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 DALA2022041902721None · noneSHIP 3259 CORROSION BEARING OB FLAP PENDULUM ASSY O/B POSITION ON RH WING. CORRECTIVE ACTION: REPAIRED PER ERA 598347-14 PRI REV ORIGINAL. (2196527)SDR DALA2022041902720None · noneSHIP 3259 CORROSION INTERCONNECTING STRUT IB FLAP TARGET ON RH WING. CORRECTIVE ACTION: REPLACED TARGETS ON INTERCONNECTING STRUT IB FLAP ON RH WING AS PER A320 CMM 57-52-17. (2196139)SDR DALA2022041902718None · noneSHIP 3259 CORROSION BEARING OB FLAP ON PENDULUM ASSY I/B POSITION ON RH WING. CORRECTIVE ACTION: COMPLIED WITH ERA 598568-14 PRI REV ORIGINAL. (2196259)SDR HALA2022041800138None · noneSHIP 374 HOLLOW BOLT ON FLAP TRACK CARRIAGE DAMAGED. CORRECTIVE ACTION: RPLCD DAMAGED BOLT. (6783095)SDR SWAA2022051294054Plate · crackedCRACK PLATE ASSY TRAILING EDGE LOCATED BETWEEN WS204.25 TO WS228.25 RT WING 2022-204374 / [01] REPLACED PLATE ASSY AND FASTENERS LOC. TRAILING EDGE <BR>BETWEEN WS204.25 TO WS228.25 RT WING. I.A.W B737-700 SRM 51-10-02 ITEM 9 AND DWG 115A2001 REV ?A? . ?SEE INDSDR SWAA2022042693874None · brokenFOUND CLIP BROKEN BEHIND PANEL 551FB (CLIP P/N: 115A5552-1) / [01] REMOVED AND INSTALLED ANGLE CLIP AT BEHIND PANEL 551FB LOWER INBOARD FIXED TRAILING EDGE IAW B737-700 SRM 51-40-02-OG-0;[02] VERIFIED; STEP # 1.SDR MASA20220413199None · dentedTHE INBOARD FLAP LOWER SKIN OF THE RH WING WAS FOUND WITH A DENT AT FLS 48.00. PERFORMED PERM REPAIR IAW CRJ700/900 STRUCTURAL REPAIR MANUAL (SRM) 57-52-01, ITEM 28A, D (REV.38 DATED JULY 9TH, 2021 ).SDR SWAA2022051293684Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED WS278.50 APPROX. AT LT WING 2022-204298 / [01] REPLACED ANGLE TRAILING EDGE LOCATED WS278.50 APPROX. AT LT WING IAW B737-700 SRM 51-40-02 SRM 51-10-02 AND DWG 115A6200 REV -;[02] TASK COMPLETEDSDR SWAA2022051293686Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED BETWEEN WS253.00 TO WS278.50 FORWARD POSITION AT LT WING 2022-204290 / [01] REPLACED ANGLE TRAILING EDGE LOCATED BETWEEN WS253.00 TO WS278.50 FORWARD POSITION AT LT WING IAW B737'700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02.SEE INSDR SWAA2022051293685Plate · crackedCRACK PLATE ASSY TRAILING EDGE LOCATED WS204.25 TO WS228.25 LT WING 2022-204285 / [01] REPLACED PLATE ASSY TRAILING EDGE LOCATED WS204.25 TO WS228.25 LT WING IAW B737-700 SRM 51-40-02 <BR>DWG:115A2001 RV:A;[02] CORRECTED STEP 1 <BR>REPLACED PLATE ASSY TRAILINGSDR SWAA2022051293687Plate · crackedCRACK PLATE ASSY TRAILING EDGE LOCATED WS204.25 APPROX. LT WING 2022-204282 / [01] REPLACED PLATE ASSY AND FASTENERS LOC. TRAILING EDGE WS204.25 APPROX. LT WING I.A.W B737-700 SRM 51-10-02 ITEM 9 AND DWG 115A2001 REV ?A? .;[02] CORRECTED STEP 1 : <BR>REPLACED SDR SWAA2022051893294Panel · crackedCRACK ACCESS PANEL 561AB TRAILING EDGE AT LT WING 2022-204193 / [01] TOOL USED: CALIPER P/N: 500-464 S/N: 15331926 DUE DATE: 28-SEP-22.;[02] TOOL USED: HOTBONDER: P/N:HCS9200B S/N:18165044 DUE DATE:28-FEB-23;[03] TOOL USED: SCALE: P/N: SCA-301 S/N: AE-412127 DSDR SWAA2022051293296Bracket · crackedCRACK SUPPORT BRACKET TRAILING EDGE LOCATED ORSS 274 AFT POSITION RT WING 2022-204240 / [01] REPLACED SUPPORT BRACKET TRAILING EDGE AND FASTENERS LOCATED ORSS 274 AFT POSITION RT WING IAW B737-700 51-10-02 AND 51-40-02.;[02] TASK CARD COMPLETEDSDR SWAA2022051293297Bracket · crackedCRACK SUPPORT BRACKET TRAILING EDGE LOCATED ORSS 274 FWD POSITION RT WING 2022-204242 / [01] REPLACED SUPPORT BRACKET TRAILING EDGE AND FASTENERS LOCATED ORSS 274 FWD POSITION RT WING IAW B737-700 SRM 51-10-02 AND 51-40-02.;[02] TASK CARD COMPLETEDSDR IXXA2022050305Torque Tube · wornL/H I/B FLAP #4 TORQUE TUBE FOUND PITTED AND WORN BEYOND LIMITSSDR IXXA2022042801Torque Tube · wornRH I/B FLAP TORQUE TUBE REQUIRES REMOVAL FOR INSPECTION IAW J/C ATI-57-793-12-02 #5 TORQUE TUBE FOUND TO BE PITTED AND WORNSDR DALA2022041102472None · noneSHIP 3270 CORROSION OB FLAP ECCENTRICAL BEARING CORE BOTH SIDE ON TRACK 3 ON LH WING. CORRECTIVE ACTION: COMPLIED WITH ER/A 598395-14 REV. ORIGINAL. (2190042)SDR A6WA202204088484None · noneDENT RH OTBD FLAP UPPER SKIN *****AIRCRAFT REMOVED FROM SERVICE**** REPAIREDSDR DALA2022041302580Vane · dentedDENTS 2EA ON UPPER SURFACE OF UPPER VANE STA XRS 91.000 LH WING (LW). SUMMARY OF NRC 00027: FWD MOVABLE FLAP VANE LH WAS REMOVED AND INSTALLED PER B717 AMM 27-50-03 AND AMDS 2750-4009 ALSO WAS REPLACED UNDER LOG PAGE 2176221. (LP #2188594)SDR SWAA2022041292598Skin · delaminatedL/H INBOARD TRAILING EDGE SHELF PANEL HAS LARGE PUNCTURE IN LOWER SKIN WITH DELAMINATED AREA AROUND THE PUNCTURE / [01] REMOVED PANEL 193CL REF 737 SRM 51-40-02;[02] REMOVED LH MLG DOOR TOP SEAL RETAINER REF 737 SRM 51-40-02;[03] REMOVED LH WING TE SHELF PANELSDR DALA2022041302582Vane · debondedDISBOND OF 1.10 IN X 1.00 IN LENGHT/WIDTH ON OUTBOARD FIXED GUIDE VANE AT RH WING. SUMMARY OF NRC 00239: OUTBOARD FIXED GUIDE VANE AT RH WING WAS REPAIRED PER B717 SRM 57-53-01-2R-1. (LP #2187656)SDR DALA2022040802442None · noneSHIP 3225 CORROSION INTERCONNECTING STRUT IB FLAP ON RH WING. CORRECTIVE ACTION: REPLACED INTERCONNECTING STRUT PER A320 FAM AMM 27-51-44. OK FOR SERVICE. (2187604)SDR DALA2022040802441None · noneSHIP 3225 CORROSION INTERCONNECTING STRUT IB FLAP ON LH WING. CORRECTIVE ACTION: R/R STRUT PER A320 FAM AMM 27-51-44. OK FOR SERVICE. (2187587)SDR SWAA2022050291829Access Panel · crackedCRACK AROUND HOLES ACCESS PANEL 561BB TRAILING EDGE AT LT WING 2022-192804 / [01] TOOL USED: CALIPER P/N: 500-464 S/N: 15331932 DUE DATE: 26-OCT-22.;[02] CORRECTIVE ACTION 1 ENTERED BY ERROR.<BR>CORRECTED TOOL USED IS CALIPER P/N: 500-464 S/N: 15331926 DUE DATSDR FDEA202204060881None · gougedRIGHT WING #9 SLAT UPPER TRAILING EDGE WEDGE LOWER SURFACE IS GOUGED IB OF IB MAIN TRACK. REPAIRED RIGHT WING #9 SLAT UPPER TRAILING EDGE WEDGE LOWER SURFACE GOUGE I/B OF I/B MAIN TRACK IAW B767-SRM-57-43-02-2R REPAIR 1 FIG 201 SHEET 1 AND 2.SDR IPXA2022041981297None · crackedINSPECTION TYPE:4CR/H I/B FLAP I/B TRACK THE 2ND FITTING FROM THE BOTTOM IS CRACKED.REMOVED, REPLACED R/H I/B FLAP ASSY P/N NRC6055-508 IAW MD11 AMM 27-50-20-400-801 (MINOR)SDR DALA2022041002448Skin · puncturedSHIP 1818 FOUND RH WING I/B MAIN FLAP FROM I/B EDGE 105 INCH AND FROM TE 12 INCH 01EA PUNCTURE. CORRECTIVE ACTION: REPAIRED AS PER B767-400 SRM 51-70 (2184460)SDR DALA2022040802444None · noneSHIP 3270 CORROSION SUPPORT BRACKET LOC. RIB15 INTERNAL STRUCTURE ON FLAP TRACK 4 OUTBOARD FLAP ON RH WING. CORRECTIVE ACTION: R/R BRACKET PER A320 AMM 27-54-62. OK FOR SERVICE. (2184764)SDR SWAA2022050291070Panel · debondedCUSTOMER REQUEST - DEBONDED IB MAIN FLAP T/E WEDGE PANEL AT RT WING. 2022-192659 / [01] TOOL USED CALIPER P/N 500-464 S/N 15331926 DUE DATE 28 SEP 22;[02] UT TOOL USED: AUDIBLE BOND TESTER; P/N: S-3; S/N: 064; DUE DATE: 12-JUL-22;[03] TOOL USED HOT BONDER P/N SDR KCSA202204041038Fitting · corrodedLH IB FOREFLAP IB FITTING CORROSIONSDR CALA2022040400864Skin · gougedB757-06-3-0318/LW I/B MAIN FLAP LE HAS GOUGED SKIN STREAMER ATTA CH TRANSCRIBED FROM HAECO GSO NR 9282892. DOT:X170SDR SWAA2022042590342Flap · delaminatedR/W O/B AFT FLAP I/B END UPPER SURFACE IS DELAMINATED / [01] REMOVED R/W O/B AFT FLAP IAW AMM 27-51-22-000-801 STEPS 2.D.;[02] VERIFIED;[03] ACCOMPLISHED PARTS REMOVAL TABLE;[04] R/W O/B AFT FLAP I/B END UPPER SURFACE DELAMINATED AREA WAS REPAIRED ON ATS WORK SDR SWAA2022042090491Flap · debondedLT WING O/B AFT FLAP DISBONDED ON LOWER SURFACE AT I/B T/E / [01] LEFT WING O/B AFT FLAP LOWER SURFACE I/B CORNER WAS REPAIRED ON ATS COMPONENTS JOB # 548604; SWA RO # P2796384-1. L/W O/B AFT FLAP REMOVED AND INSTALLED ON FAULT TTG8Q00BMEUE;[02] VERIFIED CORRESDR DALA2022040102209None · noneSHIP 1818 FOUND OUT DELAMINATION ON RH WING IB FWD FLAP EXTERNAL LOWER SURFACE AT 14 INCHES TO OB EDGE AND 16 INCHES TO TE. CORRECTIVE ACTION: THE DAMAGE LOCATED AT 4 INCHES TO OB PANEL EDGE AND 2 INCHES TO PANEL T/E. ASSOCIATED ER/A 14-598221 (2179165)SDR SWAA2022040590093Flap · delaminatedLH OUTBOARD TRAILING EDGE AFT FLAP DELAMINATED / [01] REMOVED AND REPLACED LH OUTBOARD AFT FLAP REF AMM 27-51-22-400-801. ALL CHECKS GOOD.;[02] INSPECTION C/W REMOVED AND REPLACED LH OUTBOARD AFT FLAP REF AMM 27-51-22-400-801. ALL CHECKS GOOD.;[03] INSPECTION SDR SWAA2022050289869Bracket · crackedR/W T/E PANEL 651FB FWD SIDE 3RD BRACKET FROM O/B END IS CRACKED / [01] REMOVED AND REPLACE R/W T/E PANEL 651FB FWD SIDE 3RD BRACKET FROM O/B END IAW SRM 51-40-02-OG-0 STEP 4.;[02] VERIFIED;[03] VERIFIED CORRECTIVE ACTION 1SDR SWAA2022050289728Bracket · crackedLEFT WING UPPER TRAILING EDGE FIXED PANEL AT DEFLECTION RIB; OUTBOARD WEB SUPPORT CRACKED.(MARKED) / [01] REMOVED AND REPLACED BRACKET PER SRM 51-40-02;[02] INSPECTED THE WORK PERFORMED ON C/A #1; NO DEFECTS NOTED.SDR AALA202204055128Trunnion · wornAIRCRAFT WAS GROUNDED: LEFT WING FLAP TRUNNION FITTING HAS WEAR DAMAGE. **SUPPLEMENTAL REPORT FOR AALA202203315128: REPLACED LEFT HAND #1 FLAP TRACK TRUNNION PER TASK CARD 26L00027003** (CLOSED)SDR DALA2022033102193None · noneSHIP 1819 ON WALK AROUND, FOUND DENT AT LT AFT INBOARD FLAP, CORRECTIVE ACTION: BOTH DAMAGES LOCATED 35.5 INCHES LEFT OF INBD HINGE ASSY AND 5.25 INCHES FROM TRAILING EDGE. DAMAGE WITHIN LIMIT PER B767-400 SRM 57-53 (7872048)SDR DALA202205703187Vane · unknownPD: DELAMINATION AT PREVIOUS REPAIR / CA: REPAIRED THE PREVIOUS REPAIR PER B717 SRM 57-53-01 REL 62.00 - 02/16/22. ESTABLISHED LOG 2226633 FOR REMAINING DENTS ON LWR SURFACE.SDR SWAA2022042589477Bracket · crackedCRACK ON LEFT WING T/E BULB SEAL RETAINER SUPPORT AT ORSS 261; 3'BELOW FROM UPPER PANEL; 20' FWD FROM T/E.(ACCESS FROM 551GB) / [01] REMOVED L. WING T/E BULB SEAL SUPPORT PANEL AND BRACKET IAW SRM 51-40-04 AND AMM 20-50-01 AND LOCATED AND DRILLED NEW BRACKET ISDR FDEA202203290730Support · corrodedRIGHT HAND WING - OUTBOARD FLAP VANE ASSEMBLY . TYPICAL FITTING (B) ECCENTRIC HOLE CORROSION. CORROSION AT RIGHT HAND WING - OUTBOARD FLAP VANE ASSEMBLY . TYPICAL FITTING (B) ECCENTRIC HOLE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57- SDR DALA2022040202243None · noneRIGHT FLAP MOVEABLE VANE FOUND DAMAGE ON THE UNDERSIDE. "M". SUMMARY SEE NRC 001-0364:2753-2003/002 00332: REPLACED RH WING FLAP AFT VANE PER B717 AMDS 2750-4008. ALL RII'S COMPLIED WITH ON AMDS 2750-4008. (LP #2175615)SDR DALA2022040202242None · noneRH MOVEABLE FLAP VANE HAS POSSIBLE DELAMINATION AT PREVIOUS DENT LOCATION. SUMMARY SEE NRC 019-0001:00-0557-8- 9290/001 00211: REPLACED RH FWD MOVEABLE VANE PER AMDS 2750-4010. ALL RII'S COMPLIED WITH ON AMDS 2750-4010. (LP #2175616)SDR FDEA2022032190730Support · corrodedRIGHT HAND WING - OUTBOARD FLAP VANE ASSEMBLY . TYPICAL FITTING (B) ECCENTRIC HOLE CORROSION.SDR SWAA2022041188682Retainer · crackedA-061 DOT 005 R/H WING #6 FWD FLAP TRACK FAIRING 642AB BULB SEAL RETAINER CRACKED / [01] REPLACED BULB SEAL RETAINER ON FWD FLAP TRACK FAIRING 642ABIAW SOPM 20-50-01 STEP 8 AND TABLE 1;[02] JOB COMPLETE; AUDIT C/WSDR SWAA2022032988090Skin · delaminatedOUTBOARD FLAP ON CAPTAINS SIDE UPPER LAYER DELAMINATED / [01] INSPECTION C/W CORRECTIVE ACTION STEPS 1 AND 2.;[02] INSPECTION C/W CORRECTIVE ACTION STEPS 1 AND 2.SDR DALA2022051203288Flap · dented(LOG 2177458) DURING INSPECTION FOUND OUTBOARD AFT FLAP LH, LOWER SURFACE(BTW OTFF 187 59+20 IN) WITH SEVERAL DENTS. OUTBOARD AFT FLAP LH. LOWER SURFACE WAS REPAIRED I.A.W. S.R.M. B737 57-53-01-2R P. 14 PG 1-6 TABLE 201 AND S.R.M. 51-70-10-2R P4 REP 4.SDR SWAA2022041287697Support Angle · crackedR/H WING TRAILING EDGE PANEL#651FB HAS 1EA SUPPORT ANGLE CRACKED. (MARKED) / [01] REMOVED AND REPLACED SUPPORT ANGLE PER SRM 51-40-02.;[02] 1. MICHAEL BALLERT (TECHNICIAN); 31-MAR-2022 12:34 UTC<BR>REMOVED AND REPLACED SUPPORT ANGLE PER SRM 51-40-02SDR MASA20220324119Flap · dentedA DENT WAS FOUND AFFECTING THE SKIN THE LOWER SKIN ON LEFT OUTBOARD FLAP ALONG THE AFT EDGE. .PERFORMED A PERMANENT REPAIR IAW CRJ900 SRM 57-52-01, FIGURE 57-53-01-001-001-A01, ITEM 3. DEFECT LOCATION: LH WING, FS235.96-245.84
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