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 FDEA2020012740224Skin · chafedWEAR MARK AT LEFT IN-BOARD FLAP LEADING EDGE. ALL WORK ACCOMPLISHED IAW EA F-5750-T0352020 P1 WING - FLIGHT SURFACES - LT INBOARD MAIN FLAP LEADING EDGE SKIN REPAIR.SDR SWAA000021989Flap Track · looseRIGHT INBOARD AFT FLAP INBOARD AFT FLAP TRACK AFT BEARING LOOSE AND SPINNING / REMOVED AND INSTALLED SERVICEABLE RIGHT INBOARD AFT FLAP; INBOARD AFT FLAP TRACK IAW SRM 51-40-02-0G-0 STEP 9; AND AMM 27-51-16-400-801 STEPS 3.E.(1)(A)(B).SDR REXA2020021230193Skin · dentedLEFT INBOARD FLAP LOWER SKIN HAS DENT WITH GOUGE LOCATED AT FLAP STATION 74.8 (24.4"" OTBD OF INBD END), 5.1"" FWD OF TRAILING EDGE. MEASURES APPROX. 1.0"" X 1.0"" X 0.040"" WITH GOUGE.
REMOVED AND REPLACED DAMAGED I/B FLAP SKIN SDR SIMA202002043005Skin · dentedLH INBD FLAP HAS DENT ON OUTBD END LOWER SKIN-C/A-REMOVED AND REPLACED LOWER SKIN ON LH INBOARD FLAP FROM FL92.800 TO OUTBOARD EDGE IAW SRM 57-52-01. SEE DT-CR-57-069 DTI.SDR SWAA2020012740740Flap Track · looseRIGHT WING OUTBOARD AFT FLAP OUTBOARD TRACK LOOSE AT AFT ATTACH POINT. R & R THE FLAP TRACK IAW MM.SDR SWAA2020012740739Flap Track · looseRIGHT WING OUTBOARD AFT FLAP INBOARD TRACK LOOSE AT AFT ATTACH POINT. R & R THE FLAP TRACK IAW MM.SDR AALA202001249015Flap Track · wornAIRCRAFT IN BASE MAINTENANCE: RIGHT WING #1 FLAP TRACK INBOARD SIDE HAS THICKNESS AND WIDTH REDUCTOIN. REPLACED FLAP TRACK PER AMM 57-54-21-400-801-B/400.SDR REXA2020012820132Flap Track · corroded"INITIAL INSPECTION: PREVIOUS TOOL MARK ON SKIN (INNER FACE) IN STA. FSL 36.00 FLS TO FSL 42.00 (AD)(BORESCOPE)
""PREVIOUS TOOL MARK ON SKIN (INNER FACE) IN STA. FSL 36.00 FLS TO FSL 42.00 WAS BLENDED OUT PER CRJ900 SRM 51-12-00-SDR SWAA2020012840847Skin · delaminatedUPPER RT CORNER OF LEFT SIDE TRAILING EDGE FLAP DELAMINATED. R & R LT WING OUTBOARD AFT FLAP ASSEMBLY IAW AMM.SDR REXA2020012820083Access Panel · worn"POST-PART RACKS :WEAR ON FLAP ACCESS PANEL 684HT, 684FT, 684ET, 584HTAND 584ET. (AI)(AD).
"ACCESS PANEL 684ET WAS REPAIRED PER EA CRJ957-10144 REV. ""IR"", 684HT REPAIRED PER EA CRJ957-10139 REV. ""IR"", 584HTSDR REXA2020012820061Retainer · bent"PART RACKS: BENT ON SEAL RETAINER OF FLAP HINGE FAIRING LH WING NBR 597BB OUTBD SIDE.(SM)(AI)
""AFT HINGE FAIRING ASSY P/N:CC670-17900-1 WAS REPLACED FOR SERVICEABLE AND VERIFIED PER CRJ900 AIPC 57-51-84-20. FIGSDR DALA2020012400590Fairing · missingRIGHT WING OUTBOARD FLAP TRACK FAIRING OUTBOARD SIDE, 1 SMALL PANEL MISSING. DEFERRED CDL 57-00-05B UNTIL PANEL IS AVAILABLE TO REPLACE. LP 7142004SDR FDEA202001210183Hinge Bracket · corrodedRIGHT HAND WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE) PIVOT OUTBOARD HOLE BORE CORROSION. CORROSION AT RIGHT HAND WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE) PIVOT OUTBOARD HOLE BORE (HOLE A AND B) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-5SDR FDEA202001210182Hinge Bracket · corrodedRIGHT HAND WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE) PIVOT INBOARD HOLE BORE CORROSION. CORROSION AT RIGHT HAND WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE) PIVOT INBOARD HOLE BORE (HOLE G AND F) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-SDR SWAA2020012740765Plate · crackedRIGHT WING WIGGLE PLATE INBOARD OF NR 6 FLAP TRACK CRACKED. R & R WIGGLE PLATE IAW SRM.SDR C77A2020012100002Skin · fracturedDURING BASIC CHECK IN BNA, DAMAGE WAS SUSTAINED ON THE RH WING IB AFT FLAP DURING A MAINTENANCE CHECK. SOME FIBER LAYERS OF THE SKIN AT THE OUTBOARD TRAILING EDGE WERE FRACTURED ON BOTH SIDES AT A LENGTH OF APPROXIMATELY 5 INCHES, AND AN EDGE OF THE SKIN WAS FSDR FDEA2020012100175Hinge Bracket · corrodedLEFT HAND WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE) PIVOT OUTBOARD HOLE BORE CORROSION. CORROSION AT LEFT HAND WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE) PIVOT OUTBOARD HOLE BORE (HOLE A AND B) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52SDR FDEA2020012100174Hinge Bracket · corrodedLEFT HAND WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE) PIVOT INBOARD HOLE BORE CORROSION. CORROSION AT LEFT HAND WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE) PIVOT INBOARD HOLE BORE (HOLE G AND F) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52- 0SDR SWAA2021071322879Skin · delaminatedLEFT HAND OUTBOARD AFT FLAP INBOARD TRAILING EDGE DELAMINATED / REPAIRED DELAMINATION DAMAGE ON I/B TRAILING EDGE OF L/H O/B AFT FLAP IAW 737 57-53-01-2R-4 AND SRM 51-70-10-2R-4 AND SRM 51-70-10-2R-0SDR SWAA2020012040555Flap · delaminatedLT WING OUTBOARD TRAILING EDGE AFT FLAP DELAMINATED. REPAIRED AFT FLAP PER EA.SDR SWAA2020012040554Flap · delaminatedLT WING OUTBOARD TRAILING EDGE AFT FLAP DELAMINATED. REPAIRED AFT FLAP PER EA.SDR AALA202001239018Tab · crackedAIRCRAFT IN BASE MAINTENANCE: LEFT WING INBOARD TRAILING EDGE FLAP TAB CRACKED 46 INCHES OUT BOARD OF THE INBOARD EDGE AND 1 INCH FORWARD OF THE TRAILING EDGE. REPAIRED FLAP TAB PER SRM 57-52-00-300-015.SDR AALA2020012199012Bracket · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FLAP TRACK 3 BRACKET CARRIAGE OUTBOARD ON RIGHT WING. REPLACED FLAP TRACK #3 BRACKET (BRIDGE) CARRIAGE OB ON RIGHT WING PER CMMTASK 27-54-48-440-801-C01 STEP 1,2 AND 3.D (8) AND (9)SDR AALA202001219021Rib · crackedAIRCRAFT IN BASE MAINTENANCE: LEFT WING INBOARD TRAILINING EDGE FLAP SUPPORT BACK UP RIB CRACKED. REPAIRED RIB PER EA 302132.SDR FDEA2020012180165Bushing · corrodedRW CENTER FLAP O/B AFT LINK UPPER ATTACH LINK BUSHING IS CORRODED AND WORN REMOVED AND REPLACED IAW CMM 57-53-25SDR FDEA2020012180164Bushing · corrodedRW CENTER FLAP I/B AFT ATTACH LINK UPPER END BUSHING IS PITTED REMOVED AND REPLACED IAW CMM 57-53-25SDR LR7A2020012082226Skin · crackedDURING SCHEDULED B-3 CHECK UNDER JOB CARD HB2703, FOUND THE LH OUTBOARD FLAP LEADING EDGE SKIN LOWER SURFACE CRACKED AT OWFS285L, 37" FORWARD OF TRAILING EDGE. / REPAIRED IAW LOCKHEED SMP583 SRM FIG. 51-140-12. NR# 1000136435.SDR FDEA202001170157Support Fitting · corrodedLEFT WING - OUTBOARD FLAP VANE NUMBER 2 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORROSION CORROSION AT LEFT WING - OUTBOARD FLAP VANE NUMBER 2 SUPPORT FITTING ECCENTRIC HOLE BORE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02- 2RSDR FDEA202001170156Support Fitting · corrodedLEFT WING - OUTBOARD FLAP VANE NUMBER 1 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - OUTBOARD FLAP VANE NUMBER 1 SUPPORT FITTING ECCENTRIC HOLE BORE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02- 2SDR REXA2020012870088Access Panel · worn"POST-PART RACKS :WEAR ON FLAP ACCESS PANEL 584LB, 584GB, 584EB, 584JBAND 684EB. (AI)(AD).
""ACCESS PANEL 584LB,584GB,584EB,584JB AND 684EB WERE REPLACED PER CRJ 900 SRM 57-52-01-101-001-A01 AND SRM 51-40-11-00SDR REXA2020012870087Access Panel · worn"POST-PART RACKS :WEAR ON FLAP ACCESS PANEL 584LB, 584GB, 584EB, 584JBAND 684EB. (AI)(AD).
"
"ACCESS PANEL 584LB,584GB,584EB,584JB AND 684EB WERE REPLACED PER CRJ 900 SRM 57-52-01-101-001-A01 AND SRM 51-40-11-SDR REXA2020012870086Access Panel · worn"POST-PART RACKS :WEAR ON FLAP ACCESS PANEL 584LB, 584GB, 584EB, 584JBAND 684EB. (AI)(AD).
"ACCESS PANEL 584LB,584GB,584EB,584JB AND 684EB WERE REPLACED PER CRJ 900 SRM 57-52-01-101-001-A01 AND SRM 51-40-11-001SDR REXA2020012870085Access Panel · worn"POST-PART RACKS :WEAR ON FLAP ACCESS PANEL 584LB, 584GB, 584EB, 584JBAND 684EB. (AI)(AD).
""ACCESS PANEL 584LB,584GB,584EB,584JB AND 684EB WERE REPLACED PER CRJ 900 SRM 57-52-01-101-001-A01 AND SRM 51-40-11-00SDR REXA2020012870084Access Panel · worn"POST-PART RACKS :WEAR ON FLAP ACCESS PANEL 584LB, 584GB, 584EB, 584JBAND 684EB. (AI)(AD).
"ACCESS PANEL 584LB,584GB,584EB,584JB AND 684EB WERE REPLACED PER CRJ 900 SRM 57-52-01-101-001-A01 AND SRM 51-40-11-001SDR SWIA2020012347978Structure · chafedR/H I/B AFT FLAP CHAFED THROUGH COPPER MESH AS MARKED. (C-CHECK) RO:1/22/2020 / RESTORED SURFACE PROTECTION TO R/H I/B AFT FLAP PER EMB SRM PO#258679 254901SDR SWAA2020021241350Skin · delaminatedR/H WING OUTBOARD AFT FLAP INBOARD LOWER CORNER DELAMINATED. / R&R AFT FLAP IAW AMM.SDR DALA2020012100414Cover · missingOUTBOARD SIDE OF LEFT FLAP TRACK FAIRING MISSING ONE COVER. DEFERRED PER CDL 57-00-07 UNTIL COVER IS AVAILABLE TO REPLACE. LP 6567780SDR SWIA2020031049232Guide · chafedCHAFFING ON THE GUIDES ON RIGHT HAND WING FLAP HINGE FAIRING 692BB. (C CHECK) RO 3/7/2020 REMOVED AND REPLACED GUIDES ON RIGHT HAND WING FLAP HINGE FAIRING 692BB REF CRJ-200 SRM.SDR IPXA2020021435285Hinge Bracket · crackedINSPECTION TYPE:2CL/H O/B FLAP I/B HINGE ASSY. HAS A CRACKED BRACKET.REMOVED AND REPLACED BRACKET IAW SRM 51-31-01. (MINOR)SDR SWIA2020021148414Fastener · corrodedINBOARD AND OUTBOARD FLAP PANEL SCREWS CORROATED. (C-CHECK) RO 2/07/2020 REPLACED 7 FASTENERS PART# AVL200-4-41R AND REPLACED CORROATED BOLTS WITH NEW ONES. PER CRJ-700 SRM.SDR A6WA2020011647107Skin · dentedLEFT WING INBOARD FLAP, OUTBOARD END HAS DENT. (OUTBOARD AND BELOW OF THE OUTBOARD FLAP ARM) AIRCRAFT REMOVED FROM SERVICE REPAIRED LEFT WING INBOARD FLAP OUTBOARD END LOWER SKIN IAW REO 601R-57-52-1544.SDR SWIA2020041050115Mount · chafedR/H OUTBOARD FLAP VANE MOUNTS HAVE SEVERE CHAFFING AT BUTE DOOR ROLLER CONTACT AREA'S. NEEDS FURTHER EVALUATION.R/H OUTBOARD FLAP WAS REMOVED AND REPLACED ON CAMP # 20262710. REFERNCE CAMP FOR WORK ACCOMPLISHED.SDR SWIA2020041050114Mount · chafedL/H OUTBOARD FLAP VANE MOUNTS HAVE SEVERE CHAFFING AT BUTE DOOR ROLLER CONTACT AREA'S. NEEDS FURTHER EVALUATION. (C-CHECK) RO 4/9/2020 L/H OUTBOARD FLAP WAS REMOVED AND REPLACED WITH A SERVICABLE FLAP ASSEMBLY. REFERENCE CAMP # 20266342SDR SWIA2020041050080Support · crackedR/H INBOARD FLAP HAS MULTIPLE CRACKS ON THE INTERNAL SUPPORT STRUCTURE FOR THE INBOARD AND OUTBOARD FLAP HINGE MOUNTS. (C-CHECK) RO 4/9/2020 R/H INBOARD FLAP REPLACED WITH NEW FLAP P/N ON: 601R14002-2, S/N ON: SB/RJ/113, P/N OFF: 601R14002-2, S/N OFF: SBSDR SWIA2020041050113Skin · chafedL/H INBOARD FLAP VANE HAS EXCESSIVE CHAFFING ON THE LEADING EDGE AT APPROXIMATELY WS 65.75, WS 97.70 AND WS 127.25. NEEDS FURTHER EVALUATION. (C-CHECK) RO 4/9/2020 L/H I/B FLAP ASSEMBLY WAS ORDERED. FLAP PARTS INFO AND INSTALLATION WILL BE REFERENCED ON CASDR SWIA2020041050112Skin · chafedR/H INBOARD FLAP HAS EXCESSIVE CHAFFING ON THE LEADING EDGE AT APPROX. W.S 65.75, W.S. 97.70, AND W.S.127.25. NEEDS FURTHER EVALUATION. (C-CHECK) RO 4/9/2020 R/H INBOARD FLAP WAS REMOVED AND REPLACED ON CAMP # 20262733. REFERENCE CAMP FOR WORK ACCOMPLISHEDSDR DALA2020011300009Tail Cone · missingDURING WALK AROUND, FOUND LEFT WING NBR 2 FLAP TRACK FAIRING TAIL CONE MISSING. DEFERRED PER CDL 57-00-04B UNTIL FAIRING TAIL CONE CAN BE PLACED. LP 6573291SDR SWIA2020021848751Access Panel · chafedRH WING INBD FLAP ACCESS PANEL 684EB IS CHAFED (MARKED) (C-CHECK) RO 2/14/2020 BLENDED CHAFE DAMAGE ON PANEL 684EB IAW CRJ700 SRM FOUND TO BE OUT OF LIMITS REF CRJ-700 SRM. REPLACED WITH NEW RH INBD FLAP ACCESS PANEL 684EB REF CRJ700 SRM. SEE CONTINUATION SDR FDEA202001100103Hinge Bracket · corrodedRIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT LUG HOLE BORE (HOLE A AND B) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57SDR FDEA202001100102Hinge Bracket · corrodedRIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT HOLE BORE (HOLE G AND F) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52- 03.
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