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 SWAA2021021841792Access Panel · crackedCRACK ACCESS PANEL 644BB ON PRELOAD PAD; FLAP SUPPORT 8 RT WING (2 EA) / REPLACED ON ACCESS PANEL 644BB PRELOAD PAD; FLAP SUPPORT 8 RT WING 2E/A IAW B737-700 SRM 51-40-02 -0G-0SDR SWAA2021021841791Access Panel · crackedCRACK ACCESS PANEL 643BB ON PRELOAD PAD; FLAP SUPPORT FAIRING 7 RT WING (2 EA). REPLACED PRELOAD PAD 2 E/A ON FLAP TRACK FAIRING 7 (643BB) AT RT WING IAW SRM 51-40-02 AND PERFORMED O/B FLAP I/B SUPPORT FAIRING ADJUSTMENT IAW B737-700 AMM 27-51-28-820-802 TOOLSDR MK1Y01132021007Skin · corrodedDURING MAINTENENCE INSPECTION FOUND CORROSION DAMAGE ON RT WING TRAILING EDGE INBOARD FLAP, REAR SPAR, UPPER CHORD, IFS 166.0.SDR IPXA2021021265619Roller · wornINSPECTION TYPE:SEGRH WING OUTBOARD FLAP UPPER L/E SURFACE ROLLER WEAR PLATES ARE GOUGED/WORNREMOVED AND REPLACED STRIP ROLLER IAW A300 SRM 51-40-21.SDR FDEA202101120063Bracket · corrodedRIGHT HAND WING TRAILING EDGE - UPON REMOVAL OF INBOARD FLAP OUTBOARD HINGE FORWARD HALF (WING SIDE) PIVOT BORE BUSHING FOUND BORE WITH CORROSION. CORROSION AT RIGHT HAND WING TRAILING EDGE - INBOARD FLAP OUTBOARD HINGE FORWARD HALF (WING SIDE) PIVOT BORE SDR FDEA202101120062Bracket · corrodedLEFT HAND WING TRAILING EDGE - UPON REMOVAL OF INBOARD FLAP OUTBOARD HINGE FORWARD HALF (WING SIDE) PIVOT BORE BUSHING FOUND BORE WITH CORROSION. CORROSION AT LEFT HAND WING TRAILING EDGE - INBOARD FLAP OUTBOARD HINGE FORWARD HALF (WING SIDE) PIVOT BORE ( SDR SWIA202155734Skin · dentedLEFT INBOARD FLAP LOWER SKIN HAS 3 DENTS INBOARD OF THE INBOARD HINGE ARM. (C-CHECK) RO 2/1/2021 REMOVED DAMAGED SKIN PANEL 601R-14028-45 AND INSTALLED NEW SERVICEABLE SKIN SECTION 601R-14028-45 IAW CRJ-200 SRM 51-42-13. SEE CONTINUATION CARD FOR DETAILS SDR IPXA2021020165134Mount Fitting · crackedINSPECTION TYPE :2C RT WING OB FLAP IB AFT HINGE FAIRING FWD, CENTER MOUNT FITTING SUPPORT IS CRACKED. REMOVED, FABRICATED AND REPLACED SUPPORT IAW DWG. ARC22356 AND SRM 51-31-01. MINORSDR SWIA202156867Fairing · chafedRH FLAP STUB FARING IS CHAFED AND SEALS ARE WORN (C-CHECK) RO 3/10/2021 REPLACED THE RIGHT FLAP STUB FARING IAW CRJ-200 SRM 51-42-06.SDR SWIA202156866Fairing · chafedLH FLAP STUB FARING IS CHAFED AND SEALS ARE WORN (C-CHECK) RO 3/10/2021 REMOVED AND REPLACE THE LH STAB FARING RIB P/N 601R31199-89 AND SEALS 601R31199-99 AND 601R31199-81 IAW CRJ 200 SRM 51-42-06 AND 51-40-11 REF ATTACHED CONTINUAITON CARD FOR DETAILS OSDR SWIA202156299Bracket · brokenRH WING O/B FLAP MOST O/B HINGE ARM BRACKET BROKEN. (C-CHECK) RO 2/13/2021 INSTALLED NEW RH WING O/B FLAP HINGE ARM BRACKET REF CRJ700 SRM 51-42-10-001-001-A01 AND CRJ700 SRM 51-42-06-001-001-A01SDR K11A2021020300042Attach Bracket · corrodedL/H WING O/B MIDFLAP BALLNUT SCREW ATTACHMENT BRACKET I/B LOWER BOLTHOLE HAS CORROSION ON INNER DIAMETER.SDR K11A2021020200040Attach Bracket · corrodedL/H WING O/B MIDFLAP BALLNUT SCREW ATTACHMENT BRACKET O/B HAS BOLT HOLE WITH CORROSION ON THE O/B LOWER BOLT HOLESDR SWAA2021071340595Skin · delaminatedL/H WING OUTBOARD AFT FLAP IS DELAMINATED AT INBOARD TRAILING EDGE 1.25' INBD LOWER EDGE. LENGTH = 3.25'; WIDTH = .50' MOD / C) INSPECTION COMPLIED WITH; ADDITIONAL DAMAGE OR DETERIORATION WAS FOUND. CONDITION HAS BEEN CORRECTED AS NOTED ON: NEW NRC: U293604 MSDR SWIA202156719Access Panel · chafedRH INBOARD FLAP PANEL 684AB IS CHAFFED. (C-CHECK) RO 3/4/2021 EVALUATED RH INBD FLAP PANEL 684AB OUT OF LIMITS REF CRJ900 SRM 57-52-01-101-001-A01. DRILLED AND LOCATED NEW PANEL AND RESTORED FINISH REF CRJ900 SRM 51-40-11-001-001-A01 AND 51-25-01-001-001SDR SWIA202156718Panel · chafedRH INBOARD FLAP PANEL 684GB IS CHAFFED. RH INBOARD FLAP PANEL 684GB EVALUATED OUT OF LIMITS REF CRJ900 SRM 57-52-01-101-001-A01. REPLACED PANEL REF CRJ900 SRM 51-40-11-001-001-A01 AND 51-25-01-001-001-A01.SDR SWIA202156717Panel · chafedRH INBOARD FLAP PANEL 684EB IS CHAFFED. (C-CHECK) RO 3/4/2021 AFTER REMOVAL FOUND FLAP PANEL 684EB TO BE WORN BEYOND ALLOWABLE LIMITS REF: CRJ900 SRM 57-52-01-101-001-A01. LOCATED AND DRILLED REPLACEMENT PANEL 684EB REF: CRJ900 SRM 51-40-11-001-001-A01SDR SWAA2021071340081Skin · delaminatedREFERENCE ORIGINAL DEFECT# 1187133. LEFT WING OUTBOARD TRAILING EDGE AFT FLAP SKIN DELAMINATION/DISBOND. DAMAGE MEASURES 5' IN LENGHT FROM LOWER INBOARD EDGE SKIN SPANWISE AND 0.75' LOWER AFT EDGE SKIN CHORDWISE. / DMA# 1187133 REMOVED AND REPLACED OUTBOARD AFSDR SWAA2021071340080Skin · delaminatedREFERENCE ORIGINAL DEFECT# 1187131. LEFT WING OUTBOARD TRAILING EDGE AFT FLAP SKIN DELAMINATION/DISBOND. DAMAGE MEASURES 5' IN LENGHT FROM LOWER INBOARD EDGE SKIN SPANWISE AND 0.75' FROM LOWER AFT EDGE SKIN CHORDWISE. / DMA# 0258744 REMOVED AND REPLACED OUTBOASDR SWAA2021060439963Skin · delaminatedDURING MAINTENANCE CHECK; FOUND LEFT WING OUTBOARD TRAILING EDGE AFT FLAP SKIN DELAMINATION/DISBOND. DAMAGE MEASURES 5' IN LENGHT FROM LOWER INBOARD EDGE OF SKIN SPANWISE AND 0.75' FROM LOWER AFT EDGE OF SKIN CHORDWISE. / DMA# 0258743 REMOVED AND REPLACED OUTBSDR IPXA2021012664888Skin · dentedINSPECTION TYPE: 2C RT WING INBOARD FLAP NR 2 ROLLER ACCESS COVER IS DENTED AND GOUGED AT STA XIFH=185.13 AND BETWEEN YIFH=7.6 & YIFH= -6.0. REPAIRED DENTED RT INBOARD FLAP NR 2 ROLLER ACCESS COVER AT STA XIFH=185.13 AND BETWEEN YIFH=7.6 & YIFH= -6.0, IAW SRMSDR SWIA202156849Skin · chafedL/H I/B FLAP VANE SKIN IS CHAFED INTO BARE METAL LARGE AREA I/B L/E AND CENTER L/E THREE SPOTS AND LARGE AREA O/B L/E . ALSO UPPER CENTER SKIN RIVET HEADS HAVE BARE METAL SHOWING AND LOWER I/B T/E HAS PAINT MISSING INTO PRIMER. (C-CHECK) RO 3/10/2021 SDR SWAA2021071339870Skin · debondedDEBONDED OB AFT FLAP IB CORNER T/E AT LT WING / REPAIRED OB AFT FLAP IB CORNER T/E AT LT WING ASPER B737-700 SRM 57-53-01-2R-16.REPAIR 16 AND B737-700 SRM 51-70-10-2R-0. REPAIR GENERAL. THIS IS ON INTERIM REPAIR. FOR INSPECTIONS REQUIREMENTS SEE TLD T080515SDR SWIA202156714Panel · chafed* THE RH INBOARD FLAP VANE PANEL 684HT IS CHAFED (C-CHECK) RO 3/4/2021 CHAFE DAMAGE BEYOND ALLOWABLE DAMAGE LIMITS. REMOVED AND REPLACED WITH NEW 684HT PANEL REF CRJ 900 SRM 51-40-11-001-001-A01. SEE CONTINUATION CARD FOR DETAILS. INSTALLED ON CAMP 220275SDR SWIA202156713Panel · chafed* THE RH INBOARD FLAP VANE PANEL 684ET IS CHAFED. (C-CHECK) RO 3/4/2021 CHAFE IS BEYOND ALLOWABLE DAMAGE LIMITS ON 684ET. REMOVED AND REPLACED 684ET REF CRJ 900 SRM 51-40-11-001-001-A01. SEE CONTINUATION CARD FOR DETAILS. INSTALLED ON CAMP 22027515.SDR SWIA202156712Vane · chafed* THE LH INBOARD FLAP VANE PANEL 584HT IS CHAFED. (C-CHECK) RO 3/4/2021 FOUND REMAINING MATERIAL ON 584HT TO BEYOND ALLOWABLE DAMAGE LIMITS. REMOVED AND REPLACED WITH NEW 584HT REF CRJ 900 SRM 51-40-11-001-001-A01. SEE CONTINUATION CARD FOR DETAILS. INSTSDR SWIA202156711Vane · chafed* THE LH INBOARD FLAP VANE PANEL 584ET IS CHAFED. (C-CHECK) RO 3/4/2021 (C-CHECK) RO 3/4/2021 FOUND REMAINING MATERIAL ON 584ET TO BEYOND ALLOWABLE DAMAGE LIMITS. REMOVED AND REPLACED WITH NEW 584ET REF CRJ 900 SRM 51-40-11-001-001-A01. SEE CONTINUSDR SWIA202156594Skin · dented* THE RH WING INBOARD FLAP PANEL HAS A DENT ON ITS LOWER SKIN NEAR THE TRAILING EDGE BETWEEN FLS112.30 AND FLS120.20. (MARKED WITH RED GREASE PENCIL) (C-CHECK) RO 3/4/2021 COMPLIED WITH NON-FLUSH PERMANENT REPAIR TO THE RH IB FLAP LOWER SKIN REF CRJ 900 SRSDR COEA2021021205913Guide · crackedWO 223107 NR 500011 HEAVY CHECK COE/MAJOR REPAIR: LH OUTBOARD FLAP 2ND FROM OUTBOARD CAM GUIDE IS CRACKED. CORRECTIVE ACTION: REPAIRED PER SRM 575320-300-801-A01.SDR IPXA2021013165119Attach Fitting · crackedINSPECTION TYPE: 2 CR H OB FLAP IB HINGE ATTACH FITTING INSIDE FLAP IS CRACKED AT LOWER END. R & R RT OB FLAP IAW EO MD11-5750-959-D. MINORSDR SWIA202156247Skin · dented*RH WING INBD FLAP HAS 3EA SMALL DENTS/NICKS ON LOWER SKIN. AREAS MARKED. (C-CHECK) RO 2/13/2021 REPAIRED RH IB FLAPS BY CUTTING OUT DENTS AND INSTALLING NEW REPAIR PARTS REF CRJ-700 SRM 57-52-01-201-005-A01, CRJ-700 SRM 51-42-13-001-001-A01, CRJ-700 SRMSDR ASAA2020123033777Skin · dentedUPON WALK AROUND FOUND DENT ON LT INBOARD FLAP LOWER. GROUNDED-YES. RESOLVED ON W/O: 376466 TASKCARD: N/R-00004. ACCOMPLISHED A MAJOR REPAIR TO THE LT INBOARD FLAP LOWER SKIN, IAW A320 SRM 57-52-00-300-093. NO REINSPECT REQUIRED. NOTIFIED DARWIN; CLEARED SDR SWIA202056925Slat Track · corroded* RH SLAT TRACK 2-2 HAS PITTING CORROSION (C-CHECK) RO 3/11/2021 COMPLIED WITH ALL STEPS OF REO 670-57-42-988 REV -- DATED 2021-01-10 AS REQUIRED. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. SEE CONTINUE CARD FOR DETAILS.SDR SWIA202056924Slat Track · corroded* RH SLAT TRACK 1-2 HAS PITTING CORROSION (C-CHECK) RO 3/11/2021 COMPLIED WITH ALL STEPS OF REO 670-57-42-986 REV -- DATED 2021-01-10 AS REQUIRED. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. SEE CONTINUE CARD FOR DETAILS. COMPLIED WITH M-337.SDR SWIA202056923Slat Track · corroded* LH SLAT TRACK 2-2 HAS PITTING CORROSION (C-CHECK) RO 3/11/2021 LH SLAT TRACK 2-2 CORROSION WAS BLENDED WITH THE NEXT DIMENSIONS: BLEND #1 1.60" L, 0.50" W, 0.002" D; BLEND #2 1.60" L, 0.80" W, 0.003" D. MIN FLANGE THICKNESS 0.250" AND MIN. TRACK HEIGHT SDR SWIA202056408Hinge Bracket · chafedRIGHT WING FLAP HINGE ARMS (BOTH WS80.50 AND WS127.25) FAIRING PLATE PANELS HAVE CHAFE MARKS IN RADIUS OF BRACKET INTO BARE METAL. (C-CHECK) RO 2/21/2021. REMOVED AND INSTALLED NEW SERVICEABLE SIDE PLATES AND BRACKET IAW CRJ 200 SRM 51-42-06,51-42-15 AND 51-SDR 3BSY20210104001Fairing · missingON 27 DECEMBER 2020, WHEN POLAR N852GT LANDED AT PVG (PUDONG AIRPORT) SHANGHAI, THE NR 2 FLAP TRACKING FAIRING WAS FOUND MISSING DURING WALK AROUND CHECK. THE OPERATOR WAS NOTIFIED. AFTER THAT, THE AIRCRAFT OPERATION CONTROL CENTER OF THE AIRPORT TOLD OPERATSDR P5CA2020122800410Fairing · missingTHE NR 2 TRAILING EDGE FLAP FAIRING MISSING. A/C DISPATCHED IAW CDL 27-51-02, MDDR 140129.SDR SWIA202056355Bolt · corrodedWHILE REMOVING RT O/B FLAP HINGE ARM ASSEMBLIES AT WS 178.00 AND WS 264.00 FOUND HARDWARE TO BE CORRODED. (C-CHECK) RO 2/17/2021. RECEIVED SERVICEABLE HARDWARE. REFERENCE CAMP 21819157-1 FOR INSTALL.SDR SWIA202056354Bolt · corrodedWHILE REMOVING LT O/B FLAP HINGE ARM ASSEMBLIES AT WS 178.00 AND 264.00, FOUND HARDWARE TO BE CORRODED. (C-CHECK) RO 2/17/2021. RECEIVED SERVICEABLE PARTS. REFERENCE CAMP 21819156-1 FOR INSTALL.SDR DALA2020122304198Fairing · corrodedCORROSION FLAP TRACK FAIRING 633CB INTERNAL STRIP RT WING. CORRECTIVE ACTION: REPLACED BONDING PLATE ON FLAP TRACK FAIRING 633CB INTERNAL STRIP RT WING, AS PER ER/A 588948-14 PRI REV 0.SDR DALA2020122304233Skin · damagedCONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR INBOARD FLAP LEADING EDGE LOWER SKIN ON RT WING. CORRECTIVE ACTION: REPAIR INSTALLED PER ER/A NR 499303-14, REV B.SDR IPXA2021012264757Hinge Bracket · crackedINSPECTION TYPE: 3C RT WING INBOARD FLAP OUTBOARD FWD HINGE OUTBOARD UPPER AFT PANEL SUPPORT BRACKET IS CRACKED. REMOVED AND REPLACED CRACKED RT WING INBOARD FLAP OUTBOARD FWD HINGE O/B UPPER AFT PANEL SUPPORT BRACKET, IAW MD-11 SRM 51-35-01. (MINOR)SDR SWAA2021071337556Skin · delaminatedRIGHT WING O/B AFT TRAILING EDGE FLAP DELAMINATED AT I/B END / REMOVED AND REPLACED RIGHT WING OUTBD AFT FLAP REF MM 27-51-22 POS: 2 TAG: 731442 PN/OFF: 113A3700-20 S/N OFF: 000974 PN/ON: 113A3700-24 S/N ON: 001980SDR SWIA202056071Hinge Arm · gouged*RIGHT WING, INBOARD FLAP HINGE ARM AT WS128 HAS A GOUGED AND CHAFED GUIDE PLATE ON THE INBOARD SIDE. (FLAGGED) (C-CHECK) RO 2/6/2021 NEW SIDE PLATE P/N CC670-14146-2 INSTALLED PER CRJ700 SRM 51-42-06-001-001-A01 AND CRJ700 SRM 51-42-15-001-001-A01.SDR IPXA2021011964641Bracket · crackedINSPECTION TYPE: C3 RT WING FLAP HINGE FAIRING 635ML HAS 2 EA CRACK BRACKET. REMOVED AND REPLACED 2 EA CRACKED BRACKET AT RT WING FLAP HINGE FAIRING 635ML, IAW SRM 51-31-01 AND 51-35-02 (MINOR).SDR IPXA2021011964637Bracket · crackedINSPECTION TYPE: C3 RT WING FLAP HINGE FAIRING 636ML BRACKET CRACK. REMOVED AND REPLACED CRACKED RT WING FLAP FAIRING 636ML BRACKET, IAW SRM 51-31-01. (MINOR).SDR REXA2021011200862Skin · chafedRT WING INBD FLAP PANEL 684EB HAS A DEEP CHAFE. BLENDED CHAFE FOUND TO BE OUT OF LIMITS, IAW CRJ 900 SRM 57-52-01-001-001-A01. REPLACED 684EB PANEL, IAW CRJ 900 SRM 51-40-11-001-001-A01.SDR JGVR20201215002Screw · strippedWHILE ATTEMPTING TO REPLACE MOUNTING HARDWARE DUE TO HARDWARE BEING SEIZED IN PLACE ON LT AND RT FLAP ANGLE GEAR BOX PN: 9914393-1 WHICH CALLS FOR A PN: WD6000-21. WE HAD TO DRILL AND EXTRACT THE SCREWS. THIS PARTICULAR SCREW HAS A COUNTERSUNK HEAD, WHICH ISSDR SWAA2021071336439Skin · delaminatedLH OUTBD AFT FLAP LOWER SURFACE HAS DELAMINATION SPOT 10' X 13' AT LOWER INBD CORNER. / REMOVED & REPLACED L/H O/B AFT FLAP PER M/M 27-51-22 POS L/H TAG 457833 P/N OFF/ON 113A3700-25 S/N OFF 004333 S/N ON 005029
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