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 FDEA202012123125Stop Fitting · crackedRIGHT HAND OUT BOARD FLAP SECONDARY UP STOP FITTING FOUND CRACKED AT XOVH 537.324. CRACKED FITTING REMOVED AND REPLACED AT RIGHT HAND OUT BOARD FLAP, AS PER SRM 51-33-01-0G AT XOVH 537.324. REPAIR CLASSIFIED AS MINOR, PER GMM 6-2-100.SDR SWIA202056757Hinge Fitting · corrodedRIGHT WING OUTBOARD FLAP - OUTBOARD FORWARD HINGE BOX SUPPORT FITTING HAS CORRODED HARDWARE. (C-CHECK) RO 3/8/2021 REPLACED RH WING OUTBOARD FLAP, OUTBOARD FORWARD HINGE BOX SUPPORT FITTING CORRODED HARDWARE WITH NEW REF CRJ-700 AMM 57-54-02-400-808-A01, SDR SWIA202056756Hinge Fitting · corrodedLEFT WING OUTBOARD FLAP - INBOARD AFT LOWER HINGE LUG FITTING HAS CORRODED HARDWARE. (C-CHECK) RO 3/8/2021 REMOVED LEFT WING OUTBOARD FLAP - INBOARD AFT LOWER HINGE LUG FITTING HARDWARE REF CRJ700 AMM 57-53-27-000-801(CONFIG A01) STEPS 4.A(2)(3)(4)(5)(6)(SDR SWIA202056755Hinge Fitting · corroded*LEFT WING OUTBOARD FLAP - OUTBOARD AFT LOWER HINGE LUG FITTING HAS CORRODED HARDWARE. (C-CHECK) RO 3/8/2021 REMOVED LEFT WING OUTBOARD FLAP - OUTBOARD AFT LOWER HINGE LUG FITTING HARDWARE REF CRJ700 AMM 57-53-27-000-803 (CONFIG A01) STEPS 4.A.(4)(5)(6). SDR SWIA202056187Hinge Fitting · chafed*CHAFFING NOTED ONL/H INBD FLAP HINGE LUG PLATE AT WS80.50 (C-CHECK) RO 2/9/2021 BLENDED L/H INBD FLAP HINGE LUG PLATE AT WS80.50 CHAFFE DAMAGE TO A SMOOTH CONTOUR AND RESTORED FINISH. REMAINING MATERIAL WITHIN LIMITS. REF REO 601R-57-21-3392 REV -- DATEDSDR SWAA2021011541192Rib · excess playRT WING DEFLECTOR PANEL SERRATED PLATE HAS PLAY. REPAIRED RT WING INBOARD FIXED TRAILING EDGE DEFLECTION CONTROL RIB UPPER TAB PER, REF B737 SRM 57-51-02-2R-3 REPAIR 3 FIG 202.SDR 6CBA2020121020202Structure · crackedPROBLEM: DURING ROUTINE AIRCRAFT INSPECTION, CRACKS WERE FOUND ON BOTH FLAPS (LT/RT). CRACK LOCATIONS, AFT FAIRING ATTACHMENT NUPLATE BETWEEN RIBS 3 AND 4. RESOLUTION: THE CRACKS ON BOTH FLAPS WERE REPAIRED USING LOCAL SKIN CUT OUTS AND AN EXTERNAL DOUBLER. SDR SWIA202055726Hinge · corrodedRH OUTBOARD FLAP HINGE BOXES HAVE SOME CORROSION ON HARDWARE. (C-CHECK) RO 1/29/2021 REPLACED HARDWARE (3 NUTS) ON RH OUTBOARD FLAP HINGE BOXES WS 178.00, AND 220.00 1 EA.PN: MS17825-9, 2 EA. PN:MS17825-7 IAW CRJ 200 AMM 57-21-35-400-801/802 STEPS 3. A.SDR SWIA202055668Nut · corrodedRT INBOARD FLAP INBOARD HINGEBOX FWD MOUNT BOLT NUT CORRODED. C-CHECK RO 1/28/2021. REMOVED AND REPLACED RT INBORD FLAP INBOARD HINGEBOX FWD MOUNT BOLT NUT, IAW CRJ200 AMM REF 57-21-34-400-801.
SDR SWIA202056219Hinge Arm · corrodedRH OTBD FLAP HINGE ARM ASSY'S AT WS178.00, WS220.00 AND 264.00 MOUNTING HARDWARE IS WORN AND CORRODED (C-CHECK) RO 2/9/2021 ODERED, RECEIVED AND INSTALLED NEW HARDWARE ON RH OUTBOARD- FLAP HINGE ASSEMBLY AT WS178.00 WS220.00 AND WS264.00. 15 BOLTS, 12 NUTSSDR SWIA202056218Hinge Arm · corrodedLH OTBD FLAP HINGE ARM ASSY'S AT WS178.00, WS220.00 AND 264.00 MOUNTING HARDWARE IS WORN AND CORRODED (C-CHECK) RO 2/9/2021 ORDERED AND RECEIVED NEW HARDWARE. SEE CAMP 21866107 JOB 2757660 OP 553 FOR INSTALL. 1 PIN, 14 NUTS, 14 BOLTS, 37 WASHERS.SDR FDEA202012083069Skin · delaminatedRIGHT WING INBOARD TRAILING EDGE FLAP LOWER SURFACE IS DELAMINATED 2" FORWARD OF TRAILING EDGE AND 7" INBOARD OF THE OUTBOARD EDGE. REPAIRED RIGHT WING INBOARD TRAILING EDGE AFT FLAP LOWER SURFACE, IAW B767 SRM 57-53-01-2R FIGURE 201 DETAIL 3, 51-70-10-2R REPSDR SWIA202055666Spring · corrodedL OUTBOARD FLAP OUTBOARD HINGEBOX BUTE DOOR ACCTUATOR SPRING HAS SURFACE CORROSION. C-CHECK RO 1/28/2021. REMOVED AND REINSTALLED LT OUTBOARD FLAP OUTBOARD HINGEBOX BUTE DOOR ACTUATOR FOR ACCESS, IAW CRJ 200 AMM 27-54-25-000-801/400/801. REMOVED AND REPLACESDR SWIA202055665Nut Plate · corrodedL OUTBOARD FLAP CENTER HINGEBOX CENTER HINGE BOLTS LEFT AND RIGHT NUTS HAVE CORROSION. C-CHECK RO 1/28/2021. REMOVED AND REPLACED LT OUTBOARD FLAP CENTER HINGEBOX CENTER HINGE BOLTS LEFT AND RIGHT NUTS, IAW CRJ200 AMM REF 57-21-35-400-802.SDR SWIA202055664Nut · corrodedL OUTBOARD FLAP INBOARD HINGBOX CENTER HINGE BOLTS LEFT AND RIGHT NUTS HAVE CORROSION. C-CHECK RO 1/28/2021. REMOVED AND REPLACED CORRODED HARDWARE AT LT OUTBOARD FLAP, INBOARD HINGE BOX AT WS 178.00 CENTER MOUNTING POSITION, IAW CRJ200 AMM 57-21-35-400-801 SDR SWIA202055663Nut · corrodedL OUTBOARD FLAP INBOARD HINGEBOX AFT HINGE MOUNT BOLT NUT HAS CORROSION. C-CHECK RO 1/28/2021. REMOVED AND REPLACED LEFT OUTBORAD FLAP INBOARD AFT HINGE MOUNT BOLTS NUT, IAW CRJ200 AMM REF 57-21-35-400-801.SDR SWAA2021071334711Skin · chafedLT WING I/B T/E AFT FLAP HAS DEEP CHAFE MARK ON UPPER O/B SIDE. (M) / R+R L/H INBD AFT FLAP PER AMM 27-51-12P/N OFF 113A2700-27 S/N OFF 000483P/N ON 113A2700-25 S/N ON D-3398SDR SWIA202055927Skin · chafed*LH INBD FLAP CHAFFED UNDER PANEL 584AB ON THE INNER UPPER SKIN, JUST BELOW THE FLAP VANE ACTUATOR (MARKED) (C-CHECK) RO 2/1/2021 LH INBD FLAP REMOVED THE CHAFFED UNDER PANEL 584AB ON THE INNER UPPER SKIN, JUST BELOW THE FLAP VANE ACTUATOR REF CRJ-900 SRM SDR SWIA202056223Vane · corrodedLH INBOARD FLAP INBOARD FLAP VANE ACTUATOR INNER SPRING AND HARDWARE HAS CORROSION. (C-CHECK) RO 2/9/2021 REPLACED L/H I/B FLAP VANE ACTUATOR INNER SPRING HARDWARE IAW CRJ 200 AMM 27-54-16-400-801SDR SWAA2021072733527Fairing · crackedLT WING FLAP FAIRING #3 POSITION. AFT O/B SEAL CAVITY CORNER; FITTING HAS EVIDENCE OF CRACK.MKD 126-008 / REMOVED PRC AT L/W FLAP FAIRING #3 POSITION B737 SRM SOPM 50-20-19SDR SWIA202055775Skin · chafedRH IB FLAP VANE LEADING EDGE IS CHAFED AT ALL 3 CONTACT POINTS (C-CHECK) RO 2/1/2021 REMOVED CHAFED DAMAGED R/H FLAP VANE LEADING EDGE SKINS. LOCATED, DRILLED, INSTALLED,ALODINED,PRIMED, AND TOPCOATED 3 NEW SERVICEABLE R/H I/B FLAP VANE LEADING EDGE SKINS SDR SWIA202055774Skin · chafedLH IB FLAP VANE LEADING EDGE IS CHAFED AT ALL 3 CONTACT POINTS (C-CHECK) RO 2/1/2021 REMOVED AND REPLACED LH IB FLAP VANE LEADING EDGE AT 3 CHAFED CONTACT POINTS IAW CRJ 200 SRM 51-42-10. REFER TO CONTINUATION CARD FOR DETAILED WORK PERFORMED.SDR FDEA202012013094Skin · delaminatedLT OUTBOARD AFT FLAP LOWER SURFACE REPAIR AT 102 INCHES FROM INBOARD EDGE AND 10 INCHES FROM THE AFT EDGE REPAIR, REQUIRES EVALUATION TO DETERMINE IF IT WAS ACCOMPLISHED IN ACCORDANCE WITH APPROVED DATA. EVALUATED REPAIR IAW EO F-5100-7-5001 A6 PT1. STRUCTURSDR FDEA202012013011Skin · delaminatedDURING AGING AIRCRAFT INSPECTION FOUND LT OUTBOARD AFT FLAP LOWER INBOARD SKIN TO BE DELAMINATED. REMOVED FINISH, EVALUATED, REMOVED DAMAGE, AND REPAIRED LT OUTBOARD AFT FLAP, IAW B757 SRM 57-53-01-2R TABLE 2, 51-70-04-0G PARA 4A-I. MAJOR REPAIR.SDR SWIA202055446Vane · damagedREPLACE RT WING INBOARD FLAP VANE OUTBOARD LEADING EDGE. C-CHECK RO 1/16/2021. REPLACED RT WING INBOARD FLAP VANE ONBOARD LEADING EDGE WITH A SERVICEABLE UNIT, REF CRJ-200 SRM 51-42-13, CRJ-200-SRM 51-40-11, AND DWG 601R14303 REV J. COMPLIED WITH TASK CARD SDR SWIA202055445Vane · damagedREPLACE RT WING INBOARD FLAP VANE CENTER OUTBOARD LEADING EDGE. C-CHECK RO 1/16/2021. REMOVED AND REPLACED RIGHTHAND WING INBOARD FLAP VANE CENTER SKIN OUTBOARD LEADING EDGE, IAW CRJ200 SRM 51-42-13 AND DRAWING 601R14303 REV J. SEE CONTINUATION FOR FUTHER DSDR SWIA202055444Vane · damagedREPLACE RT WING INBOARD FLAP VANE INBOARD LEADING EDGE. C-CHECK RO 1/16/2021. REPLACED RT WING INBOARD FLAP VANE INBOARD LEADING EDGE WITH A SERVICEABLE UNIT, REF CRJ-200 SRM 51-42-13, CRJ-200 SRM 51-40-11, AND DWG 601R14303 REV J. COMPLIED WITH TASK CARD 5SDR AALA202012079022Skin · delaminatedAIRCRAFT IN BASE MAINTENANCE. LEFT WING INBOARD TRAILING EDGE FLAP, UPPER SURFACE SKIN DISBONDED BETWEEN RIB 1 AND RIB 3 AT 5.5 INCHES FROM INBOARD EDGE. REPAIRED FLAP, PER SRM 57-52-00-300-095.SDR KCSA202011301171Roller · missingRT INBOARD MIDFLAP OUTBOARD GUIDE ROLLER MISSING.SDR KCSA202011301170Web · crackedWEB DAMAGE ON RT INBOARD MIDFLAP ON OUTBOARD EDGE. WBL 445, 15.750" FROM FWD EDGE.SDR SWIA202055727Skin · dented*L/H WING I/B FLAP LOWER CENTER T/E SKIN IS DENTED (C-CHECK) RO 1/29/2021 REMOVED AND REPLACED THE L/H I/B FLAP REF CRJ 200 AMM 27-54-01-400-801. CHECKS GOOD.SDR SWIA202055681Skin · dented*R/H WING I/B FLAP LOWER CENTER T/E SKIN IS DENTED. (C-CHECK) RO 1/29/2021 REPAIRED DAMAGE ON R/H WING I/B FLAP LOWER CENTER T/E SKIN REF CRJ 200 SRM 57-52-00 REPAIR NO.3 COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY.SDR R61A2020122000908Pan · corrodedLT WING, INBOARD AFT FLAP FAIRING PANEL 562AB, CHAFED AND 2 BONDING PLATES CORRODED. REPAIRED IAW SRM 51-73-00 REV 44.SDR SWIA202054607Flap Track · out of limitsRT WING FLAP TRACK 1A HAS DEPTH REDUCTION OF 0.030", OUT OF LIMITS. ASSET NR 7153 DUE: 11-17-21. C-CHECK RO 12/10/2020. REMOVED AND REPLACED RT WING FLAP TRACK 1A, REF AMM TQ WRENCH HG2-50003 DUE CAL 04-30-21, HG2-696 DUE CAL 04-07-21.SDR FDEA202011253066Skin · dentedLT INBOARD MAIN FLAP UPPER SURFACE HAS SMALL PUNCTURE HOLE. REPAIRED DAMAGES, IAW SRM 51-70-07-0G AND FEDEX EA F-5730-T0358461 "WING-FLIGHT SURFACES-LT INBOARD MAIN FLAP COMPOSITE REPAIR-RSC TRACKING."SDR DU4R2020112500054Skin · dentedDURING SCHEDULED INSPECTION, FOUND 2 EACH DENTED AREAS THAT REQUIRED A PERMANENT REPAIR, IAW A320 SRM 57-33-00-300-102 ZONE 2 PG 3 AND A320 SRM 57-33-00-300-100 ZONE 2 PG 3-5. S/O 193116 ROUTINE NR 9004.SDR DALA2020112403849Skin · wornRT OUTBOARD FLAP TRAILING EDGE LOWER SKIN WORN, REF ERA 588686-14. CORRECTIVE ACTION: REF ERA 588686-14 REF ORIG.SDR DALA2020112403848Skin · wornLT OUTBOARD FLAP TRAILING EDGE LOWER SKIN WORN, REF ERA 588685-14, SEC I, STEP 6, REV O. CORRECTIVE ACTION: REF ERA 588685-14 REV ORIG.SDR DALA2021031601473Skin · damagedSHIP 3504 DAMAGE ON THE LH IB FLAP TRAILING EDGE UPPER SKIN. CORRECTIVE ACTION: COMPLIED WITH ER/A 588651-14 PERMANENT REPAIR. (1661440)SDR SWIA202056005Panel · chafedL/H WING INBOARD FLAP L/E PANEL 584ET , HAS CHAFFING CONDITION (C-CHECK) RO 2/5/2021 REMOVED PNL 584ET, BLENDED DAMAGE, DETERMINED TO EXCEED LIMITS IAW CRJ700 SRM 57-52-01-101-001-A01, ORDERED AND RECIEVED NEW PANEL P/N CC670-14027-3, LOCATED,DRILLED AND SDR SWIA202055926Skin · chafed*R/H INBD FLAP LWR SKIN IS CHAFED WHERE INBD HINGE FAIRING CONTACTS SURFACE. AREA MARKED. (C-CHECK) RO 2/1/2021 COMPLIED WITH REO 690-57-52-367 REV-- DATE 2020-11-26 STEPS.1-4 (SEE CONTINUATION FOR FURTHER DETAILS)SDR SWIA202055786Skin · chafed*L/H INBD FLAP LWR SKIN IS CHAFED WHERE INBD HINGE FAIRING CONTACTS SURFACE. AREA MARKED. (C-CHECK) RO 2/1/2021 BLENDED L\H INBD LWR FLAP SKIN WHERE INB HINGE FAIRING CONTACTS SURFACE REF CRJ900 SRM 51-12-00-001-001-A01. EVALUATED AND FOUND TO BE OUT OF LSDR SWIA202055785Vane · chafed*L/H INBD FLAP VANE HAS 2EA SMALL CHAFES ON UPPER SURFACE AT CENTER AFT AREA. AREA MARKED. (C-CHECK) RO 2/1/2021 (L/H INBD FLAP VANE 2EA. SMALL CHAFES ON UPPER SURFACE AT CENTER AFT AREA) ORIGINAL MATERIAL THICKNESS BLEND OUT #1 IS .050", REMAINING MATERIASDR SWIA202055498Vane · dentedLT INBOARD FLAP VANE LEADING EDGE IS DENTED AT WS 140 APPROXIMATELY .250 IN DIAMETER X .030 IN DEEP. C-CHECK RO 1/16/2021. REMOVED AND REPLACED DAMAGED LT INBOARD FLAP VANE LEADING EDGE WITH NEW SERVICEABLE PN 601R14303-43S, IAW CRJ 200 SRM 51-42-13, FORM 33SDR SWIA202055496Vane · chafedLT INBOARD FLAP VANE LEADING EDGE IS CHAFED AT WS 56 APPROXIMATELY 1 IN LONG X .5 IN WIDE X .015 DEEP. C-CHECK RO 1/16/2021. REPLACED THE LT INBOARD FLAP VANE INBOARD LEADING EDGE SKIN, IAW CRJ 200 SRM 51-42-13 AND 51-40-11 REV B DATED 11/25/2020, TASK CARD SDR SWIA202055495Vane · chafedLT INBOARD FLAP VANE LEADING EDGE IS CHAFED AT WS 105 APPROXIMATELY 1 IN LONG X .5 IN WIDE X .015 IN DEEP. C-CHECK RO 1/16/2021. INSTALLED NEW SERVICEABLE LT FLAP VANE LEADING EDGE, IAW CRJ 200 SRM 51-42-13 AND SKYWEST TASK CARD 51-900-1003-SKY. FORM M-337 SDR SWIA202055404Vane · chafedLT WING INBOARD FLAP (CENTER OUTBOARD) VANE IS CHAFED. C-CHECK RO 1/16/2021. REMOVED AND REPLACED LT WING INBOARD FLAP (CENTER OUTBOARD) VANE, REF CRJ-200 SRM 51-42-13 AND DWG 601R14302 REV E. SEE CONTINUATION CARD FOR DETAILS. COMPLIED WITH TASK CARD 51-9SDR SWIA202055403Vane · chafedLT WING INBOARD FLAP (INBOARD) VANE IS CHAFED. C-CHECK RO 1/16/2021. INSTALLED NEW PANEL PN 601R14303-53, REF CRJ200 SRM 51-42-13 AND DWG 601R14303 REV J. COMPLIED WITH 51-900-1003-SKY. SEE CONTINUATION CARD FOR DETAILS.SDR SWIA202055997Bolt · corroded* CORROSION DETECTED ON (BOLT HEADS) ON L/H OTBD FLAP, (INBD) HINGE BOX, (FWD) SUPPORT FITTING (WING PLANK SIDE), ATTACHING HARDWARE (MARKED). (C-CHECK) RO 2/5/2021 - INSTALLED 6 NEW BOLTS AND ATTACHING HARDWARE ON TO FLAP HINGE BOX SUPPORT FITTING AT WS17SDR SWIA202055046Nut · corrodedRIGHT SIDE FLAP BPSU MOUNTING BOLT NUT IS CORRODED. C-CHECK RO 12/30/2020. REMOVED AND REPLACED RIGHT SIDE FLAP BPSU MOUNTING BOLT NUT, IAW AMM.
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