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 FDEA201205051744Hinge Fitting · corrodedLEFT WING FLAP SIDE HINGE FOUND CORRODED. CORROSION REMOVED AND FOUND TO EXCEED LIMITS IAW CMM 57-52-03, REV 72 EXISTING HOLE DIA : 1.220", FINAL HOLE DIA: 1.248" , MAX ALLOWABLE DIA : 1.220" REPAIR ACCOMPLISHED IAW EA NR 1-5750-160604 PART 1. REPAIR CLASSSSDR FDEA201205041741Skin · gougedLEFT WING CENTER FLAP UPPER SURFACE MID SECTION BETWEEN RIBS 13 TO RIBS 15 AND BETWEEN STRINGERS 2.5 & 2.7 HAS SIX GOUGES. REPAIRED IAW FSRM 57-50-00, FIG 205, PAGE 216-219.SDR IPXA2673453Skin · delaminatedINSPECTION TYPE: 9C, RT WING INBD AFT FLAP INBD LOWER AREA FOUND DELAMINATED. METAL HOT BOND REPAIR PERFORMED IAW SRM 51-70-10-2R, REPAIR 4, FIG 201, SHEET 1, REV 52.SDR FDEA201205041739Skin · chafedRIGHT WING INBD FLAP TOP SIDE MIDDLE FWD AREA HAS 2 EA .75 SQUARE INCH CHAFED AREAS WITH BARE METAL SHOWING. REPAIRED RT INBD FLAP UPPER SURFACE AT RIBS 14 TO 17 STR 2.1 TO 2.2 IAW FSRM 57-50-00, FIG 206.SDR AALA20120504007Skin · debondedDISBOND ON LEFT OUTBOARD FLAP LOWER SURFACE. ACCOMPLISHED BONDED REPAIR PER SRM 57-53-01.SDR FDEA201205041737Skin · damagedLT WING CENTER FLAP TOP SKIN HAS AN EXISTING REPAIR DOUBLER WITH GOUGES. REMOVED DOUBLER IAW SRM 51-40-21 ID MATERIAL AS PO 13-11130 2024T3 CLAD .056 IAW FSRM 51-31-02. LOCATED AND DRILLED DOUBLER IAW FSRM 57-50-00. ALODINED AND PRIMED AND TOPCOATED IAW FSRM SDR FDEA201205041735Skin · dentedLT WING CENTER FLAP L/E 7.5" FROM OTBD EDGE HAS DENT THAT MEASURES APPROX 3.7" X 1.2" X .22" VERIFIED LT WING CTR FLAP L/E DAMAGE OUT OF LIMITS IAW FSRM 57-50-00-101. REPAIRED L/E IAW FSRM 57-50-00.SDR FDEA201205031731Skin · dentedLT WING OTBD FLAP L/E TOP EXTERNAL SKIN 77.5" FROM INBD EDGE HAS A DENT MEASURING APPROX 6.0" X 14". R & R REPAIR DOUBLER IAW SRM 57-50-00-21 PARA 4H, REPROTECTED AREAS IAW SRM 51-21-10 AND 51-75-10 LT WING OTBD FLAP L/E SKIN 75.5" FROM INBD EDGE.SDR IPXA12573623Skin · delaminatedINSPECTION TYPE: C, LEFT WING INBD AFT FLAP UNDER SIDE INBD EDGE IS DEAMINATED. REPAIRED FLAP IAW SRM 51-70-04 CURED AT 350 DEGREE FOR 150 MINUTES.SDR FDEA201205021705Hinge Bracket · corrodedDURING FLOURESCENT PARTICLE INSPECTION, FOUND CORROSION ON LT WING INBD FLAP OTBD AFT HINGE BRACKET PIVOT INBD LUG HOLE. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-52-03, REV 72. REPAIR ACCOMPLISHED IAW EA 1-5750-157194. REPAIR CLASSIFIED AS MAJOR IAW GMM 6SDR FDEA201205021704Hinge Bracket · corrodedDURING FLOURESCENT PARTICLE INSPECTION, FOUND CORROSION ON LT WING INBD FLAP OTBD AFT HINGE BRACKET PIVOT OTBD LUG HOLE. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-52-03, REV 72. REPAIR ACCOMPLISHED IAW EA 1-5750-157194 PART 1. REPAIR CLASSIFIED AS MAJOR IASDR FDEA201205021703Bushing · wornLEFT WING INBD FLAP, OTBD AFT HINGE BRACKET PIVOT INBD LUG BUSHING FOUND WORN. BUSHING REMOVED CMM 20-20-07, REV 72, EXISTING HOLE DIAMETER 1.328" , MAX ALLOWABLE DIAMETER 1.220" FOUND EXCEED LIMIT IAW CMM 51-52-03, REV 72. BUSHING FABRICATED AND INSTALLED RSDR FDEA201205021702Bushing · wornLEFT WING INBD FLAP, OTBD AFT HINGE BRACKET PIVOT OTBD LUG BUSHING FOUND WORN. BUSHING REMOVED IAW CMM 20-20-07 REV 72. HOLE MEASURED AND FOUND EXCEED LIMIT IAW CMM 57-52-03, REV 72. BUSHING FABRICATED AND INSTALLED REF EA 1-5750-157194. REPAIR CLASSIFIEDSDR FDEA201205021701Hinge Bracket · corrodedLEFT WING OTBD FLAP, INBD AFT HINGE BRACKET PIVOT INBD LUG BORE, FOUND CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-52-04, REV 72. EXISTING BORE DIAMETER: 1.147", FINAL BORE DIAMETER: 1.1605", MAXIMUM ALLOWABLE DIAMETER: 1.150". REPAIR ACCOMPLISHEDSDR FDEA201205021700Hinge Bracket · corrodedLT WING OTBD FLAP, OTBD FORWARD HINGE BRACKET ACTUATOR ATTACH INBD LUG BORE SPOT FACE FOUND CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-09 REV 72. EXISITING THICKNESS 0.321", REMAINING THICKNESS 0.318", MATERIAL REMOVED 0.003", MINIMUM ALLOWABLSDR AALA20120502007Skin · corrodedCORROSION WAS FOUND ON THE RIGHT INBOARD MAIN FLAP AT THE UPPER SKIN. INSTALLED DOUBLER PER EA B757-57-023402.SDR CA120504002Flap Track · cracked(CAN) ON MAINTENANCE WALKAROUND, THE RT OTBD FLAP HAD MORE PLAY THAN USUAL. FLAP WAS REMOVED AND THE INBD FLAP TRACK WAS FOUND TO BE CRACKED ON THE REAR TIP. TRACK REPLACED AND ACFT RETURNED TO SERVICE.SDR FDEA201205011693Attach Fitting · crackedLEFT WING OTBD FLAP INBD HINGE FWD LT ATTACH FITTING APPEARS TO HAVE A CRACK BETWEEN THE 2ND AND 3RD LOCK FASTENER. REMOVED CRACKED FITTING. LOCATED NEW FITTING AND SPOTFACED PER PRINT B6013. INSTALLED NEW FITTING PER SRM 51-41-01, PRINT B6013,SRM 51-33-01SDR SWAA2012060404567Skin · puncturedLEFT WING I/B AFT FLAP LOWER SURFACE PUNCTURED. REPAIRED AFT FLAP PER SRM.SDR ABXA20120430345Beam · wornRIGHT WING OUTBD FLAP I/B HINGE CARRIER BEAM (ATTACHED TO FLAP) WHERE 3-10 LINK ATTACHS TO FLAP I/B FLANGE BOTH BUSHINGS LOOSE IN FLANGE AND I/B BUSHING ON O/B FLANGE LOOSE. REPAIRED ON REA B657-59823, ACFT WAS GROUNDED.SDR NSVA20120429526Panel · dentedITEM NR 4 ON LT FLAP PANEL HAS A DENT THAT IS DISBONDED AND REQUIRES REPAIR. REPAIRED IAW TD340-57-1-03.SDR SWAA2012051403994Flap · delaminatedLEFT WING O/B AFT FLAP DELAMINATED AT I/B TRAILING EDGE. REPAIRED AFT FLAP IAW SRM.SDR DALA1226930181Hinge Fitting · crackedRT WING I/B AFT FLAP FWD HINGE ARM IS CRACKED AND REPAIRED PER B767-300 SRM 57-53-02 FIG 201 REPAIR 1.SDR FDEA201204261625Skin · dentedLEFT WING OTBD FLAP LOWER SURFACE SKIN BET X-467 AND X-478 HAS SEVERAL DENTS. FOUND DENTS OUT OF LIMITS IAW SRM 51-80-01, VOL II AND 57-10-00, VOL I. REPAIRED DAMAGED AREA IAW SRM 57-10-00, FIGURE 7. MAJOR REPAIR.SDR SWAA2012043003568Flap · delaminatedRT WING O/B AFT FLAP INBD T/E CORNER DELAMINATED. REPAIRED AFT FLAP IAW SRM.SDR SWAA2012043003567Flap · delaminatedLT WING O/B AFT FLAP INBD T/E CORNER DELAMINATED. REPAIRED AFT FLAP IAW SRM.SDR FDEA201204261615Skin · damagedLT INBD FLAP LOWER SKIN HAS GRAVEL DAMAGE. REPAIRED LEFT INBD FLAP LOWER SKIN DAMAGE IAW SRM 57-10-00, 57-00-01, FIG 3 AND 51-31-01. MAJOR REPAIR.SDR LR7A2012042500377Skin · crackedDURING SCHEDULED B-3, FOUND LT OTBD FLAP LOWER SKIN CRACKED AT OWS 265. REPAIRED IAW SMP583, FIG 57-70-10.SDR DALA1226819230Flap · puncturedMAINTENANCE FOUND SMALL PUNCTURE IN LEFT WING INBOARD FLAP 30 INCHES FORWARD OF TRAILING EDGE AND 44 INCHES OUTBOARD OF FUSELAGE. COMPLIED WITH ERA 502781-14 REV 0 TEMPORARY REPAIR.SDR DALA1226360181Skin · delaminatedLT WING I/B AFT FLAP LWR SURFACE IS DELAMINATED AND REPAIRED PER B767-300 SRM 57-53-01 REPAIR 1 FIG 201 AND 51-70-10 REPAIR 4 FIG 201 SHT 1.SDR DALA1226330181Fairing · delaminatedLT WING I/B MAIN FLAP O/B L/E FAIRING IS DELAMINATED AND REPAIRED PER B767-300 SRM 57-53-01 REPAIR 1 TABLE 1 AND 51-70-05 PAR 5A(1) FIG 5.SDR CHQA20120424140Skin · debondedDURING INSPECTION, THE RIGHT INBOARD FLAP TRAILING EDGE AND LOWER SKIN WERE FOUND TO BE DISBOUND. MAINTENANCE REPAIRED THE RIGHT INBOARD FLAP TRAILING EDGE UPPER AND LOWER SKIN IN ACCORDANCE WITH ETD 2012-145-005883 REVISION B.SDR SWAA2012043003583Flap · delaminatedRIGHT WING OUTBOARD AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR AALA20120424010Skin · puncturedLEFT OUTBOARD FLAP UPPER SURFACE HAS PUNCTURE 83 1/2 INCHES FROM INBOARD END. ACCOMPLISHED BONDED REPAIR PER SRM 57-53-01-2R.SDR AALA20120424008Skin · puncturedLEFT OUTBOARD FLAP UPPER SURFACE HAS PUNCTURE 70 3/4 INCHES FROM INBOARD END. ACCOMPLISHED BONDED REPAIR PER SRM 57-53-01.SDR AALA20120424007Skin · damagedLEFT OUTBOARD FLAP UPPER SURFACE HAS PUNTURE 56 3/4 INCHES FROM INBOARD END. ACCOMPLISHED BONDED REPAIR PER SRM 57-53-01.SDR DALA1225990181Fairing · delaminatedLT WING O/B FLAP MID L/E FAIRING IS DELAMINATED AND REPAIRED PER B767-300 SRM 57-53-01 REPAIR 1 TABLE 1 AND 51-70-03 PAR 5A(1) FIG 5.SDR AALA20120424002Flap · delaminatedLEFT OUTBOARD AFT FLAP HAS DENTED AREA LOCATED APPROXIMATELY 131.5 INCHES FROM INBOARD END OF FLAP. INSTALLED HOT BONDED REPAIR DOUBLER PER SRM 51-70-10.SDR AALA20120424001Flap · delaminatedLEFT OUTBOARD AFT FLAP HAS DELAMINATED AREA LOCATED APPROXIMATELY 69.50 INCHES FROM INBOARD END OF FLAP. INSTALLED HOT BONDED REPAIR DOUBLER PER SRM 51-70-10.SDR VNAA2012042500012Skin · dentedDURING SCHEDULED MAINTENANCE A DENT WAS FOUND ON RIGHT INBOARD FLAP SKIN. THE RIGHT INBOARD FLAP SKIN WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.SDR IPXA12M73586Skin · gougedINSPECTION TYPE: 4C, LEFT INBD FLAP, OTBD T/E WEDGE LOWER SKIN GOUGED AT XIFM.276. FABRICATED AND INSTALLED REPLACEMENT SKIN SECTION ON LOWER SURFACE OF LEFT INBD FLAP IAW SRM 57-50-01, REPAIR 1, FIG 201.SDR SWAA2012051403982Flap · crackedLEFT WING INBOARD RIB FORE FLAP CRACKED AT WBL 355. REMOVED AND REPLACED FORE FLAP IAW AMM.SDR A6WA201240481Vane · chafedLEFT INBD FLAP VANE L/E IS CHAFED IN 3 PLACES. R & REINSTALLED 1 EA SERVICEABLE SKIN PN 601R14303-535 ALSO REPAIRED CENTER AND OTBD AREAS IAW REO 601R-57-52-004, REV C.SDR AALA20120421001Flap · damagedLEFT INBOARD AFT FLAP HAIL DAMAGED. REPAIRED FLAP ASSEMBLY PER ESO 90252 AND EA COMP-57-022935.SDR A6WA201240480Vane · chafedRT INBD FLAP VANE IS CHAFING IN 3 EA PLACES. REPAIR IAW REO 601R-57-52-004, REV C.SDR AALA20120426028Skin · dentedRIGHT WING INBOARD MID FLAP UPPER SURFACE DENTED CLUSTER IN THE CENTER. ACCOMPLISHED BONDED REPAIR PER SRM 57-53-01.SDR SWAA2012042603451Skin · puncturedRIGHT WING INBOARD AFT FLAP LOWER SURFACE PUNCTURED. REPAIRED AFT FLAP IAW SRM AND AMM.SDR SWAA2012042603450Flap · delaminatedLT WING O/B AFT FLAP, INBOARD TRAILING EDGE DELAMINATED. REPAIRED AFT FLAP PER SRM.SDR USAA2012042400023Flap · delaminatedPILOT REPORT - LEFT TRAILING FLAP DELAMINATED. REPLACED LEFT OUTBOARD AFT FLAP IAW B737 AMM27-51-34-825-001. OPS CHECK GOOD.SDR FDEA201204191497Structure · damagedAFTER REMOVAL OF THE PANEL FOUND 2EA DAMAGED HOLES ON THE RT WING OTBD FLAP. APPROX BETWEEN STA 565 & 590. COMPLIED WITH EA F-5750-160553. MAJOR REPAIR.
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