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 FDEA202009172238Skin · delaminatedLT WING OUTBOARD FLAP UPPER TRAILING EDGE PANEL HAS DELAMINATED AREA AT WS 495.SDR FDEA202009172240Skin · delaminatedRT WING OB MAIN FLAP EXTERNAL AREA T/E HAS ONE DENT. UPON FURTHER EVAL FOUND 1/2" DENT DELAMINATED, IAW B757 SRM 51-10-06-2R. ACCOMPLISHED REPAIR ON RT WING O/B MAIN FLAP EXTERNAL AREA T/E AT WS 560-565, IAW B757 SRM 57-53-01-2R REP 1 TABLE III SRM 51-70-07-SDR FDEA202009172239Skin · delaminatedLT WING O/B FLAP UPPER T/E PANEL HAS DELAMINATED AREA AT WS 475. REPAIRED LT WING O/B FLAP UPPER T/E PANEL BY HOT-BONDING REPAIR PLYS, IAW B757 SRM 57-53-01-2R FIG 201 TABLE III AND B757 SRM 51-70-07-06 PARAG 5B AND B757 SRM 51-70-17-0G PARAG 3G AT WS 475.SDR FDEA202009172237Skin · delaminatedLT WING O/B FLAP UPPER T/E PANEL HAS DELAMINATED AREA AT WS 495. REPAIRED LT WING O/B FLAP UPPER T/E PANEL BY HOT-BONDING REPAIR PLYS, IAW B757 SRM 57-53-01-2R FIG 201 TABLE III SRM 51-70-07-0G PAR 5B AND SRM 51-70-17-0G PAR 3G AT WS 495.SDR FDEA202009172236Skin · delaminatedLT WING O/B FLAP UPPER T/E PANEL HAS DELAMINATED AREA AT WS 595. REPAIRED LT WING O/B FLAP UPPER T/E PANEL BY HOT-BONDING REPAIR PLYS, IAW B757 SRM 57-53-01-2R FIG 201 TABLE III SRM 51-70-07-0G PAR 5B AND SRM 51-70-17-0G PAR 3G AT WS 595.SDR IPXA2020091760336Hinge Fitting · wornINSPECTION TYPE: 2C LT OUTBOARD FLAP INBOARD FLAP ACTUATOR UPPER MOUNT INBOARD BUSHING IS MIGRATED. REPAIRED LT OUTBOARD FLAP INBOARD ACTUATOR HINGE LUG, IAW VT-SAA EA NR 011-5740-01-A8524 I/R AND UPS EO NR MD11-5740-77852-A (MINOR).SDR SWAA2021071316694Skin · delaminatedRT WING O/B AFT FLAP UPPER SURFACE IS DELAMINATED FROM I/B END TO 17' O/B FROM I/B END. / REMOVED & REPLACED RT OB AFT FLAP IAW MM 27-51-22-000-801 AND MM 27-51-22 400-801 ADJUSTMENT CHECK GOOD IAW MM 27-51-22-400-801 ALL TORQUES VERIFIED. (POS:RT O/B;TAG NO.:SDR SWIA202053296Bushing · corrodedLT INBOARD FLAP INBOARD HINGE BOLT BUSHING FOUND TO BE CORRODED. C-CHECK RO 10/13/2020. RECEIVED NEW SERVICEABLE BUSHING FOR LT INBOARD FLAP INBOARD HINGE, REF CAMP 21380330 FOR INSTALLATION OF HARDWARE AND OPS.SDR SWIA202053341Hinge Fitting · corrodedLT AND RT OUTBOARD FLAP HINGE BOXES HAVE SEVERAL CORRODED MOUNTING HARDWARE NUTS. LT CENTER HINGE BOX, AFT INBOARD AND OUTBOARD NUTS, LT INBOARD HINGE BOX, AFT OUTBOARD NUT, RT CENTER HINGE BOX, AFT INBOARD NUT, RT INBOARD HINGE BOX, AFT INBOARD NUT. C-CHECKSDR FDEA202009152230Skin · gougedRIGHT OUTBOARD FLAP UPPER SIDE INBOARD OF FLAP ATTACH POINT HAS A GOUGE (MWT). C/W EA 8-5750-TO356663 AND N/R N00012, W/O 78394.SDR SWIA202053545Doubler · wornLT INBOARD FLAP VANE HAS WEAR ON DOUBLER AT WS 104 FROM FLAP STOP. C-CHECK RO 10/20/2020. REMOVED EXISTING LT INBOARD FLAP (OUTBOARD CENTER) LEADING EDGE. FIT AND INSTALLED NEW LT INBOARD FLAP (OUTBOARD CENTER) LEADING EDGE P/N 601R14303-51 WITH SEALANT, RESDR SWIA202053544Doubler · wornRT INBOARD FLAP VANE HAS WEAR ON DOUBLER AT WS 55 FROM FLAP STOP. C-CHECK RO 10/20/2020. REMOVED INBOARD RT FLAP VANE AT WS 55 AND WET INSTALLED NEW FLAP VANE P/N 601R14303-54, REF CRJ 200 SRM AND DWG. INSTALLATION OF REPAIR DOUBLER TITANIUM CAPS ON INBOARDSDR SWIA202052786Guide · crackedRT WING NR 2 MAIN FLAP CARRIAGE INBOARD AFT TRACK GUIDE CRACKED. C-CHECK RO 9/24/2020. REMOVED AND REPLACED RT NR 2 MAIN FLAP CARRIAGE INBOARD AFT TRACK GUIDE, REF E-175 AMM. RIGGING AND OPERATIONAL TEST CHECKS GOOD.SDR SWIA202052785Guide · crackedLT WING NR 4 AFT FLAP CARRIAGE INBOARD FWD TRACK GUIDE CRACKED. C-CHECK RO 9/24/2020. REMOVED AND REPLACED LT NR 4 AFT FLAP CARRIAGE INBOARD FWD TRACK GUIDE, REF E-175 AMM.SDR SWIA202053528Hinge Arm · chafedLEFT OUTBOARD FLAP CENTER HINGE ARM CHAFED ON OUTBOARD SIDE NEAR ATTACHMENT TO HINGE BOX. C-CHECK RO 10/20/2020. BLENDED OUT CHAFE ON LEFT OUTBOARD FLAP CENTER HINGE ARM ON OUTBOARD SIDE NEAR ATTACHMENT TO HINGE BOX, IAW CRJ200 SRM. BLENDED AREA FOUND TO BESDR SWAA2021071315391Flap Track · looseLEFT WING I\B AFT FLAP I\B TRACK AFT ATTACH POINT LOOSE. / REPLACED LEFT WING I\B AFT FLAP I\B TRACK PER AMM 27-51-16.SDR IPXA2020092360557Beam · crackedINSPECTION TYPE: 2C LT WING OUTBOARD FLAP AFT HINGE FAIRING INBOARD SUPPORT BEAM IS CRACKED. REMOVED AND REPLACED CRACKED LT WING OUTBOARD FLAP AFT HINGE FAIRING INBOARD SUPPORT BEAM, IAW MD-11 SRM 51-33-01, 51-35-01 AND 51-35-02. (MINOR)SDR FDEA2020090962136Skin · dentedLT WING INBOARD AFT FLAP LOWER SURFACE IS DENTED 10.5 INCHES AFT OF THE LEADING EDGE AND 31.5 INCHES FROM INBOARD SIDE. REPAIRED LT WING INBOARD AFT FLAP LOWER SURFACE IAW B767-300 SRM 57-53-01-0I, SRM 57-53-01-1A, SRM 57-53-01-2R, SRM 51-70-03 PARA 5 FIG 5 ASDR FDEA2020090962135Skin · dentedLT WING INBOARD AFT FLAP LOWER SURFACE IS DENTED AT TRAILING EDGE AND 64 INCHES FROM INBOARD SIDE. REPAIRED LT WING INBOARD AFT FLAP LOWER SURFACE, IAW B767-300 SRM: 57-53-01-1A, SRM 57-53-01-2R REPAIR 1, SRM 51-70-10-2R REPAIR 4. MAJOR REPAIR.SDR SWAA2021081714615Fairing · delaminated#6 FLAP SUPPORT FAIRING HAS AN AREA OF DELAMINATION UNDER SCISSOR LINK ASSY. / REPLACED # 6 FLAP SUPPORT FAIRING IAW AMM 27-51-18POS #6PN OFF: 113A9310-2 PN ON: 113A9350-2 SN OFF: K4845SN ON: 2228 (SAM 326: A1314566SDR SWIA202053622Slat Track · wornRT SLAT TRACK 3-3 HAS MULTIPLE WEAR MARKS ON ITS UPPER AND LOWER ROLLING SURFACES. C-CHECK RO 10/22/2020. REPAIRED RT SLAT TRACK 3-3, REFERENCING REO CRJ 700 SRM CRJ 700 AMM AND DWG. OPERATIONAL TEST GOOD. COMPLIED WITH SKYWEST TASK CARD. COMPLETED SKYWESSDR SWIA202053620Slat Track · wornLT WING SLAT TRACK 3-3 HAS MULTIPLE WEAR MARKS ON UPPER AND LOWER ROLLER CONTACT SURFACES. C-CHECK RO 10/22/2020. REPAIRED LT WING SLAT TRACK 3-3 WEAR MARKS, IAW REO CRJ700 SRM CRJ700 AMM. OPERATIONS CHECK GOOD AT THIS TIME.SDR SWIA202053345Hinge Arm · chafedRT OUTBOARD FLAP CENTER HINGE ARM, FAIRING GUIDE PLATES ARE CHAFED. C-CHECK RO 10/13/2020. REMOVED AND REPLACED RT OUTBOARD FLAP CENTER HINGE ARM, FAIRING GUIDE PLATES (OUTBOARD AND INBOARD), REF CRJ-200 SRM AND DWG. SEE CONTINUATION CARD FOR DETAILS.SDR SWAA2020090414105Skin · delaminatedLEFT WING OUTBOARD AFT FLAP DELAMINATED ON INBOARD AFT CORNER. R&R LT WING OUTBOARD AFT FLAP PER M/M 27-51-22, ISSUE #3009231. INSPECTOR H551 PN OFF:113A3700-7 SN OFF:00210PN ON:113A3700-23 SN ON:002017.SDR IPXA2020092560627Rib · damagedINSPECTION TYPE: A300 LT INBOARD FLAP RIB 26B FOUND DAMAGED AFTER LOWER SKIN REMOVAL. REPAIRED RIB, IAW UPS EO-A300-5750-77857-A VT MAE EA 300-5752-27-A2502 REV.SDR SWIA202053357Skin · dentedRIGHT WING INBOARD FLAP LOWER SKIN HAS TWO DENTS BY EACH OTHER, MARKED. C-CHECK RO 10/16/2020. ACCOMPLISHED REPAIR TO RT INBOARD FLAP LOWER SKIN, IAW CRJ700 SRM. COMPLIED WITH TASK CARD.SDR SWIA202053347Fairing · gougedRT FLAP STUB FAIRING HAS GOUGE ALONG BOTTOM LENGTH OF FAIRING AND FORWARD HINGE HALF HAS BROKEN NUTPLATE. C-CHECK RO 10/13/2020. REPLACED WITH NEW RT FLAP STUB FAIRING ASSEMBLY, REF CRJ 200 SRM. SEE CONTINUATION CARD FOR DETAILS.SDR SWAA2021071313276Skin · delaminatedLT WING OB AFT FLAP IS DELAMINATED ON I/B END / REMOVED AND REPLACED LT WING OB AFT FLAP IAW AMM 27-51-22(SAM 326: A1314592)POS LT PN OFF: 113A3700-27PN ON: 113A3700-7SN OFF: 005029SN ON: 00507SDR SWAA2020100515459Skin · dentedSEVERAL DENTS ON INBOARD MAIN FLAP LOWER SURFACE LOCATED AT 4.5IN FROM TRAILING EDGE AND 6.25 IN FROM OUTBOARD EDGE WEDGE PANEL AT RT WING. PERFORMED PERMANENT REPAIR ON INBOARD MAIN FLAP WEDGE PANEL AT RT WING, AS PER B737-700 SRM 57-53-01-2R-7 REP 7. TOOL SDR SWAA2020091415882Skin · dentedDENT INBOARD MAIN FLAP LOWER SURFACE LOC AT 3.75 IN FROM TRAILING EDGE AND 4.25 IN FROM OUTBOARD EDGE AT RT WING. PERFORMED PERMANENT REPAIR ON INBOARD MAIN FLAP WEDGE PANEL AT RT WING AND IS DOCUMENTED ON DEFECT NO L177042.SDR SWAA2020091415881Skin · dentedDENT INBOARD MAIN FLAP UPPER SURFACE LOC AT 2.5 IN FROM TRAILING EDGE AND 43.5 IN FROM OUTBOARD EDGE AT RT WING. PERFORMED PERMANENT REPAIR ON INBOARD MAIN FLAP WEDGE PANEL AT RT WING AND IS DOCUMENTED ON DEFECT NO L177042.SDR IPXA2020091436160Former · crackedINSPECTION TYPE: 2C LT OUTBOARD FLAP INBOARD HINGE FRAME, FORMER IS CRACKED. REMOVED, FABRICATED, AND REPLACED FORMER, IAW DWG ARC 0547 AND SRM 51-31-01 (MINOR).SDR UIEA2020090431926Skin · delaminatedLHW AFT FLAP OUTBOARD EDGE FOUND DELAMINATION. PERFORMED PERMANENT COMPOSITE REPAIR IAW SRM 51-70-07 PART 5.G REV 89.SDR UIEA2020090431927Panel · delaminatedLHW OUTBOARD MID FLAP INBOARD UPPER PANEL 587LT FOUND DELAMINATION. PERFORMED PERMANENT METAL HOT BOND REPAIR.SDR UIEA2020090431947Skin · delaminatedL/H I/B MID FLAP L/E I/B SIDE DELAMINATION(<P>PERFORMED PERMANENT COMPOSITE REPAIR IAW SRM 51-70-07 PAR 5.A REV 89.</P>)SDR IPXA2020093060816Skin · gougedINSPECTION TYPE: A300 RT WING INBOARD FLAP UPPER SURFACE LARGE REPAIR DOUBLER HAS GOUGE DAMAGE. REPLACED DOUBLER, IAW UPS EO A300-5750-777833.SDR IPXA2020093060810Rub Strip · chafedINSPECTION TYPE: A300 RT WING UPPER SURFACE LEADING EDGE HAS 8 EACH RUBSTRIPS WITH CHAFE DAMAGE. REMOVE, FABRICATED, REPLACED RUBSTRIPS, IAW UPS EO A300-5750-78032.SDR FDEA202008272042Hinge Bracket · corrodedRIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSIONS. CORROSIONS AT RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CSDR FDEA202008272041Hinge Bracket · corrodedRIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSIONS. CORROSIONS AT RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMMSDR FDEA202008272040Hinge Fitting · corrodedRIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSIONS. CORROSIONS AT RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE (#3 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. REPAIR BUSHING FABRSDR FDEA202008272038Lug · corrodedLEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSIONS. CORROSIONS AT LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM SDR FDEA202008272036Hinge Bracket · corrodedRT WING FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG HOLE BORE FOUND CORROSION. CORROSION AT RT WING FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD. PIVOT LUG HOLE BORE (F AND G HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-52-03. REPASDR SWIA202053651Actuator · corrodedLEFT HAND OUTBOARD FLAP BUTE DOOR ACTUATOR ON THE CENTER HINGE BOX ATTACH POINT HAS A CORRODED BUSHING, FLAGGED. C-CHECK RO 10/22/2020. LEFT OUTBOARD FLAP BUTE DOOR ACTUATOR LEVER, OUTBOARD SPACER REMOVED AND REPLACED WITH NEW, REF CRJ 700 AMM.SDR SWAA2020083111955Skin · delaminatedR/H WING INBD FLAP OTBD WEDGE DELAMED / R & R'D R/H I/B MAIN FLAP ASSY PER M/M 27-51-12. OPS CHK GOOD. SEE SA-M 326 ATTACHED #A1045546 PN OFF: 113A2100-60A SN OFF: T1934 PN ON: 113A2100-54A SN ON: K1047SDR SWIA202053650Hinge Fitting · corrodedRT OUTBOARD FLAP INBOARD HINGE BOX FWD FITTING 3 EA BOLTS CORRODED. C-CHECK RO 10/22/2020. REMOVED AND REINSTALLED THE RT FLAP HINGE BOX AT WS 178 WITH NEW BOLTS, BUSHINGS, NUTS AND WASHERS, REF CRJ700 AMM. ALL OPERATIONS AND LEAK CHECKS CHECKED GOOD. SEE SDR SWIA202053649Hinge Fitting · corrodedRT OUTBOARD FLAP OUTBOARD HINGE BOX FWD FITTING 2 EA BOLTS CORRODED. C-CHECK RO 10/22/2020. REMOVED 2 EA CORRODED BOLTS FROM RT OUTBOARD FLAP OUTBOARD HINGE BOX FWD FITTING AND REPLACED WITH NEW, REFERENCING CRJ 700 AMM. OPERATIONAL AND LEAK TESTS GOOD.SDR SWIA202053605Hinge Fitting · chafedRT OUTBOARD FLAP MID HINGE ARM LUG HAS CHAFE. C-CHECK RO 10/22/2020. COMPLIED WITH REPAIR TO CHAFE ON THE RT OUTBOARD FLAP MID HINGE ARM REFERENCING REO, REWORK IS WITHIN LIMITS, SEE CONTINUATION CARD FOR ADDITIONAL DETAILS OF WORK PERFORMED. COMPLIED WITH SDR FDEA2020082652017Bracket · corrodedRT WING, WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT RT WING, WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE (NR 4 HOLE). REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-SDR FDEA2020082652016Bracket · corrodedRT WING, WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT RT WING, WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE (NR 4 HOLE). REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. SDR FDEA2020082652015Bracket · corrodedLT WING, WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT LT WING, WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE (NR 4 HOLE). REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-
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