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 NACA2023033100037Unknown · unknownRH WING INBOARD TRAILING EDGE FLAP LH SIDE SKIN BROKEN. PERFORMED MAJOR REPAIR AT INBOARD TE FLAP AFT FLAP LH SKIN IAW B767 SRM 57-53-01 REPAIR 2.SDR SWAA2023041125949Flap · delaminatedLH INBD TRAILING EDGE FLAP DELAMINATED ON TRAILING EDGE<[01] REMOVED AND REPLACED L/H INBD AFT FLAP; OPS CHECK OK IAW AMM. 27-51-12. REF TTG8Q00K6M7B FOR PART R/R INFOR.SDR AALA202305105458Flap · corrodedAIRCRAFT IN BASE MAINTENANCE: COOROSION ON RIGHT WING OUTBOARD TRAILING EDGE FLAP LEADING EDGE AT THE #4 TRACK INTERNAL AREA . REPLACED FLAP PER TASK CARD 26L00027009SDR DALA2023033102475Unknown · unknownAIRCRAFT 9571, INITIAL INSPECTION: BROKEN BRACKET INSIDE ACCESS PANEL NBR 530AF ON FLAP AT LH WING. CORRECTIVE ACTION: BRACKET INSIDE ACCESS PANEL NBR 530AF ON FLAP AT LH WING WERE REPLACED PER B-717-200 SRM 51-41-02-0G AND SRM 51-41-05-0G. (LP 2694546)SDR SWAA2023033021358Rib · crackedRIGHT WING UPPER INBOARD FIXED TRAILING EDGE SEAL RIB CRACKED AND BROKEN<[01] REMOVED AND REPLACED RIGHT WING UPPER INBOARD FIXED TRAILING EDGE SEAL RIB PER SRM 51-40-02SDR IPXA2023032892358Bracket · brokenINSPECTION TYPE:CK1CR/H WING CENTER FLAP O/B EDGE HAS BROKEN BRACKET.REMOVED AND REPLACED BRACKET IAW SRM 51-40-21.SDR U2RA2023040300017Flap · crackedDURING SCHEDULED INSPECTION, FOUND CRACK ON THE R/H INBOARD FORE-FLAP THAT EXCEEDS ALLOWABLE DAMAGE LIMITS IN B747 SRM 57-53-01-0I-1 FIGURE 1: CRACK LOCATION AT RWBL 360, ON NOSE RIB SPLICE ANGLE. REMOVED AND REPLACED FORE-FLAP ASSEMBLY.SDR U2RA2023040300016Flap · crackedDURING SCHEDULED INSPECTION, FOUND CRACK IN L/H OUTBOARD FORE-FLAP INTERNAL SHEAR-TIE WEB EMANATING FROM LOWER EDGE THAT EXCEEDS LIMITS PER B747 SRM 57-53-02-0I-1 FIGURE 1, @ RIB #6 AND LWBL 305 APPROXIMATE. REMOVED AND REPLACED FORE-FLAP ASSEMBLY.SDR VNAA202302040001Skin Panel · nickedSEVERAL NICKS ON LOWER/FWD FACE OF LH/RH INBOARD FLAP FROM FLS 15.00 TO FLS 65.50SDR LR7A2023032403275Skin · crackedDURING SCHEDULED B-3 CHECK UNDER JOB CARD HB2703, FOUND RH OUTBOARD FLAP UPPER CENTER SKIN CRACKED AT OWFS30-34R. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. NR# 1000916300. / PSE# 57-50-16, AD 2012-06-09SDR UATA202306013481Fairing · looseUPON SCHEDULED MAINTENANCE INSPECTION, FOUND FIBERGLASS FLAP HINGE FAIRING LOOSENED, AND SUBSEQUENTLY CHAFED THE FLAP ATTACH PYLON BEYOND LIMITS.SDR DALA2023032702323Unknown · unknown(LOG 9913737) DURING INSPECTION FOUND RT WING #6 FLAP SUPPORT AFT FAIRING OB SIDE MISSING. RT WING #6 FLAP SUPPORT AFT FAIRING OB SIDE MISSING. REPAIRED PER ERA 519351-14.SDR DALA2023032402299Unknown · unknownSHIP 6808 DAMAGE TO THE RH INBD MAIN FLAP CAUSE BY DEBRIS FROM THE #7 AND #8 TIRES BLOWING OUT. CORRECTIVE ACTION: DAMAGE CONSISTS OF A CRACK MEASURING 4"X3.5" ON THE BOTTOM OF THE FLAP. C/W SECTION I: TIME LIMITED REPAIR PER RI 607277-14 REV ORIG. REF ERA 607SDR ABXA2023051599Skin · corrodedDURING C21 MAINTENANCE CHECK AT HAECO AMERICAS, AIRCRAFT MAINTENANCE DISCOVERED (2 EA.) AREAS OF CORROSION ON THE LOWER OUTER SKIN PANEL (P/N 113T3143-3) OF THE LEFTWING OUTBOARD FLAP ASSEMBLY (P/N 113T3100-77, S/N 000664) CURRENTLY INSTALLED ON AIRCRAFT N219CSDR SWIA202305190003Vane · corroded*R/H INBOARD FLAP VANE MOUNTING STRUCTURE INBOARD HAS EVIDENCE OF CORROSION. (C-CHECK RO 5/15/2023) DUE TO EXTENSIVE REPAIRS REQUIRED ON EXISTING R/H INBD FLAP, R/H INBD FLAP ASSY REPLACED ON JOB 2787291 OP-181 MXTRANS-26359905 TRANSFERRED TO PART DISCRSDR SWAA2023032117555Fairing · crackedRH WING O/B AFT FLAP; #8 AFT FLAP TRACK LOWER FAIRING IS CRACKED.<[01] REMOVED AND REPLACED LOWER FAIRING IAW SRM 51-40-02. RIVETS REQUIRE PAINT TOUCH UP.;[02] APPLIED TOUCH UP PAINT PER SRM 51-40-02-0G-0-A00729SDR SWAA2023041017155Retainer · corrodedRH INBOARD FLAP ;RETAINER CORRODED.<[01] RECEIVED NEW RETAINER FROM R/H I/B FLAP PER SRM 51-40-02;[02] CORRECT STEP 1. RECEIVED NEW RETAINER FROM R/H I/B FLAP;[03] VERIFIED NEW RETAINER INSTALLED ON CLOSE CARD.SDR SWAA2023040717429Flap · delaminatedL/H OUTBOARD AFT FLAP I/B LOWER CORNER DELAMINATED.<[01] REMOVED L/H OUTBOARD AFT FLAP REF AMM 27-51-22;[02] INSPECTED WORK ABOVE;[03] INSTALLED L/H OUTBOARD TRAILING EDGE FLAP;' AFT FLAP ASSY ' IAW AMM 27-51-22-400-801. FROM STEPS 3. (A) UP TO AND INCLUDING 3SDR SWAA2023040717432Flap · delaminatedR/H OUTBOARD AFT FLAP I/B LOWER CORNER SURFACE DELAMINATED<[01] REMOVED R/H OUTBOARD AFT FLAP REF AMM 27-51-22;[02] INSPECTED WORK ABOVE;[03] INSTALLED R/H OUTBOARD TRAILING EDGE FLAP;' AFT FLAP ASSY ' IAW AMM 27-51-22-400-801. FROM STEPS 3. (A) UP TO AND INCLSDR SWAA2023040717436Flap · delaminatedL/H I/B MAIN FLAP TRAILING EDGE WEDGE; LOWER SURFACE DELAMINATED.<[01] REMOVED L/H MAIN FLAP TRAILING EDGE WEDGE REF SRM 57-53-01; AND SOPM 20-50-01;[02] REMOVED L/H I/B MAIN FLAP TRAILING EDGE WEDGE TO F.O.M.;[03] INSTALLED NEW WEDGE PER AMM 20-50-11;[04] VERSDR ASAA2023031543424Skin · delaminatedAFTER FURTHER INSPECTION ON CUSTOMER CARD NUMBER G1761648 FOUND RIGHT HAND I/B FLAP TOP SKIN PREVIOUS REPAIR DELAMINATED 31.5" FROM O/B EDGE GROUNDED - YES. REPAIRED R/H I/B FLAP TOP SKIN PREVIOUS REPAIR DELAM 31.5" FROM O/B EDGE IAW A320-200 SRM 57-52-00-283SDR ASAA2023031542943Skin · delaminatedAFTER FURTHER INSPECTION ON CUSTOMER CARD NUMBER G1761648 FOUND RIGHT HAND I/B FLAP TOP SKIN PREVIOUS REPAIR DELAMINATED 31.5" FROM O/B EDGE GROUNDED - YES. REPAIRED R/H I/B FLAP TOP SKIN PREVIOUS REPAIR DELAM 31.5" FROM O/B EDGE IAW A320-200 SRM 57-52-00-28SDR SWAA2023040516539Plate · crackedWAFFLE PLATE CRACKED UNDER PANEL 651DB R/H WING. (MARKED)<[01] REMOVED AND REPLACED WAFFLE PLATE UNDER PANEL 651DB R/H WING PER SRM 51-40-02;[02] INSPECTED WORK PERFORMED.SDR AALA202303303872Bracket · excess playAIRCRAFT IN BASE MAINTENANCE: RIGHT WING TRAILING EDGE INBOARD FLAP INTERCONNECTING STRUT FITTING / BRACKET BEARING HAS EXCESSIVE PLAY AT RIB 13. REPLACED FITTING / BRACKET PER SRM 51-72-11.SDR NACA2023072001Unknown · unknownLH WING.- OUTBD AFT FLAP LWR PART WITH CORROSION POINT STA WBL 351.0. REMOVED DAMAGED AREA OUTBD AFT FLAP LWR PART STA WBL 351.0 ON LH WING IAW B737 SRM 51-70-10 REV 130. FABRICATED FILLER AND DOUBLER OF CLAD 2024 T3-0.016 IAW SRM 57-53-02, REV 130 APPLIED PRISDR DALA2023031701969Unknown · unknownSHIP 199 FOUND LHW OB FLAP UPR SURFACE BULGE SKIN FROM IB EDGE 18" FROM AFT EDGE 26". CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B767 SRM 57-53 & 51-70. (2668393)SDR AALA202303218214Skin · delaminatedAIRCRAFT IN BASE MAINTENANCE: DELAMINATION OF LEFT OUTBOARD FLAP LOWER SKIN LOCATED AT WS 302.50 TO WS 326.50, WBL 658.17. REPAIRED SKIN PER SRM 57-53-01-2R REPAIR 16.SDR AALA202303211263Skin · delaminatedAIRCRAFT IN BASE MAINTENANCE: DELAMINATION OF LEFT INBOARD FLAP WEDGE LOWER SKIN LOCATED FROM WS 228.25 TO WS 278.50, WBL 658.17. REPAIRED SKIN PER SRM 57-53-01-2R REPAIR 18.SDR DALA2023031401877Unknown · unknownSHIP 694 REPAIR TO RH WING INBOARD MAIN FLAP LEADING EDGE REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 606448-14. CORRECTIVE ACTION: REF ERA 606448-14. (2667311)SDR DALA2023031401874Unknown · unknownSHIP 694 DAMAGE T IN REFERENCE NRC 00612: DENT WAS FOUND AT RH INBOARD MAIN FLAP LOWER NOSE SKIN APROX. MFSTA 227.28. CORRECTIVE ACTION: SUMMARY OF NRC 00614: RH INBOARD MAIN FLAP LOWER NOSE SKIN APROX . MFSTA 227.28 WAS REPAIRED PER PRI 606448-14 REV. 2 AND ESDR AALA202303147368Tab · debondedAIRCRAFT IN BASE MAINTENANCE: LEFT WING FLAP TAB LOWER SURFACE PREVIOUS METAL REPAIR WAS FOUND TO BE DEBONDED BETWEEN TAB RIBS 4 AND TAB HINGE 3B, 107.0 INCHES INBOARD OF OUTBOARD END OF THE FLAP. MAINTENANCE REPAIRED FLAP TAB LOWER SURFACE PER EA 342880.SDR AALA202303148549Tab · debondedAIRCRAFT IN BASE MAINTENANCE: LEFT WING FLAP TAB LOWER SURFACE PREVIOUS METAL REPAIR FOR A DENT WAS FOUND TO BE DEBONDED BETWEEN TAB RIBS 4 AND 5, 30 INCHES INBOARD OF OUTBOARD END OF THE FLAP. MAINTENANCE REPAIRED FLAP TAB LOWER SURFACE PER EA 342880.SDR DALA2023031401852Unknown · unknownINTERFERENCE BETWEEN FITTING TO ATTACH RIGHT WING FLAP MOVABLE VANE CABLE AND PLATE THROUGH UPPER ACCESS PANEL 630AF AT RH WING FLAP INTERNAL STRUCTURE. SUMMARY OF NRC 00105: FITTING TO ATTACH RIGHT WING FLAP MOVABLE VANE CABLE AND PLATE THROUGH UPPER ACCESS PSDR DALA2023031401851Unknown · unknownINTERFERENCE BETWEEN FITTING TO ATTACH LEFT WING FLAP MOVABLE VANE CABLE AND PLATE THROUGH UPPER ACCESS PANEL 530AF AT LH WING FLAP INTERNAL STRUCTURE. SUMMARY OF NRC 00060: FITTING TO ATTACH LEFT WING FLAP MOVABLE VANE CABLE AND PLATE THROUGH UPPER ACCESS PANSDR SWAA2023031615030Flap · delaminatedL/H AFT INBOARD FLAP DELAMINATING<[01] REMOVED LH INBOARD AFT FLAP PER AMM 27-51-12;[02] INSTALLED LH INBOARD AFT FLAP PER AMM 27-51-12;[03] R&R LH INBOARD AFT FLAP PER AMM 27-51-12 OPS CHECK GOOD<BR>TORQUE WRENCH 20-150 SN 0415039670 NEXT CAL DUE JAN 24;[04] SDR SWAA2023031516327Flap Track · looseLEFT WING OUTBOARD AFT FLAP #3 TRACK LOOSE AT AFT ATTACH POINT<[01] REMOVED AND REPLACED LH WING OUTBD AFT FLAP TRACK #3 PER AMM 27-51-26SDR AALA202303138785Trunnion · damagedAIRCRAFT WAS GROUNDED: LEFT HAND INBOARD FLAP TRUNNION DAMAGED, MAINTENANCE REPLACED FLAP TRUNNION PER TASK CARD 26L00027003.SDR GTIA2023031037029Strut · wornWEAR ON OB FLAP INTERCONNECTING AREA IB SIDE ON LH WING. RAF-01 2824485-02 GENERATED. REF AEROMAN NR 2023-47274.-PERFORMED PERMANENT REPAIR LOCATED ON FLAP INTERCONNECTING AREA I/B SIDE ON LH WING IAW EA # 57-0057-23 REV #1, EA # 57-0057-23 REV #2, EA # 57-00SDR GTIA2023031037026Strut · wornWEAR ON OB FLAP INTERCONNECTING AREA IB SIDE ON RH WING. RAF-01 2824485-01 GENERATED. REF AEROMAN NR 2023-47265.-PERFORMED PERMANENT REPAIR LOCATED ON OB FLAP INTERCONNECTING AREA I/B SIDE ON RH WING IAW EA # 57-0056-23 REV #1, EA # 57-0056-23 REV #2, EA # 57-SDR AALA202304261176Attach Fitting · wornAIRCRAFT IN BASE MAINTENANCE: RIGHT WING INBOARD FLAP INTERCONNECTION STRUT AFT ATTACH FITTING BEARING HAS EXCESSIVE PLAY AT RIB 24. REPLACED ATTACH FITTING PER SRM 51-42-11.SDR AALA202304251819Attach Fitting · wornAIRCRAFT IN BASE MAINTENANCE: RIGHT WING FLAP INTERCONNECTING STRUT ATTACH FITTING HAS EXCESSIVE PLAY BEARING ON THE INBOARD FLAP END AT RIB 14. REPLACED ATTACH FITTING PER SRM 51-42-11.SDR DALA2024071807235Skin · dentedDENT & 3/8" HOLE IN FLAP SKIN AFT OF LT MAIN LANDING GEAR. PER ERA 606778-14 REV ORIGINAL, SEC 1 ACCOMPLISHED DETAILED VISUAL INSPECTION, NO DAMAGE BEYOND PUNCTURE, NO LOOSE, MISSING, OR PULLED FASTNERS. COMPLIED WITH PERMANENT REPAIR OF FLAP OF ERA 606778-14 SDR SWAA2023031012965Flap · delaminatedLEFT WING O/B AFT FLAP I/B CORNER IS DELAMINATED 4.3 X 3.1<[01] REMOVED DAMAGED L/W O/B AFT FLAP AND INSTALLED SERVICEABLE L/W O/B AFT FLAP IAW BOEING 737 AMM 27-51-22 UP TO AND INCLUDING STEPS 3.F(5)G).<BR><BR>CONTINUE FROM STEPS 3.G.;[02] COMPLETED INSTALLATSDR SWAA2023041813178Panel · pulledL/W T/E PANEL 561BB HAS SEVERAL PULLED FASTENER HOLE ON AFT END OF PANEL (MARKED)<[01] IDENTIFIED PART AND MATERIAL IAW SRM 57-51-01-0I-1 FIGURES 1+3; TABLE 3; ITEM [9].<BR>FOUND DAMAGE TO FASTENER HOLES TO BE OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 57-51-01-1ASDR AALA202303300609Strut · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING TRAILING EDGE FLAP INTERCONNECTING STRUT BETWEEN WS 4067 AND 5512, BETWEEN RIBS 8 AND 10. REPLACED FLAP INTERCONNECTING STRUT PER AMM 27-51-44.SDR AALA202303303535Strut · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING TRAILING EDGE FLAP INTERCONNECTING STRUT BETWEEN WS 4067 AND 5512, BETWEEN RIBS 8 AND 10. REPLACED FLAP INTERCONNECTING STRUT PER AMM 27-51-44.SDR SWAA2023040512586Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS261 AT RT WING 2023-143011<[01] REPLACED CORRUGATED PLATE ON TRAILING EDGE LOCATED ORSS 261 AT RT WING. IAW B737-700 SRM 51-40-02 AND DWG # 115A2001; SHEET 32 AND REV -.;[02] CORRECTED STEP 1.<BR>REPLACED CORRUGSDR SWAA2023040512588Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS261 AT LT WING 2023-143014<[01] REPLACED CORRUGATED PLATE ON TRAILING EDGE LOCATED ORSS 261 AT LT WING. IAW B737-700 SRM 51-40-02. ?SEE INDIVIDUAL SIGNOFFS BELOW?.;[02] TASK COMPLETED <BR>SEE INDIVIDUAL SIGNOFFSSDR SWAA2023040512589Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED IRSS214 AT LT WING 2023-143016<[01] REPLACED CORRUGATED PLATE ON TRAILING EDGE LOCATED IRSS 214 AT LT WING. IAW B737-700 SRM 51-40-02. ?SEE INDIVIDUAL SIGNOFFS BELOW?.;[02] TASK COMPLETED <BR>SEE INDIVIDUAL SIGNOFFSSDR SWAA2023040512587Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED IRSS214 AT RT WING 2023-143012<[01] REPLACED CORRUGATED PLATE ON TRAILING EDGE LOCATED IRSS 214 AT RT WING. IAW B737-700 SRM 51-40-02 AND DWG # 115A2001; SHEET 32 AND REV -.;[02] REPLACED CORRUGATED PLATE ON TRAILIN
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