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 P5CA2021053000199Fairing · delaminatedRH O/B FORE FLAP L/E FAIRING FOUND DELAMINATION(<P>PERFORMED PERMANENT HOT BOND REPAIR AS PER SRM51-70-07 PARA 5.A</P>)SDR P5CA2021053000200Fairing · delaminatedRH O/B FORE FLAP L/E FAIRING FOUND DELAMINATION (COUNT FROM I/B EDGE 138.5")(<P>PERFORMED PERMANENT HOT BOND REPAIR AS PER SRM51-70-07 PARA 5.A</P>)SDR P5CA2021060400224Fairing · delaminatedLHW O/B FORE FLAP L/E FAIRING FOUND DELAM (COUNT FROM I/B EDGE 42")(<P>PERFORMED PERMANENT COMPOSITE HOTBOND REPAIR IAW SRM 51-70-07</P>)SDR P5CA2021060400225Fairing · delaminatedLHW O/B FORE FLAP L/E FAIRING FOUND DELAM (COUNT FROM I/B EDGE 62")(<P>PERFORMED PERMANENT COMPOSITE HOTBOND REPAIR</P>)SDR P5CA2021060400226Fairing · delaminatedLHW I/B FORE FLAP L/E FAIRING FOUND DELAM (<P>PREFORMED PERMANENT COMPOSITE HOTBOND REPAIR</P>)SDR P5CA2021061400238Skin · chafedRHW #17 VC FLAP BULLNOSE SKIN CHAFE ON O/B EDGE(<P>RHW #17 VC FLAP BULLNOSE SKIN CHAFE ON O/B EDGE DAMAGE AREA TRIM OFF REPAIRED IAW RI-57-00-14635 REV A.</P>)SDR P5CA2021061400239Seal · puncturedLHW I/B FORE FLAP COMPRESSION SEAL RIB PUNCTURE(<P>LHW I/B T/E FORE FLAP COMPRESSION SEAL RIB P/N: 65B08466-29 DAMAGED AREAS REPAIRED IAW RI-57-55-14642 REV A.</P>)SDR AALA202107239977Tab · debondedAIRCRAFT IN BASE MAINTENANCE: RIGHT WING TRAILING EDGE FLAP TAB EXISTING REPAIR ON THE LOWER SURFACE WAS FOUND TO BE DEBONDED BETWEEN HINGES 3C AND 4 . REPAIRED FLAP TAB LOWER SURFACE PER EA 328780SDR FDEA202106131521Skin · cracked.RH WING OUTBOARD TRAILING EDGE FLAP NOSE SKIN CRACKED , LOC:APPROX 120CM FROM INBD EDGE TO OUTBD EDGE. PERFORMED THE REPAIR ON RH WING OUTBOARD TRAILING EDGE FLAP NOSE SKIN PER B767 SRM 57-53-01-2R AND SRM 51-70-17. THE RSC TRACKING EA # :H-5750-T0362239 SDR SWAA2021071282560Skin · debondedDEBONDED OB AFT FLAP UPPER SURFACE ON IB SIDE AT LT WING. ; 2021-282247 / [01] TOOL USED: HOT BONDER P/N:HCS9200B S/N:18165044 DUE DATE:15-FEB-22; [02] TOOL USED:HOT BONDER P/N:HCS9000B-AV S/N:18164925 DUE DATE:19-NOV-21; [03] TOOL USED CALIPER P/N: 500-197-30SDR SWAA2021070182140Wedge · delaminatedL/H INBD. FLAP OUTBD. AFT WEDGE DELAM. / REPLACED FLAP WEDGE PER SOPM 20-50-01SA-M 326 A1303766INSP D107SDR SWAA2021070182012Support Angle · crackedCRACKED SUPPORT ANGLE IN AFT FLAP WHEEL ATTACHED TO INBOARD SIDE OF RH DEFLECTION CONTROL ARM. / REMOVED AND REPLACED SUPPORT ANGLE AT AFT FLAP R/H I/B OF DEFLECTION RIB PER SRM 51-40-02SDR SWIA2021081860320Skin · out of limitsTHE RH INBD FLAP, THE INBD LOWER SKIN IS OUT OF LIMITS AND REQUIRES REPAIR (C-CHECK RO 8/16/2021) WET INSTALLED NEW -4 EXTERNAL STRAP, -20 INTERNAL STRAP, -30 FILLER, -40 INTERNAL STRAP & -52 LOWER SKIN INSERT ON R/H I/B FLAP I/B LOWER SKIN, REF. CRSDR SWIA2021081860319Skin · out of limitsTHE LH INBD FLAP, THE INBD LOWER SKIN IS OUT OF LIMITS AND REQUIRES REPAIR (C-CHECK RO 8/16/2021) PERFORMED REPAIR ON LH INBD FLAP LOWER SKIN IAW ALL STEPS OF CRJ700 SRM 57-52-01-201-005-A01 SPLICE REPAIR FROM FLS42.00 TO FLS48.00 FIGURE 57-52-01-995-80SDR SWAA2021070186014Plate · crackedCRACK ON PLATE 2E/A OB AFT FLAP AT LT WING ; 2021-255418 / [01] REPLACED PLATE 2E/A LOC. ON OB AFT FLAP AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9; CMM 57-53-08.; [02] COMPLETESDR SWAA2021070181508Support Angle · crackedCRACKED SUPPORT ANGLE IN AFT FLAP WELL ATTACHED INBD SIDE OF DEFLECTION CONTROL ARM / REPLACED SUPPORT ANGLE PER SRM 51-40-02SDR SWIA202160728Skin · dentedLH UPPER INBD FLAP 11.5" FROM SPAR 23.5" FROM FUSELAGE HAS DENT ROUGH DIMENSIONS .3" X .25" X .015" DEEP.PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE EVIDENCE USING STANDARD ACFT PRACTICES. (C-CHECK RO 9/3/21) REPAIRESDR IPXA2021062370892Tee Angle · crackedINSPECTION TYPE:3CRT WING O/B FLAP I/B AFT HINGE FAIRING FWD END TEE ANGLE IS CRACKED.REMOVED AND REPLACED CRACKED RT WING O/B FLAP I/B AFT HINGE FAIRING FWD END TEE ANGLE IAW SRM 51-33-01. (MINOR)SDR SWIA2021082060482Skin · damaged* LEFT WING OUTBD FLAP TOP SKIN HAS SMOKING RIVETS MARKED (C-CHECK RO 8/18/2021) REMOVED AND REPLACED 15EA FASTENERS IN L/H WING O/B FLAP TOP SKIN REF REO 690-57-53-125 REV -- DATED 2021-06-30. COMPLIED WITH ALL STEPS OF REO 69-57-53-125-REV -- DATED 20SDR SWIA2021080560046Fitting · chafed* THE RH WING, OUTBOARD FLAP'S NOSE RIB FITTING AT APPROX. FLS 235, HAS CHAFING ON ITS INTERNAL INBOARD SURFACE IN MULTIPLE SPOTS. (MARKED WITH RED GREASE PENCIL) (C-CHECK RO 8/1/2021) REPAIRED R/H WING OUTBOARD FLAP NOSE RIB FITTING AT APPROX FLS 235 SDR SWIA2021080560045Attach Fitting · galled* THE LH WING, OUTBOARD FLAP'S VANE ATTACH FITTINGS HAVE GALLING AND CHAFING PRESENT ON THEIR LOWER SURFACES AT THE FOLLOWING APPROX. LOCATIONS: FLS 171, FLS 189, FLS 235, FLS 280, AND FLS 296. (C-CHECK RO 8/1/2021) REMOVED GALLING REF REO 601R-57-53-19SDR SWIA2021080560044Attach Fitting · chafed* THE LH WING OUTBOARD FLAP, INBOARD HINGE BOX'S AFT ATTACH FITTING IS CHAFED ON THE CENTER 2 LUGS. (C-CHECK RO 8/1/2021) REPAIRED L/H WING OUTBOARD FLAP INBOARD HINGE BOX AFT ATTACH FITTINGS REF REO 601R-57-21-3497 REV.-- DATED 2021-06-29 . COMPLIED SDR SWIA2021080560043Attach Fitting · chafed* THE LH WING OUTBOARD FLAP, CENTER HINGE BOX'S AFT ATTACH FITTING IS CHAFED ON THE CENTER 2 LUGS. (C-CHECK RO 8/1/2021) REPAIRED L/H WING OUTBOARD FLAP CENTER HINGE BOX AFT ATTACH FITTING REO 601R-57-21-3497 REV.-- DATED 2021-06-29. COMPLIED WITH 51-9SDR SWIA2021080560042Attach Fitting · chafed* THE LH WING OUTBOARD FLAP, OUTBOARD HINGE BOX'S AFT ATTACH FITTING IS CHAFED ON THE CENTER 2 LUGS. (C-CHECK RO 8/1/2021) REPAIRED L/H WING OUTBOARD FLAP OUTBOARD HINGE BOX AFT ATTACH FITTING REF REO 601R-57-21-3497 REV.-- DATED 2021-06-29. COMPLIED WSDR IPXA2021070171171Hinge Bracket · corrodedINSPECTION TYPE:3CLT WING I/B FLAP O/B AFT HINGE BRACKET LUGS HAS CORROSION.REPAIRED CORRODED LT WING I/B FLAP O/B AFT HINGE BRACKET LUGS IAW VT-SAA EA 011-5740-01-A9196 REV. IR AND UPS EO MD11-5740-80863-A. (MINOR)SDR IPXA2021070171170Hinge Bracket · corrodedINSPECTION TYPE:3CRT WING I/B FLAP O/B FWD HINGE BRACKET LUGS HAS PITTING CORROSION.REPAIRED CORRODED RT WING I/B FLAP O/B FWD HINGE BRACKET LUGS IAW VT-SAA EA 011-5740-01-A9192 REV. IR AND UPS EO MD11-5740-80879-A. (MINOR)SDR IPXA2021070171168Hinge Bracket · corrodedINSPECTION TYPE:3CRT WING I/B FLAP O/B AFT HINGE BRACKET LUG BORES HAS PITTING CORROSION.REPAIRED CORRODED RT WING I/B FLAP O/B AFT HINGE BRACKET LUGS IAW VT-SAA EA 011-5740-01-A9191 REV. IR AND UPS EO MD11-5740-80847-A. (MINOR)SDR IPXA2021063071151Hinge Bracket · corrodedINSPECTION TYPE:3CR/H WING O/B FLAP HINGE BRACKET ASSY ON A/C SIDE HAS CORROSION ON LUG BORE AND FACE.REPAIRED HINGE BRACKET ASSY IAW VT-SAA EA 011-5700-01-A9180 REV. I/R AND UPS EO MD11-5740-80834-A. (MINOR)SDR IPXA2021062971104Hinge · corrodedINSPECTION TYPE:3CLH O/B FLAP O/B AFT HINGE #7 LUG HOLE HAS PITTING CORROSION.REPAIRED CORRODED LH O/B FLAP LUG HOLE IAW CMM 57-52-04 (MINOR)SDR IPXA2021062971102Hinge · corrodedINSPECTION TYPE:3CLT O/B FLAP O/B FWD HINGE #2 LUG HOLE HAS PITTING CORROSION.REPAIRED CORRODED LT O/B FLAP HINGE IAW CMM 57-44-09 PG 602 (MINOR)SDR IPXA2021062570959Hinge Bracket · corrodedINSPECTION TYPE:3CLT WING O/B FLAP O/B FWD HINGE #1 LUG BORE HOLE HAS PITTING.REPAIRED CORRODED LT WING O/B FLAP O/B FWD HINGE BRACKET LUG AT STA. XW 638.31 IAW VT-SAA EA 011-5740-01-A9190 REV. IR AND UPS EO MD11-5740-80794-A. (MINOR)SDR DALA2021060903148Skin · dentedSHIP 5650 DENT ON THE UNDERSIDE OF THE RIGHT WING INBOARD FLAP. CORRECTIVE ACTION: MEASURED DENT IS BEYOND DENT LIMIT. REMOVED PANEL FOR COMP. SHOP VISIT. REMOVED CUTOUT WITH REF B757-200 SRM. ACCOMPLISHED HFEC INSP IAW B757 NTM 51-00-01, NO CRACKS, APPLIED RESDR DALA2021060903147Skin · chafedSHIP 6705 LT WING I/B MAIN FLAP UPPER SURFACE O/B DOUBLER IS CHAFFED. CORRECTIVE ACTION: EVALUATED DOUBLER AT LT WING I/B MAIN FLAP UPPER SURFACE O/B AND FOUND TO BE BEYOND SERVICEABLE LIMITS. APPLIED NEW REPAIR DOUBLER AND FILLER IAW B757-200 SRM. (1832814)SDR SWIA2021081860315Vane · chafed* LH INBD FLAP VANE CHAFED AT APPROXIMATELY WS88 (C-CHECK RO 8/16/2021) REMOVED AND REPLACED LH IB FLAP VANE CAP AT WS88 REF CRJ700 SRM 51-42-13-001-001-A01 & DWG NO: CC670-14010 REV E. COMPLIED WITH TASK CARD 51-900-1002-SKYSDR P5CA2021053100202Skin · puncturedRH O/B AFT FLAP L/E FAIRING FOUND PUNCTURE(<P>PERFORMED PERMANENT HOT BOND REPAIR AS PER SRM 51-70-07 PARA 5.A</P>)SDR P5CA2021053100203Skin · delaminatedLHW I/B FORE FLAP UPPER SURFACE O/B AREA FOUND DELAMINATED(<P>PERFORMED PERMANENT HOT BOND REPAIR AS PER SRM 51-70-07 PARA 5.A</P>)SDR P5CA2021053100204Skin · delaminatedLHW I/B FORE FLAP O/B UPPER EDGE FOUND DELAMINATION(<P>PERFORMED PERMANENT HOT BOND REPAIR AS PER SRM 51-70-07 PARA 5.G</P>)SDR P5CA2021053100205Link · damagedRHW O/B T/E MID FLAP T/E #8 SUPPORT LINK UPR MOUNT BOLT HOLE ELONGATED (COUNT FROM O/B)(<P>PERFORMED PERMANENT HOT BOND REPAIR AS PER SRM 51-70-07 PARA 5.K</P>)SDR P5CA2021060100220Skin · delaminatedRHW I/B AFT FLAP LOWER SURFACE T/E FOUND DELAM(<P>PERFORMED PERMANENT HOT BOND REPAIR AS PER SRM 51-70-07 PARA 5.A</P>)SDR P5CA2021060100221Fairing · delaminatedRHW O/B FORE FLAP L/E FAIRING MID AREA FOUND DELAM(<P>PERFORMED PERMANENT HOT BOND REPAIR AS PER SRM 51-70-07 PARA 5.A</P>)SDR SWAA2021072279964Fairing · punctured#6 FLAP TRACK FAIRING 642EB HAS A PUNCTURE AND DELAM (MARKED) ; / [01] REMOVED AND REPLACED #6 AFT FAIRING PANEL 642EB PER AMM 27-51-18-000-802 STEP 4E(6); AMM 27-51-18-400-802 STEP 5G(5) ID IS000661 SN G97548; [02] REPLACE COMPLETE; [03] VERIFIED REMOVED AND SDR SWAA2021072279957Skin · chafedRIGHT WING OB AFT FLAP UPPER SURFACE HAS CHAFING DAMAGE AT IB EDGE; 9' FROM AFT EDGE. ; / [01] REMOVED AND REPLACED R/W O/B AFT FLAP ON SWA CUSTOMER CARD TTG8Q005CXKR AND REPAIRED ON COMPONENTS CUSTOMER RO NO P0375196-1; [02] VERIFIED REMOVED AND REPLACED R/W SDR SWIA2021073059819Hinge Arm · damaged*L/H INBD FLAP, INBD HINGE ARM, HAS FOD DAMAGE AT HINGE LOCATION ON ARM. (AREA MARKED) (C-CHECK RO 7/27/2021) REPAIRED AREA L/H INBD FLAP, INBD HINGE ARM, FOD DAMAGE AT HINGE LOCATION ON ARM BY COMPLYING WITH REO 601R-57-54-330 REV-- DATED 2021-06-16 (SSDR AALA202107012259Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY BEARING INTERCONNECTING STRUT IB FLAP (MEASURE OF PLAY 0.011 INCH). REPLACED RIGHT WING INBOARD FLAP INTERCONNECTING STRUT HINGE FITTING.SDR AALA202107010357Bracket · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY BEARING INTERCONNECTING STRUT INBOARD FLAP AT INBOARD FLAP REAR SPAR AND RIB 13. REPLACED LEFT WING INBOARD FLAP INTERCONNECTING STRUT HINGE FITTING BRACKET.SDR REXA2021062900422Vane · chafedLH INBOARD FLAP VANE IS CHAFED ON LEADING EDGE WS 38.00 INBOARD ACTUATOR ARM. REPLACED PANEL 584ET IAW CRJ 900 SRM 51-40-11-001-001-A01.SDR SWAA2021060780465Skin · delaminatedLEFT WING AFT OUTBOARD (LEFT) FLAP DELAMINATION ON UPPER INBOARD CORNER / REMOVED AND REPLACED L/H O/B AFT FLAP RIG & OPS CK GOOD PER MM 27-51-22P/N OFF 113A3700-25 S/N 004420P/N OFF 113A3700-25 S/N 004333 P/N TRANS 171359SDR FDEA202106021432Skin · dentedLH WING O/B FLAP L/E NOSE GOT A DENT AT RIB17 5". ACCOMPLISHED THE DENTED AREA REPAIR I.A.W. A300-600 SRM 57-50-00-201, PARA. 4H, P. 230- 234, FIG. 208. THIS IS CAT. B REPAIR I.A.W. A300-600 SRM 57-50-00-201, P. 202 AND SRI 57-50-00-201 IIR 57-50- 00-2- 00SDR IPXA2021061570614Bracket · rustedINSPECTION TYPE:3CR/H WING O/B FLAP I/B FWD. HINGE O/B SIDE LOAD FITTING HAS RUST COMING OUT.REMOVED AND REPLACED SIDE LOAD FITTING/BRACKET IAW AMM 57-53-01-400-801. (MINOR)SDR DALA2021110306774None · noneSHIP 3247 CORROSION AFT MOVABLE FAIRING WEB ON RH PYLON. CORRECTIVE ACTION: REPLACED AFT MOVABLE FAIRING WEB PER SRM A320 51-72-11. (1825789)
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