HOLE COMMON TO THE INBD SEAL AT AFT END.SDR DALA2017081106135Vane · crackedCRACK ON UPPER INBD CIRCULAR PANEL AT LT OTBD FLAP OTBD FIXED VANE CIRCULAR PANEL ON TOP SURFACE IAW NRC 00935. THE FLAP OTBD FIXED VANE WAS REPLACED IAW AMM 27-51-03.SDR SWAA2017080915551Skin · delaminatedRT WING INBOARD AFT FLAP DELAMINATED ON UPPER SURFACE. R&R AFT FLAP PER MM.SDR DALA2017080405951Skin · nickedNICK ON LOWER SKIN INBD EDGE ON RT OUTBD FIXED GUIDE VANE OUTBD FLAP. RT OUTBD FIXED GUIDE VANE OUTBD FLAP WAS REPAIRED PER SRM 57-03 D PAR 11.SDR IPXA2017081820675Vane · puncturedINSPECTION TYPE: 3C, RT INBD FLAP VANE LOWER SKIN PUNCTURED 77 INCHES FROM INBD EDGE & 20 INCHES FROM T/E. REPAIRED THE FLAP VANE LOWER SKIN IAW SRM 51-71-00, PARA. 19B. MAJOR.SDR SWIA201743650Plate · gougedRIGHT FLAP INBOARD ROLLER GUIDE PLATE IS GOUGED. REPLACED THE ROLLER GUIDE PLATE IAW SRM.SDR SWIA2017082143649Vane · chafedLEFT OTBD FLAP VANE HAS CHAFING NEAR OTBD ACTUATOR. INSTALLED A REPAIR IAW REO.SDR DALA2017080305950Vane · delaminatedHIDDEN DAMAGE DELAMINATION BELOW RUB STRIP ON LT OUTBD FIXED GUIDE VANE INBD FLAP. LT WING INBD FLAP OUTBD FIXED GUIDE VANE WAS REPAIRED PER SRM 57-03 D PARAGRAPH 11 FIG 11.SDR DALA2017080305884Doubler · wornWORN LEADING EDGE REPAIR DOUBLER ON RT OUTBOARD FLAP INBOARD GUIDE VANE. RT OUTBOARD FLAP INBOARD GUIDE VANE WAS REPAIRED PER SRM 57-03 D.SDR JGVR20170803001Skin · delaminatedONE SPOT OF DELAMINATION ON LT INBOARD FLAP BOTTOM SURFACE. REPAIRED DELAMINATED AREA ON LT INBD FLAP IAW SRM 57-50-02.SDR SWIA2017091943769Skin · dentedLEFT INBOARD FLAP LOWER SKIN HAS A DENT .041 INCH DEEP AT THE INBOARD TRAILING EDGE. REPAIRED IAW REO.SDR SWIA2017091943768Skin · dentedRIGHT INBOARD FLAP LOWER SKIN HAS THREE DENTS ALONG INBOARD EDGE MEASURING .027 INCH DEEP, .072 INCH DEEP AND .041 INCH DEEP. REPAIRED IAW REO.SDR AALA201708039021Stud · corrodedAIRCRAFT IN BASE MAINTENANCE. CORROSION ON LEFT WING OUTBOARD FLAP CENTER HINGE FITTINGS LOWER OUTBOARD MOUNT STUD BETWEEN STATION 984 AND 1007. REPLACED INBOARD UPPER MOUNT STUD PER AMM 57-40-01-201. (SEE AALA20170731001, AALA201708039018, AALA201708039019, SDR AALA201708039020Stud · corrodedAIRCRAFT IN BASE MAINTENANCE. CORROSION ON LEFT WING OUTBOARD FLAP CENTER HINGE FITTINGS LOWER OUTBOARD MOUNT STUD BETWEEN STATION 984 AND 1007. REPLACED INBOARD UPPER MOUNT STUD PER AMM 57-40-01-201. (SEE AALA20170731001, AALA201708039018, AALA201708039019, ASDR AALA201708039019Stud · corrodedAIRCRAFT IN BASE MAINTENANCE. CORROSION ON LEFT WING OUTBOARD FLAP CENTER HINGE FITTINGS LOWER OUTBOARD MOUNT STUD BETWEEN STATION 984 AND 1007. REPLACED INBOARD LOWER MOUNT STUD PER AMM 57-40-01-201. (SEE AALA20170731001, AALA201708039018, AALA201708039020, ASDR AALA201708039018Stud · corrodedAIRCRAFT IN BASE MAINTENANCE. CORROSION ON LEFT WING OUTBOARD FLAP CENTER HINGE FITTINGS LOWER OUTBOARD MOUNT STUD BETWEEN STATION 984 AND 1007. REPLACED OUTBOARD LOWER MOUNT STUD PER AMM 57-40-01-201. (SEE AALA20170731001, AALA201708039019, AALA201708039020, SDR AALA20170731001Hinge Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE. CORROSION ON LEFT WING OUTBOARD FLAP CENTER HINGE FITTING LOWER OUTBOARD MOUNT STUDS BETWEEN STATION 984 AND 1007. REPLACED HINGE FITTING PER AMM 57-40-01. (SEE AALA201708039018, AALA201708039019, AALA201708039020, AALA20170803902SDR RAIA201707290002Flap Track · crackedFLAP OVERSPEED 290 KNOTS AT FLAPS 9. PERFORMED MAX FLAP EXTENDED SPEED INSPECTION, FAILED NDI TESTING ON LEFT WING O/B FLAP INBD TRACK AND RIGHT WING O/B FLAP INBD TRACK.
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