JASC 5753
Service difficulty reports · 31,496
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 DALA2024121111653Skin · damagedSHIP 1200 L/H WING O/B FLAP UPPER SURFACE FOUND SWELL AT 46' TO I/B EDGE AND 26' TO AFT EDGE. CORRECTIVE ACTION: REPAIRED L/H WING O/B FLAP UPPER SURFACE SWELL AT 46'' TO I/B EDGE AND 26'' TO AFT EDGE AS PER B767-300 SRM 51-70-10 (0700510)SDR FDEA202412071779Wedge · damagedRH WING, MAIN FLAP TRAILING EDGE WEDGE AT THE OUTBD END OF THE EXTENSION HAS COMPOSITE DAMAGE AND DENT. REMOVED RH WING MAIN FLAP TRAILING EDGE WEDGE AT THE OUTBD IAW SRM 51-40-02. REPAIRED FLAP WEDGE IAW SRM 51-70-10-2R REPAIR 4. REINSTALLED RH WING MAIN SDR SWAA2024120974494Skin · delaminatedLEFT WING OUTBOARD TRAILING EDGE FLAP DELAMINATED(MARKED).<[01] REMOVED AND REPLACED L/H O/B AFT FLAP IAW AMM 27-51-22.;[02] C/W INSPECTIONSDR VNAA20250127010Skin · nickedSEVERAL NICKS ON INBOARD FLAP OF INNER FACE AT RH AND LH WING BTWN FLS 15.00/FLS 77.00. SEVERAL NICKS ON INBOARD FLAP OF INNER FACE AT RH AND LH WING BTWN FLS 15.00/FLS 77.00 WERE BLEND OUT PER CRJ700 SRM 51-12-00-001-001-A01 AND WERE EVALUATED WITHINN LSDR JJBA20241209017Bracket · corrodedINBD L-SHAPE BRACKET FOUND HEAVY CORROSION ON LH INBD FLAP. INBD L-SHAPE BRACKET ON LH INBD FLAP BLENDED OUT OF LIMIT. LH INBD FLAP INBD L-SHAPE BRACKET REPLACEDSDR AALA202412169904Skin · delaminatedAIRCRAFT IN BASE MAINTENANCE: LEFT HAND WING OUTBOARD AFT FLAP INBOARD UPPER SURFACE HAS DELAMINATION ACCOMPLISHED PERMANENT REPAIR ON LEFT HAND WING OUTBOARD AFT FLAP INBOARD UPPER SURFACE. PER B737-NG SRM 57-53-01-2R-14, SRM 51-70-10-2R REPAIR GENERAL, AND SSDR UIEA2024120301162Seal · damagedRIGHT O/B T/E FLAP WITH SEAL DAMAGED AT INBOARD SIDE.(<P>REMOVED DAMAGED SEAL AT R/H O/B T/E FLAP, I/B SIDE AREA, LOCATED, CLEANED, PREPARED, SECURED AND INSTALLED NEW SEAL AS REQUIRED AT R/H O/B T/E FLAP, I/B SIDE AREA PER BOEING 767-300 AMM 57-25-01-05 & AMMSDR DALA2024120311389Flap Track · corrodedSHIP 3133 CORROSION ON #2 RT WING FLAP TRACK ATTACHMENT POINT FOR FAIRING. CORRECTIVE ACTION: REMOVED ATTACH TUBE FROM FLAP TRACK FAIRING. REMOVED ATTACH TUBE FROM FLAP TRACK STRUCTURE. INSTALLED NEW TUBE AND HARDWARE PER A319 AMM 57-55. (6643136)SDR WRXR20241203004Panel · damagedGOUGE FOUND ON R/H I/B PANEL 684JB 1 5/16" X 1/16", .009 DEEP. BLENDED RH I/B PANEL 684JB IAW CRJ700 SRM 51-12-00-001-001-A01. NDI NO CRACKS. REPAIRED IAW REO 670-57-52-583, REV --.SDR WRXR20241203003Panel · chafedCHAFING FOUND ON L/H I/B PANEL 584HT. BLENDED LH I/B PANEL 584HT IAW CRJ700 SRM 51-12-00-001-001-A01. NDI NO CRACKS. REPAIR COMPLIED WITH IAW EA A1-670-57-00079.SDR WRXR20241203002Skin · chafedCHAFING FOUND ON R/H I/B PANEL 684LB. PERFORMED BLENDING ON RH I/B PANEL 684LB IAW CRJ700 SRM 51-12-00-001-001-A01. NDI, JOB NO. K211024, NO CRACKS NOTED. PERFORMED REPAIR IAW REO 670-57-52-582, REV --.SDR WRXR20241203001Panel · chafedCHAFING FOUND ON LH I/B FLAP PANEL 584EB. PERFORMED BLENDING ON LH I/B FLAP PANEL 584EB IAW CRJ700 SRM 51-12-00-001-001-A01. PERFORMED NDI, NO CRACKS NOTED.SDR AALA202502263035Doubler · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION OB FLAP LOWER EXTERNAL DOUBLER LOCATED BTW RIB 14 AND RIB 15 ON RH WING L=3.387 INCH W= 1.842INCH D= 0.026 INCH. MAINTENANCE REPLACED DOUBLER EXTERNAL LOCATED ON OB FLAP LOWER BTW RIB 14 AND RIB 15 ON RH WING IAW A320 SRSDR AALA202502247352Skin · wornAIRCRAFT WAS GROUNDED: GOUGE (WEAR) SLAT 3 LOCATED ON TRAILING EDGE LOWER SURFACE I/B SIDE RH WING MEASURES OF WEAR ARE L=2.0INCH, W=0.340INCH, D=0.018INCH. MAINTENANCE ACCOMPLISHED PERMANENT REPAIR DOUBLER LOC BETWEEN I/B RID DATUM AND TRACK RIB 7 DATUM TRAILSDR SWAA2025010273163Angle · crackedCRACK SUPPORTS ANGLE TRAILING EDGE LOCATED ORSS287 AFT POSITION AT RT WING 2024-728574<[01] REPLACED SUPPORTS ANGLE TRAILING EDGE LOCATED ORSS287 AFT POSITION AT RT WING IAW B737-800 SRM 51-40-02-0G AND DWG 115A3700 SHEET 72 REV -;[02] REPLACED SUPPORTS ANGLE SDR SWAA2024120272824Flap · delaminatedRH INBOARD AFT FLAP DELAMINATED.<[01] R&R RH INBOARD AFT FLAP REF AMM 27-51-12. OPS TEST AND RIG CHECK GOOD.;[02] RII- VERIFIED INBOARD AFT FLAP INSTALLATION AND RIG.SDR UIEA2024112901132Seal · damagedRH INBOARD MID FLAP , MID FLAP WITH SEAL DAMAGED AT INBOARD SIDE(<P>REMOVED DAMAGED AREA AT SEAL LOCATION BY RH INB. MID FLAP, INBOARD SIDE, CLEANED, PREPARED, APPLIED SEALANT AND INSTALLED RE-INFORCEMENT FABRIC AS REQUIRED PER BOEING 767-300 AMM 52-09-00-358-SDR UIEA2024112801124Seal · damagedRH OUTBOARD FLAP WITH SEAL DAMAGED AT INBOARD SIDE(<P>REMOVED DAMAGED SEAL AT INBOARD SIDE BY R/H OUTBOARD FLAP AREA, LOCATED, CLEANED, PREPARED, TRIMMED, SECURED AND INSTALLED NEW SEAL AS REQUIRED, AT R/H OUTBOARD FLAP AREA, BY INBOARD SIDE, PER BOEING 767-30SDR UIEA2024112801123Seal · damagedLEFT O/B FLAP WITH SEAL DAMAGED AT INBOARD SIDE(<P>REMOVED DAMAGED SEAL AT L/H O/B FLAP, BY I/B SIDE AREA, LOCATED, CLEANED, PREPARED, SECURED, TRIMMED, SECURED AND INSTALLED NEW SEAL, AS REQUIRED, AT L/H O/B FLAP, BY I/B SIDE AREA, PER BOEING 767-300 AMM 20-SDR DALA2024113011283Roller · wornSHIP 3145 WEAR ON CRUISE ROLLER OB FLAP ON LH WING. CORRECTIVE ACTION: REPLACED CRUISE ROLLER OB FLAP ON LH WING A319 CMM 57- 53-21 TASK 57-53-21-000-810-A01. (0683395)SDR SWAA2024121872389Panel · crackedCRACK ON SUPPORT PANEL #561AB.<[01] REMOVE AND REPLACED SUPPORT PANEL #561AB IAW SRM 51-40-02-0G-0. STEP 4.B;[02] VERIFIED CORRECTIVE ACTION ENTRY 1.SDR LR7A2024112603694Rib · crackedDURING SCHEDULED C-10 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LH OUTBOARD FLAP UPPER MIDDLE RIB CAP CRACKED AT OWFS30-33. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 57-70-08. NR# 0624. / PSE# 57-50-16, AD 2012-06-09SDR LR7A2024112603631Skin · crackedDURING SCHEDULED C-10 CHECK UNDER JOB CARD HC5711, FOUND LH OUTBOARD FLAP UPPER TRAILING EDGE SKIN CRACKED AT OWFS332L. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0219.SDR LR7A2024112603630Skin · crackedDURING SCHEDULED C-10 CHECK UNDER JOB CARD HC5711, FOUND LH OUTBOARD FLAP LOWER CENTER SKIN CRACKED AT OWFS286L. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0218.SDR LR7A2024112603629Skin · crackedDURING SCHEDULED C-10 CHECK UNDER JOB CARD HC5712, FOUND RH OUTBOARD FLAP UPPER CENTER SKIN CRACKED AT OWFS102R. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. NR# 0215. / PSE# 57-50-16, AD 2012-06-09SDR SWAA2024122071578Flap · delaminatedR/H WING O/B AFT FLAP DELAMINATED AT THE I/B AFT CORNER.<[01] REMOVED DELAMINATED R/W I/B AFT FLAP (PN:113A3700-28 SN:005141); RECEIVED NEW R/W I/B AFT FLAP (PN:113A3700-8 SN:000362); FOUND TO BE BAD FROM STOCK. R/W I/B AFT FLAP (PN:113A3700-8 SN:000362) TO BESDR SWAA2024123171318Skin · debondedCUSTOMER REQUEST - DEBONDED OB AFT FLAP ON IB SIDE AT LT WING. REPAIRED OB AFT FLAP ON IB SIDE AT LT WING IAW B737-800 SRM 57-53-01-2R-16 REPAIR 16.SDR IPXA2024112675606Skin · crackedFOUND TWO CRACKS GENERATING FROM ACCESS HOLE ON LEFT SIDE INBOARD FORE FLAP, OUTBOARD END , TOP LEADING EDGE SURFACE. ALL STEPS OF REPAIR EO-92183 CWSDR SWAA2024122070685Panel · crackedSTA 540 B.LINE 0 PANEL BRAKER LEFT AND RIGHT CORNER HAS CRACK. DOT P833<[01] REMOVED AND REPLACED 2 EACH PANEL BREAKS REF BAC DWG 143A0060 REV - AND B737-NG 51-40-02;[02] REMOVED AND REPLACED 2 EACH PANEL BREAKS REF BAC DWG 143A0060 REV - AND B737-NG 51-40-02SDR DALA2024112511162Skin · dentedSEVERAL DENTS ON SKIN OF AFT MOVABLE FLAP VANE GUIDE AT RH WING. SUMMARY OF NRC 00196: AFT RH FLAP VANE WAS REPLACED PER AMDS 2750-4008. (LP #0670862)SDR DALA2024112211142Bearing · corrodedSHIP 3132 RH WING / INB FLAP / TRACK 2 BEARING AT RIB 9 LEVEL / INB & OUTB PLATES / CORROSION. CORRECTIVE ACTION: COMPLIED WITH ERA 618466-14 REV A. (0671062)SDR SWAA2024112561668Skin · delaminatedLEFT WING OUTBOARD TRAILING EDGE FLAP HAS A 6' X 6' DELAMINATION ON THE UPPER INBOARD SURFACE.<[01] ACCOMPLISHED TEMP REPAIR TO LW OTBD AFT FLAP DELAMINATION PER EA 24-127-03237 REF TASK ID # TTG8Q00X68ZX.;[02] CORRECTION; ACCOMPLISHED INTEREM REPAIR AS DESCRISDR SWIA2024112500020Skin · damagedRH OTBD FLAP UNDER WING SKIN HAS CREASING DUE TO BIRD STRIKE DAMAGE. REPAIRED RH OTBD FLAP UNDER WING SKIN IAW SRM 57-53-01 TYPE 3 REPAIR.SDR SWIA202411210001Skin · damagedRH OTBD FLAP UNDER WING SKIN HAS CREASING DUE TO BIRD STRIKE DAMAGE. (FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESSSDR DALA2024112111102Hinge Fitting · crackedCRACKED OUTBOARD LOWER BORE OF FLAP HINGE FITTING #3 AT RH WING. RH OUTBOARD WING FLAP HINGE FITTING WAS REMOVED PER B717-200 AMM 57-55-25 000-803 STEP A TO STEP E (2). RH OUTBOARD WING FLAP HINGE FITTING WAS REPLACED & INSTALLED PER B717-200 AMM 57-55-25 400-SDR MASA20241120020Rib · bentRH OUTBOARD FLAP WAS BENT CHAFFED, AND CRACKED. ARRIVED AT C CHECK WITH TEMPORARY REPAIR COMPLIED WITH. PERMANENT REPAIR COMPLIED WITH BY REPLACING RH O/B MAIN FLAP OUTBD RIB15 WITH NEW AS PER RO E175-27-4021R3.SDR FDEA202411201706Skin · erodedLH WING, MID FLAP LEADING EDGE WITH EROSION AT APPROX 23'' THE INBOARD EDGE . LH WING, MID FLAP LEADING EDGE WAS REPAIRED IAW B767 SRM 57-53-01-2R REPAIR 1 FIG.201 SHEET 5 AND SRM 51-70-03-0G PAR.5.A FIG.5 REV.90 AUG 15/2024SDR FDEA202411201703Skin · cracked1EA CRACK (5MM) WAS FOUND AT R/H WING CENTER FLAP RIB27 AFT AREA OF TOP SURFACE RIB FLANGE. PERFORMED CUT OUT DAMAGED FLANGE AND INSTALLED REPAIR ANGLE AT RIB27, S-2.7~S-2.8 AND EXTERNAL PLATE AT RIB26~27,S-2.2~S-2.1 FOR REPAIR I.A.W FEDEX EA NO:T6-5750- SDR FDEA202411201701Skin · cracked1EA CRACK (25MM) WAS FOUND AT R/H WING CENTER FLAP RIB18 AFT AREA OF TOP SURFACE RIB FLANGE. PERFORMED CUT OUT DAMAGED FLANGE AND INSTALLED REPAIR ANGLE AT RIB18, S-2.8~REAR SPAR AND EXTERNAL PLATE AT RIB18~19,S-2.1~REAR SPAR FOR REPAIR I.A.W FEDEX EA NO:TSDR FDEA202411201700Skin · cracked1EA CRACK (25MM) WAS FOUND AT R/H WING CENTER FLAP RIB12 AFT AREA OF TOP SURFACE RIB FLANGE. PERFORMED CUT OUT DAMAGED FLANGE AND INSTALLED REPAIR ANGLE AT RIB12, S-2.7~S-2.8 AND EXTERNAL PLATE AT RIB11~12,S-2.2~REAR SPAR FOR REPAIR I.A.W FEDEX EA NO:T6-57SDR FDEA202411201699Skin · cracked2EA CRACKS (20MM) & (20MM) WERE FOUND AT R/H WING CENTER FLAP RIB11 AFT AREA OF TOP SURFACE RIB FLANGE. PERFORMED CUT OUT DAMAGED FLANGE AND INSTALLED REPAIR ANGLE AT RIB11, S-2.7~REAR SPAR AND EXTERNAL PLATE AT RIB11~12,S-2.2~REAR SPAR FOR REPAIR I.A.W FESDR SWIA202504301119Vane · chafedRH WING, OTBD FLAP VANE MOUNT FITTINGS SHOW CHAFFING AND WEAR ALONG THE LOWER EDGE, AT WS 171, 189, 235, 280, 296, (5EA FITTINGS) (C-CHECK RO 04/30/2025) COMPLIED WITH REO 601R-57-53-195 DISPOSITION FOR WEAR DAMAGE ON O/B FLAPS BUJTE DOOR CAMS AND RIB FITTINGSDR CALA2024112002909Skin · dented9B757-57-06-3-0248) DOT 210-18 R/H WING I/B FLAP O/B SIDE HAS MA RK/DENT. REF NR 114209. REPAIRED FLAP LE SKIN IAW SRM 57-53-01-2R-2. VERIFIED INSPECTION PERFORMED RIISDR CALA2024112002908Skin · gouged(B757-57-06-3-0248) R/H WING MAIN FLAP I/B AT MFSTA 153.43 WITH GOUGE. REF NR 114426. REPAIRED FLAP LE SKIN IAW SRM 57-53-01-2R-2. VERIFIED INSPECTION PERFORMED RIISDR LR7A2024111903603Baffle · crackedDURING SCHEDULED C-5 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RH OUTBOARD FLAP UPPER BAFFLE SKIN CRACKED AT OWFS0R. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. NR# 1001190949.SDR LR7A2024111903602Skin · crackedDURING SCHEDULED C-5 CHECK UNDER JOB CARD HC 5712, FOUND RH OUTBOARD FLAP UPPER LEADING EDGE SKIN CRACKED AT OWFS303R. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-11. NR# 1001188008. / PSE# 57-50-16, AD 2012-06-09SDR HNAA202412010144Hinge Fitting · cracked57-2441 RH OB FLAP SHROUD, IB HINGE AFT SECTION LUG CRACKED. RAR HINGE IAW SRM 51-40-02 AND AMM20-10-01SDR SWI2025F00175Vane · dentedDURING AUDIT OF 1C TASK CARD 57-680-302 (EXTERNAL ZONAL INSPECTION OF THE RIGHT-WING INBOARD FLAP, FLAP VANE, AND HINGE ARMS), FOUND DENT ON UNDERSIDE OF RH INBD FLAP APPROXIMATELY 18 INCHES FROM INBOARD SIDE EDGE AND 5 INCHES UP FROM THE TRAILING EDGE. PLOT, SDR IPXA2025011325354Skin · puncturedRH TRAILING EDGE FLAP HAS PUNCTURE 1.5X1.5€? AND .6€? DEEP. HANGAR REQUIRED FOR COMPOSITE REPAIR. L/M 3.0 HRS TO DROP AND LOCKOUT FLAPS. S/M 40.0 HOURS FOR REPAIR. REF. SRM 57-53-01-2R-2, TABLE 205 ZONE 5. 350 DEGREE COOK (51-70-05). BMS8-256,STYLE3K-70-PW SDR SWAA2024112060413Wedge · debondedLH WING IB MAIN FLAP HAS A METAL BOND REPAIR THAT HAS DISBONDED AND DEPARTED THE AIRCRAFT. LOCATED AT THE LOWER OB END TRAILING EDGE SKIN.<[01] REPAIRED PANEL WEDGE PER SRM 57-53-01-2R-7.
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