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 ASAA0945785Skin · puncturedLEFT I/B FORE FLAP LOWER SKIN PUNCTURED 16 INCHES FROM I/B EDGE AND 6 INCHES FROM TRAILING EDGE. REPAIRED PUNCTURE ON LEFT I/B FORE FLAP LOWER SKIN PUNCTURED 16 INCHES FROM I/B EDGE AND 6 INCHES FROM TRAILING EDGE.SDR QXEA2009060100384Vane · gougedTHE LEFT OUTBOARD FLAP MOST OUTBOARD BUTE DOOR GUIDE RAIL HAS GOUGE ON THE LEADING EDGE AT THE TOP AND THE MIDDLE OF THE RAIL. REMOVED OUTBOARD FLAP VANE FROM FLAP. REMOVED OUTBOARD MOST VANE RIB END GUIDE RAIL BY REMOVING OUTBOARD MOST VANE L/E. INSTALLEDSDR DLM88090937Skin · gougedLT INBD FLAP LOWER SURFACE DAMAGED WITH SEVERAL GOUGES. REPLACED SKIN IAW 57-50-14 AND 51-30-02.SDR FDEA200905281841Skin · crackedRT FORE FLAP OTBD WBL 442 CRACK ON SKIN ABOVE CARRIAGE ATTACH FITTING. REMOVED RT OTBD FORE FLAP TO FOM REPAIR IAW MM 27-51-011-4. STOPPED DRILLED CRACK IAW SRM 51-10-1. HFEC INSPECTED STOP DRILL AREA IAW NDTM 51-00-00 FIG 3 PT6 NO DEFECTS NOTED. FABRICASDR ASAA0945781Skin · gougedLT OB MID FLAP LOWER AFT PANEL UPPER SKIN IS GOUGED AT NR 4 AFT FLAP TRACK. LT OB MID FLAP LOWER AFT PANEL UPPER SKIN IS GOUGED AT NR 4 AFT FLAP TRACK WAS REAPIRED.SDR ASAA0945780Skin Panel · chafedRT, OB MID FLAP LOWER AFT PANEL UPPER SKIN IS CHAFED AT NR4 AFT FLAP TRACK. RT OB MID FLAP LOWER AFT PANEL UPPER SKIN IS CHAFFED AT NR 4 AFT FLAP TRACK WAS REPAIRED.SDR ASAA0945782Skin · chafedLEFT O/B FORE FLAP LLE IS CHAFED AT O/B EDGE. REPAIRED LEFT O/B FORE FLAP LEADING EDGE O/B EDGE.SDR ASAA0945783Skin · chafedRIGHT O/B FORE FLAP LLE IS CHAFED AT O/B EDGE. REPAIRED RIGHT O/B FORE FLAP LEADING EDGE O/B END.SDR FDEA200905281840Skin · crackedLT WING OTBD FLAP UPPER SKIN FOUND CRACK ON SKIN. REPAIRED AREA IAW SRM 57-00-01 FIG 4 SHT 2 VOL I.SDR USAA2009062391563Fitting · crackedMCN - C22 - MAJOR REPAIR - CRACK IN NR 3 FLAP TRACK FIXED FAIRING INTERFACE FITTING. REPAIRED NR 3 FLAP TRACK FIXED FAIRING INTERFACE FITTING IAW US AIRWAYS EA 130263.SDR ASAA0995734Support Fitting · wornRT OTBD FLAP, OTBD FLAP TRACK SUPPORT FITTING WORN FROM SEAL. REPAIRED FITTING.SDR AALA20090528TUL03Carriage · damagedNUMBER 1 FLAP CARRIAGE BELLCRANK HOLE OVERSIZED. REPAIRED PER EA COMP 57-006352 AND CARD J1071AB.SDR AALA20090528TUL02Carriage · damagedNUMBER 2 FLAP CARRIAGE HOLE OVERSIZED. REPAIRED HOLE PER EA COMP - 57-006351 AND CARD J1071AB.SDR DLM88090924Vane · dentedLT INBD FLAP, INBD VANE HAS DENTS AND PUNCTURE ON EXISTING REPAIR LWR SURFACE. REPAIRED IAW ERA 4731169-14 REV ORIG. DATED 5/20/09.SDR QXEA2009052600380Panel · chafedPDX - 20K - RT WING FLAP PANEL 684LB IS CHAFED. BLENDED OUT DAMAGE AND FOUND TO BE WITHIN LIMITS. MAX MATERIAL REMOVED .006 ETCHED, ALODINED AFFECTED AREA REF SRM 57-52-01-101-001-A01. FPI IAW CRJ 700 NDTM PART I 51-20-008, NO CRACKS NOTED. PRIMED AND PASDR QXEA2009052600379Panel · chafedPDX - 20K - RT WING FLAP PANEL 684JB HAS CHAF. BLENDED OUT DAMAGE IAW CRJ SRM 57-52-02 PG 102 AND FOUND TO BE WITHIN LIMITS. MAX MATERIAL REMOVED .007 ETCHED, ALODINED AFFECTED AREA REF SRM 51-12-00-001-001-A01. FPI IAW CRJ 700 PART 1 51-20-008. NO CRACKS SDR QXEA2009052700378Panel · chafedPDX - 20K - RT FLAP PANEL 684AB HAS CHAF. BLENDED OUT DAMAGE IAW CRJ SRM 57-52-02 PG 102 AND FOUND TO BE WITHIN LIMITS. ORIGINAL THICKNESS .100 REMAINING IS .088 OK FOR SERVICE. FPI BLENDED AREA FOR CRACKS IAW SRM 51-12-00-001-001-A01 PAGE 10, PAR 7B(4), ASDR QXEA2009052700377Panel · chafedPDX - 20K - RT FLAP PANEL 684EB HAS CHAF. BLENDED OUT DAMAGE IAW CRJ SRM 57-52-02 PG 102 AND FOUND TO BE WITHIN LIMITS. ORIGINAL THICKNESS .100 REMAINING IS .085 OK FOR SERVICE. FPI BLENDED AREA FOR CRACKS IAW SRM 51-12-00-001-001-A01 PAGE 10, PAR 7B(4), ANSDR QXEA2009052700376Panel · chafedPDX - 20K - LT FLAP PANEL 584GB HAS CHAF. BLENDED OUT AND FOUND TO BE WITHIN LIMITS MAX MATERIAL REMOVED .011. ETCHED AND ALODINED AFFECTED AREA REF DAMAGE IAW CRJ 700 SRM 57-52-01-101-001-A01. FPI IAW CRJ 700 PART 1, 51-20-008, NO CRACKS NOTED. PRIMED ANSDR QXEA2009052600375Panel · chafedPDX - 20K - LT FLAP PANEL 584LB HAS CHAFE. BLENDED OUT AND FOUND TO BE WITHIN LIMITS MAX MATERIAL REMOVED .008. ETCHED AND ALODINED AFFECTED AREA REF DAMAGE IAW CRJ 700 SRM 57-52-01-101-001-A01. FPI IAW CRJ 700 PART 1, 51-20-008, NO CRACKS NOTED. PRIMED ASDR QXEA2009052600374Panel · chafedPDX - 20K - LT FLAP PANEL 584JB HAS CHAF. BLENDED OUT DAMAGE AND FOUND TO BE WITHIN LIMITS. MAX MATERIAL REMOVED .010. ETCHED AND ALODINED AFFECTED AREA REF DAMAGE IAW CRJ 700 SRM 57-52-01-101-001-A01. FPI IAW CRJ 700 PART 1, 51-20-008, NO CRACKS NOTED. PSDR QXEA2009052700373Panel · chafedPDX - 20K - LT FLAP PANEL 584EB HAS CHAF APPROX .020. BLENDED OUT DAMAGE IAW CRJ 700 SRM 57-52-02 PG 102. DAMAGE IS WITHIN LIMITS AND OK FOR CONTINUED SERVICE. ORIGINAL THICKNESS .100 MATERIAL REMAINING IS .078. PERFORMED FPI OF PANEL 584EB BLEND FOR CRACKSDR QXEA2009052700372Panel · chafedPDX - 20K - RT FLAP PANEL 684BB HAS CHAF ON SHORT CURVE PANEL APPROX .010. BLENDED OUT DAMAGE IAW CRJ 700 SRM 57-52-02 PG 102. DAMAGE IS WITHIN LIMITS AND OK FOR CONTINUED SERVICE. ORIGINAL THICKNESS .100 MATERIAL REMAINING IS .085.SDR IPXA09156197Skin · misrepairedINSPECTION TYPE-4/C REPAIR SURVEY SEQ NR 125-W4-03 ON RT MIDDLE FLAP LEADING EDGE DOES NOT CORRELATE WITH SRM. REMOVED AND REPLACED REPAIR DOUBLER IAW EO A300-5750-33755-A AND EA NR 300-5753-01-A1801, REF RCD NR 358681.SDR IPXA09156193Skin · gougedINSPECTION TYPE-4/C REPAIR SURVEY SEQ. NR 125-W4-01 ON RT INBD FLAP UPPER SURFACE IS GOUGED. REPLACE DOUBLER IAW SRM 57-50-00, PARA. 4E, FIG 205 REF. RCD NR 358679.SDR IPXA09156192Skin · gougedINSPECTION TYPE-4/C REPAIR SURVEY SEQUENCE NR 125-W3-02 ON MIDDLE FLAP UPPER SURFACE IS GOUGED. REPLACED DOUBLER IAW SRM 57-50-00 PARG. 4E, AND FIG. 205 REF UPS RCD NR 358682.SDR IPXA09M56211Skin · damagedINSPECTION TYPE-2C REPAIR SURVEY SEQ NR 250-W4-03 FOUND TO BE IAW SRM. REMOVED EXISTING REPAIR, FABRICATED AND INSTALLED REPLACEMENT REPAIR IAW UPS EO MD11-5750-33764-A AND SAA EA 011-5730-01-A1807.SDR HALA2009052200215Frame · corrodedLEVEL 2 CORROSION ON TOP OF LT FLAP AFT INTERNAL FRAMES TOP SURFACE. SECTION REPLACEMENT, REPAIRED IAW 767-300 SRM 51-70-12 FIG 2.SDR DLM88090913Vane · puncturedLT INBD FLAP OTBD VANE HAS PUNCTURES AND GOUGES LWR INBD SIDE. REPAIRED LT INBD FLAP OTBD VANE LWR SURFACE DAMAGE IAW SRM 57-03D FIG 11.SDR IPXA09M56242Skin · damagedINSPECTION TYPE-C REPAIR SEQUENCE NBR 280-W4-007, RT INBD FLAPS OUTER SKIN SURFACE STA XIFH 153.3 23 INCH AWAY FROM FLAPS L/E. REPAIR NEEDS VALIDATION. EXISTING REPAIR DOUBLER REMOVED. 10X VISUAL INSP C/O, FOUND NO CRACK OR CORROSION. HFEC INSP C/O ON EXISSDR ASAA0945822Skin · dentedRIGHT I/B FORE FLAP UPPER SURFACE HAS CHAFED REPAIRS. REPAIRED DAMAGED AREAS IAW SRM.SDR ASAA0945819Skin · dentedRIGHT I/B FORE FLAP LOWER SURFACE PREVIOUS REPAIR HAS DENTS. REPAIRED DAMAGE IAW SRM.SDR SWAA093358Flap · delaminatedDURING SCHEDULED MV2 CHECK, FOUND RT WING O/B AFT FLAP DELAMINATED ON I/B END. R&R AFT FLAP PER MM.SDR AALA20090609TUL33Vane · damagedTEMP REPAIR ON L/E OF VANE. INSTALLED HOT BOND REPAIR ON DAMAGED AREA PER ESO8OO95.SDR IPXA09156198Doubler · gougedINSPECTION TYPE-4/C 4 GOUGED AREAS CENTER OF BACKSIDE OF RT MID FLAP APPX. 7 INCHES FROM INBD END. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-50-00, PAGE 220, FIG. 205, AND SRM 57-50-00, PARA. 4 E.,FIG 205 REF SAA EA 300-7530-01-A1817 AND UPS EO NR ASDR ASAA0975705Flap Track · corrodedRT WING IB FLAP IB TRACK HAS LIGHT RUST AND BARE METAL. REMOVED AND REPLACED FLAP TRACK.SDR UIEA201000122Support · damagedTHE PURPOSE OF THIS EO IS TO RECORD A MAJOR REPAIR. DURING C CHECK INSPECTION BEING PERFORMED AT HKG; DAMAGE WAS FOUND TO THE RIGHT O/B MID FLAP NR 3 TRAILING EDGE PANEL SUPPORT (I/B OF NR 8 CARRIAGE) CONSISTING OF A SCREW HOLE ELONGATED (REFERENCE FIGURE 1).SDR FDEA200905191733Skin · misrepairedEXISTING REPAIR FOUND ON RT WING INBD FLAP UPPER SKIN AT STA. XIFH= 216. FOUND NOT IAW SRM. REPAIR CARRIED OUT AS PER SRM 57-10-00 FIG. 38 REV. 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107.SDR IPXA09656116Fairing · delaminatedINSPECTION TYPE:7C LT WING - I/B MAIN FLAP O/B LEADING EDGE FAIRING DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-05, PAR 5A (1), FIG 5, REV 43.SDR UALA2009051901421Flap · damagedLT OTBD FLAP REPLACEMENT. LT OTBD FLAP REPLACED. TEST FLT ACCOMPLISHED. FLAPS TEST OK, FLAP LD RELIEF REPAIRED. FSEU REPLACED, AIL LOCK"L" ON AT LOW SPEED REPAIRED, LEFT AIL LOCKOUT ACT REPLACED. NO REFLY RQD.SDR FDEA200905191751Hinge Bracket · corrodedLEFT WING, FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT HOLE FOUND CORRODED. COMPLIED WITH E.A. 1-5750-130946, CLASSIFIED AS MAJOR REPAIR AS PER GMM 6-2-100 REV. 107.SDR FDEA200905191749Hinge Bracket · corrodedRIGHT WING, FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT HOLE FOUND CORRODED. COMPLIED WITH E.A. 1-5750-130949, CLASSIFIED AS MAJOR REPAIR AS PER GMM 6-2-100 REV. 107.SDR FDEA200905191748Hinge Bracket · corrodedRIGHT WING, FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT HOLE FOUND CORRODED. COMPLIED WITH E.A. 1-5750-130949, CLASSIFIED AS MAJOR REPAIR AS PER GMM 6-2-100 REV. 107.SDR FDEA200905191747Support · corrodedRIGHT WING, FLAP SIDE OUTBOARD FLAP INBOARD HINGE INBOARD PIVOT HOLE FOUND CORRODED. COMPLIED WITH E.A. 1-5750-130945, CLASSIFIED AS MAJOR REPAIR AS PER GMM 6-2-100 REV. 107.SDR SWAA093279Flap · delaminatedDURING SCHEDULED 2HC2 CHECK, FOUND LT WING I/B FOREFLAP UPPER SURFACE DELAMINATED. R&R FOREFLAP PER MM.SDR SWAA093271Flap · delaminatedDURING SCHEDULED SPV CHECK, FOUND LT WING O/B FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER SRM.SDR SWAA093257Flap · delaminatedDURING SCHEDULED 22Y CHECK, FOUND RT WING O/B MID FLAP DELAMINATED. R&R MID FLAP PER MM.SDR SWAA093256Flap · delaminatedDURING SCHEDULED 22Y CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED LOWER O/B END. R&R AFT FLAP PER MM.SDR USAA2009060491399Housing · corrodedCLT - Q1 - MAJOR REPAIR - CORROSION ON RIGHT INBOARD MID FLAP, INBOARD OUTBOARD FLIGHT ROLLER BEARING HOUSING BORE SURFACE. REPLACED RIGHT INBOARD MID FLAP IAW US AIRWAYS TASK CARD 03C40927012.SDR FDEA200905181715Skin · misrepairedLEFT WING, EXISTING REPAIR FOUND ON INBOARD FLAP UPPER SURFACE AT BETWEEN XIFH 122 TO XIFH 140. EXISTING REPAIR EVALUATED AND FOUND NOT CARRIED OUT IAW SRM 57-10-00 FIG.39 VOL.1 REV.40. REPAIR CARRIED OUT AS PER SRM 57-10-00 FIG.39 VOL.1 REV.40. (MAJOR REPAIR
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