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.

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-0Jan 13, 2021 · N566WN · Boeing 7377CTSDR 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 TOOLJan 13, 2021 · N566WN · Boeing 7377CTSDR MK1Y01132021007Skin · corrodedDURING MAINTENENCE INSPECTION FOUND CORROSION DAMAGE ON RT WING TRAILING EDGE INBOARD FLAP, REAR SPAR, UPPER CHORD, IFS 166.0.Jan 13, 2021 · N388AA · Boeing 767323SDR 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.Jan 12, 2021 · N140UP · Airbus A300F4622RSDR 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 Jan 12, 2021 · N583FE · Doug MD11FSDR 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 ( Jan 12, 2021 · N583FE · Doug MD11FSDR 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 Jan 12, 2021 · N498CA · Cndair CL6002B19SDR 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. MINORJan 12, 2021 · N255UP · Doug MD11FSDR 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.Jan 10, 2021 · N958SW · Cndair CL6002B19SDR 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 OJan 10, 2021 · N958SW · Cndair CL6002B19SDR 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-A01Jan 10, 2021 · N760SK · Cndair CL6002C10SDR K11A2021020300042Attach Bracket · corrodedL/H WING O/B MIDFLAP BALLNUT SCREW ATTACHMENT BRACKET I/B LOWER BOLTHOLE HAS CORROSION ON INNER DIAMETER.Jan 10, 2021 · N730CK · Boeing 7374C9SDR 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 HOLEJan 10, 2021 · N730CK · Boeing 7374C9SDR 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 MJan 9, 2021 · N551WN · Boeing 73776QSDR 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 51-25-01-001-001Jan 9, 2021 · N162PQ · Cndair CL6002D24SDR 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.Jan 9, 2021 · N162PQ · Cndair CL6002D24SDR 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-A01Jan 9, 2021 · N162PQ · Cndair CL6002D24SDR 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 AFJan 7, 2021 · N494WN · Boeing 7377H4SDR 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 OUTBOAJan 7, 2021 · N494WN · Boeing 7377H4SDR 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 OUTBJan 7, 2021 · N494WN · Boeing 7377H4SDR 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 SRMJan 7, 2021 · N270UP · Doug MD11FSDR 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 Jan 6, 2021 · N958SW · Cndair CL6002B19SDR 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 T080515Jan 5, 2021 · N564WN · Boeing 73773VSDR 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 220275Jan 5, 2021 · N162PQ · Cndair CL6002D24SDR 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.Jan 5, 2021 · N162PQ · Cndair CL6002D24SDR 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. INSTJan 5, 2021 · N162PQ · Cndair CL6002D24SDR 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 CONTINUJan 5, 2021 · N162PQ · Cndair CL6002D24SDR 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 SRJan 5, 2021 · N162PQ · Cndair CL6002D24SDR 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.Jan 5, 2021 · N913FX · Aerosp ATR42300SDR 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. MINORJan 5, 2021 · N270UP · Doug MD11FSDR 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 SRMJan 3, 2021 · N760SK · Cndair CL6002C10SDR 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 Dec 30, 2020 · N837VA · Airbus A320214SDR 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.Dec 29, 2020 · N717EV · Cndair CL6002C10SDR 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.Dec 29, 2020 · N717EV · Cndair CL6002C10SDR 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 Dec 29, 2020 · N717EV · Cndair CL6002C10SDR 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-Dec 28, 2020 · N246PS · Cndair CL6002B19SDR 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 OPERATDec 27, 2020 · N852GT · Boeing 74787UFSDR P5CA2020122800410Fairing · missingTHE NR 2 TRAILING EDGE FLAP FAIRING MISSING. A/C DISPATCHED IAW CDL 27-51-02, MDDR 140129.Dec 27, 2020 · N852GT · Boeing 74787UFSDR 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.Dec 23, 2020 · N506CA · Cndair CL6002B19SDR 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.Dec 23, 2020 · N506CA · Cndair CL6002B19SDR 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.Dec 22, 2020 · N345NW · Airbus A320212SDR 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.Dec 21, 2020 · N801NW · Airbus A330323SDR 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)Dec 19, 2020 · N263UP · Doug MD11FSDR 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: 001980Dec 18, 2020 · N412WN · Boeing 7377H4SDR 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.Dec 18, 2020 · N708SK · Cndair CL6002C10SDR 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).Dec 18, 2020 · N263UP · Doug MD11FSDR 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).Dec 18, 2020 · N263UP · Doug MD11FSDR 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.Dec 18, 2020 · N311PQ · Cndair CL6002D24SDR 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 ISDec 15, 2020 · N202AV · Cessna 650SDR 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 005029Dec 14, 2020 · N8605E · Boeing 7378H4
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