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 ASAA2024061351518Wedge · dentedLESSOR ITEM : L/H I/B FLAP DENTS REQUIRE MAPPING AND MEASURE FOR D&B RECORD AND SERVICEABILITY GROUNDED - YES. PERFORMED A CATEGORY A PERMANENT REPAIR OF THE LEFT-HAND INBOARD FLAP DENTS. THIS NON ROUTINE IS ONLY FOR DOCUMENTATION OF THE STRUCTURAL DIFFICULTYJun 13, 2024 · N361VA · Airbus A320214SDR IPXA2024072637979Rib · crackedLH CENTER FLAP CRACK RIB 25 ACCOMPLISH REPAIR IN ACCORDANCE WITH EO-90495-REQ1 AND VT-MAE EA 300-5750-27-A3607, REV. -. REVIEWEDJun 13, 2024 · N127UP · Airbus A300F4622RSDR IPXA2024061737979Rib · crackedLEFTCENTER FLAP CRACKED RIB 25.Jun 13, 2024 · N127UP · Airbus A300F4622RSDR DALA2024112111125Flap Track · corrodedSHIP 3134 LH OUTBOARD FLAP TRACK 3 RIB 5 LUG FITTING CORROSION. CORRECTIVE ACTION: REPAIRED PER ERA 611826-14. (0390527)Jun 12, 2024 · N334NB · Airbus A319114SDR SWI202408260776Vane · chafedLH INBOARD FLAP VANE LEADING EDGE CENTER VANE CAP CHAFFED (C-CHECK RO 8/24/2024) REMOVED REPAIR ITEM REF CRJ900 SRM 51-42-13-001-001-A01.INSTALLED NEW REPLACEMENT LH INBD FLAP VANE CAP, PN:CC670-14022-1, REF INSTALLATION DWG# CC670-14010, REV -E. AND CRJun 12, 2024 · N187PQ · Cndair CL6002D24SDR ASAA2024061251519Skin · puncturedLESSOR ITEM: RH INBD FLAP LOWER AREA WITH SEVERAL DENTS - EVALUATE / REPAIR AND INCLUDE IN D&B (NOTE ONLY: DB #2) GROUNDED - YES. REMOVED 35 EA FASTENERS TO FOM IAW A320 SRM 57-52-00-300-093 REV. 149. FOUND 66 EA. DENTS WITH PUNCTURES AT 2EA. CLUSTERS REQUIRIJun 12, 2024 · N361VA · Airbus A320214SDR ASAA2024061251517Wedge · dentedLESSOR ITEM: LH INBD FLAP LOWER AREA WITH SEVERAL DENTS - EVALUATE / REPAIR AND INCLUDE IN D&B (NOTE ONLY: DB #3) GROUNDED - YES. PERFORMED A CATEGORY A, PERMANENT REPAIR OF THE LEFT-HAND INBOARD FLAP LOWER AREA DENTS IN 2 AREAS. THE INBOARD REPAIR IS LOCATED Jun 12, 2024 · N361VA · Airbus A320214SDR CALA2024062401881Skin · damagedLEFT INBD FLAP HAS DENTS FROM TIRE BLOWOUT, REMOVED LT INBD TE FLAP & AFT FLAP AS ONE UNIT, IAW AMM 27-51-11-000-801 UP TO AND INCLUDING STEP 8 (E). INSTALLED NEW LT INBD TE FLAP IAW AMM 27-51-11-400-801 FROM STEP G(3) TO STEP H(3F) CONTINUE FROM STEP H (4) Jun 12, 2024 · N68842 · Boeing 737924ERSDR DALA2024061506107Fairing · puncturedAIRCRAFT 1003, #3 RIGHT FLAP FAIRING 632CB HAS PUNCTURE DAMAGE 8 INCHES FROM LOWER RIGHT LEADING EDGE. CORRECTIVE ACTION: PUNCTURE CONTAINED TO OUTER SURFACE & HONEYCOMB, MEASURES 2" LONG AND 1/8" DEEP. NO DAMAGE NOTED ON INNER SURFACE. PERFORMED SECTION I PERJun 12, 2024 · N103DY · Airbus A321211SDR UIEA2024051100388Skin · corrodedLHW I/B T/E MID FLAP UPR SURFACE I/B AFT PNL 577JT AFT EDGE SURFACE CORRODED(<P>PANEL REPAIRED AS PER RI NO: RI-57-53-16875 REV.A. NO FURTHER DEFECTS NOTED.</P>)Jun 12, 2024 · N473MC · Boeing 74745ESDR UIEA2024052900468Skin · delaminatedRHW I/B MID FLAP L/E FAIRING I/B AREA FOUND DELAMINATION(<P>PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5A. NO FURTHER DEFECTS NOTED.</P>)Jun 12, 2024 · N473MC · Boeing 74745ESDR UIEA2024052900469Skin · delaminatedRHW O/B FORE FLAP L/E FAIRING FOUND DELAMINATION(<P>PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5A. NO FURTHER DEFECTS NOTED.</P>)Jun 12, 2024 · N473MC · Boeing 74745ESDR DALA2024061306064Flap Track · corrodedSHIP 3120 CORROSION OUTBD FLAP TRACK #3 INNER & OUTER RIB 5 AT ECCENTRIC BEARING. CORRECTIVE ACTION: REPAIRED PER ERA 614191-1. (0390337)Jun 12, 2024 · N320NB · Airbus A319114SDR SWAA2024062500546Skin · delaminatedREMOVE/INSTALL LH T/E INBD MAIN FLAP (PN: 113A2100-61A; SN: T2242) WEDGE PANEL FOR DELAMINATION DAMAGE<[01] REMOVED AND REPLACED LH T/E INBD MAIN FLAP (PN: 113A2100-61A; SN: T2242) WEDGE PANEL;[02] REMOVED AND REPLACED LH T/E INBD MAIN FLAP OUTBOARD WEDGE PANEJun 11, 2024 · N907WN · Boeing 7377H4SDR IPXA2024070986136Hinge · corrodedRIGHT OTBD FLAP INBD FWD HINGE LWR LUG #4 BORE HAS CORROSION. REMOVE AND REPLACE HINGE BRACKET ASSEMBLY ARC0502-508 PER MD11 AMM 57-53-01/401 (REV 96).Jun 10, 2024 · N257UP · Doug MD11FSDR AALA202407017555Skin · debondedAIRCRAFT IN BASE MAINTENANCE: RIGHT WING OUTBOARD TRAILING FLAP REPAIR DOUBLER DEBONDED BETWEEN FLAP RIBS 11 AND 13. REPAIRED FLAP PER SRM 57-53-00-300-119Jun 10, 2024 · N821AW · Airbus A319132SDR CALA2024061301787Skin · delaminatedL SIDE FLAP DELAMINATING AND NOT FLUSH. APPEARS RIVETS/SCREWS A RE MISSING INSPECTED LEFT WING OUTBOARD FLAP, INBOARD TRAILING EDGE. FOUND PICS ADDED. PICS ADDED TRAILING EDGE DELAMINTION MEASURES 15 " IN LENGTH, LEADING EDGE PIC ADDED SCREWS PULLED THRU AND Jun 10, 2024 · N65832 · Boeing 737924ERSDR DALA2024061206035Skin · debondedAIRCRAFT 1023, FOUND DISBONDING DAMAGE TO THE UPPER AND LOWER COVER SHEETS ON THE LH OUTBOARD FLAP TAB TRAILING EDGE AT HINGE 3C TRAILING EDGE, AND PUNCTURE DAMAGE TO THE TE CLOSURE CAUSED BY THE USE OF A SCREWDRIVER TO REMOVE THE FAIRING. CORRECTIVE ACTION: CJun 10, 2024 · N123DW · Airbus A321211SDR HNAA2024061000490Shroud · unsecureFLAP FAIL WITH FLAPS STUCK AT 8 DEGREES. INSPECTED FLAPS AND FOUND LH IB FLAP SHROUD JAMMED INTO LH IB FLAP LEADING EDGE. REMOVED LH IB FLAP IAW AMM27-50-00-000-801-A. REPLACED AND INSTALLED LH IB FLAP IAW AMM27-50-00-400-801-AJun 9, 2024 · N939AE · Emb EMB145LRSDR UIEA2024060500483Skin · crackedLEFT WING INBOARD MAIN FLAP LEADING EDGE BROKEN(<P>CRACK ON LH WING INBD MAIN FLAP LEADING EDGE AT IFS 296.25 / 282.75 WAS REPAIRED PER SRM 57-53-01-2R-1. NO FURTHER DEFECTS NOTED.</P>)Jun 8, 2024 · N1499A · Boeing 767328SDR UIEA2024060500492Collar · corrodedRIGHT WING INBD FLAP COLLAR FITTING WITH EVIDENCE OF CORROSION.(<P>COLLAR FITTING WAS REPLACED PER AMM TASK 27-51-41-400-801. NO FURTHER DEFECTS NOTED.</P>)Jun 8, 2024 · N1499A · Boeing 767328SDR AALA202406111839Trunnion · wornAIRCRAFT WAS GROUNDED: LEFT WING INBOARD TRAILING EDGE FLAP INBOARD DRIVE STRUT TRUNNION FORWARD AND AFT SIDES WORN BEYOND LIMITS. REPLACED TRUNNION PER CMM 57-52-23 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.Jun 8, 2024 · N170US · Airbus A321211SDR SWAA2024060798942Skin · delaminatedLH T/E INBD MAIN FLAP WEDGE PANEL DELAMINATION DAMAGE REF EA 21-157-01555. REMOVED AND REPLACED LH T/E INBD MAIN FLAP OUTBOARD WEDGE PANEL IAW SRM 51-40-02-0G-0 AND DWG 113A2100 REV A.Jun 7, 2024 · N907WN · Boeing 7377H4SDR WX0A2024070132101Skin · damaged(AIRCRAFT NOT GROUNDED) NRC 6000-0013: RH OUTBRD FLAP, DAMAGE FOUND ON UPPER SURFACE / RH OUTBRD FLAP, UPPER SURFACE T/E WEDGE PANEL REPAIRED AS PER AIRBUS DOSSIER REFERENCE #81416455 AND COMPLY AS PER SRM TASK 57-53-00-300-121 ZONE 2. PARA. 2.A. REV. 149. THJun 6, 2024 · N329NV · Airbus A319111SDR SWAA2024060798912Skin · delaminatedLEFT I/B MAIN FLAP DELAMINATED AT OB WEDGE PANEL. REMOVED LH IB MAIN FLAP OB WEDGE PANEL IAW CMM 57-53-05. RE-INSTALLED LT MAIN FLAP OUTBOARD WEDGE PANEL PER CMM 57-53-05 AND COMPLIED WITH TEMPORARY REPAIR OF DELAMINATED DAMAGE PER EA 21-157-01555 (REF TTG8QJun 6, 2024 · N907WN · Boeing 7377H4SDR SWAA2024060698913Skin · delaminatedLH OB TE FLAP DELAMINATED. ] R/R L/H O/B AFT FLAP PER AMM 21-51-22 STEPS F -F5G. REQUIRES OPS AND RIG CHECK PER SAME;[02] R/R L/H O/B AFT FLAP PER AMM 21-51-22 STEPS F -F5G.; COMPLETED OP`S AND RIG CHECKS PER AMM 27-51-22. NO DEFECTS NOTED.Jun 6, 2024 · N907WN · Boeing 7377H4SDR SWAA2024071898546Skin · debondedCUSTOMER REQUEST - DISBONDED OB AFT FLAP EXTERNAL SKIN LOWER INBOARD CORNER AT LT WING 2024-376371<[01] TOOL USED CALIPER PN: 500-197-30; SN: B20189521; DUE DATE: 26/JAN/25.;[02] TOOL USED HOT BONDER P/N: HCS9200B-AV S/N: 18175478 DUE DATE: 25 JAN 25.;[03] TOOJun 5, 2024 · N7876A · Boeing 7377Q8SDR SWAA2024060698471Skin · delaminatedR&R LH OB AFT FLAP FOR UPPER SKIN DEMALMINATION 24-127-01494-TLD (COMPONENT - SWA - REPAIR - L/H O/B T/E AFT FLAP (PN: 113A3700-27 SN: 005725) UPPER SKIN DELAMINATION - PERMANENT) [TTG8Q00TQ8SF]<[01] R & R O/B AFTFLAP PER AMM 27-51-22Jun 5, 2024 · N8678E · Boeing 7378H4SDR ASAA2024060451446Skin · delaminatedRH WING INBD FLAP LOWER SURFACE CLUSTER 1 REQUIRES REPAIR OF DENTS. GROUNDED - YES. ACCOMPLISHED PERMANENT CLASS A REPAIR OF R/W INBRD FLAP T.E. WEDGE LOWER SURFACE P/N D2525033150300 S/N NSN ON A320-214 S/N 4894, WV 015, FH 35490:29, FC 11792. REPAIR IS LOCATJun 4, 2024 · N846VA · Airbus A320214SDR DALA2024060405779Bearing · corrodedSHIP 3140 CORROSION ON SPHERICAL BEARING FLAP TRACK 3 OF THE FLAP OUTBOARD RH. CORRECTIVE ACTION: REPLACED SPHERICAL BEARING OF FLAP TRACK 3 OUTBOARD R/H AS PER A320 FAM AMM 57-53-21-000-001-A AND AMM 57-53-21-400-001-A. (0374650)Jun 3, 2024 · N340NB · Airbus A319114SDR SWI202408210696Skin · dentedTRANSFER FROM EAML 1352978 : CREATED FROM FORWARD DISCREPANCY. PLEASE REFERENCE AML 1352408 FOUND 23 DENTS ON ON LH OTBD FLAP UPPER SKIN. (FLIGHT 5057 - FILED CLOSED)REMOVED AND REPLACED LH OUTB FLAP ASSEMBLY IN REFERENCE WITH AMM 27-54-05. COMPLIED WITH TASK Jun 2, 2024 · N980SW · Cndair CL6002B19SDR SWIA2024082100602Skin · dentedTRANSFER FROM EAML 1352982 : CREATED FROM FORWARD DISCREPANCY. PLEASE REFERENCE AML 1352408 FOUND 74 DENTS ON RH INBD FLAP UPPER SKIN. (FLIGHT 5057 - FILED CLOSED)REMOVED AND REPLACED RH INBD FLAP ASSEMBLY IN REFERENCE WITH AMM 27-54-01. COMPLIED WITH TASK CAJun 2, 2024 · N980SW · Cndair CL6002B19SDR SWI2024082100696Skin · dentedTRANSFER FROM EAML 1352978 : CREATED FROM FORWARD DISCREPANCY. PLEASE REFERENCE AML 1352408 FOUND 23 DENTS ON ON LH OTBD FLAP UPPER SKIN. (FLIGHT 5057 - FILED CLOSED)REMOVED AND REPLACED LH OUTB FLAP ASSEMBLY IN REFERENCE WITH AMM 27-54-05. COMPLIED WITH TASK Jun 2, 2024 · N980SW · Cndair CL6002B19SDR FDEA202406010758Support · damagedL/H WING, AFT FAIRING SUPPORT INBD MAIN FLAP FITTING IS LOOSE. FOUND AFT MOUNT HOLE DAMAGED IN LH I/B LWR MAIN FLAP FOR FAIRING SUPPORT BRACKET. REPAIRED DAMAGED HOLE AND REPLACED BRACKET REF. B757 SRM 57-53-02-2R REPAIR 3. AND INSTALLED FAIRING TO BRACKET RJun 1, 2024 · N919FD · Boeing 75723ASDR SWAA2024071194424Fairing · crackedFOUND CRACK ON THE FWD LWR END OF THE #6 FLAP SUPPORT AFT FAIRING (642BB)<[01] REPAIRED CRACK DAMAGE ON FWD LWR END OF THE #6 FLAP SUPPORT FAIRING 642BB PER EA 24-157-01559.;[02] VERIFIED CORRECTIVE ACTION ITEMS; CARD COMPLETE.;[03] UPDATED MEASUREMENTS TABLE;May 31, 2024 · N7737E · Boeing 7377BDSDR DALA2024062106325Strut · corrodedSHIP 3132 CORROSION INTERCONNECTING STRUT INTERNAL AREA ON LH WING. CORRECTIVE ACTION: REPLACED INTERCONNECTING STRUT ON LH WING ASPER A320 FAM AMM 27- 51-44-000-001-A AND ASPER A320 FAM AMM 27-51-44-400-001-A. (0370064)May 31, 2024 · N332NB · Airbus A319114SDR CALA2024060301674Skin · damagedDAMAGE APPROX 25X 12 IN METALLIC PART MEETS PROX OF DAMAGE & MATERIAL 15 SQUARE TO 150 SQUARE IN. FOUND SKIN PEELED AWAY AT TRAILING EDGE OUTBOARD AFT FLAP, UNDER INBOARD SIDE , LT WING. REMOVED OUTBOARD AFT FLAP IAW AMM TASK 27-51-22-000-801. INSTALLEMay 31, 2024 · N37422 · Boeing 737924ERSDR DALA2024060305743Plate · corrodedSHIP 3132 CORROSION WAS FOUND AFFECTING THE IB AND OB AL PLATES (FACES AND BORES) AT TRACK #3 LEVEL. CORRECTIVE ACTION: REPAIRED PER ER/A 14-618088. (0369854)May 31, 2024 · N332NB · Airbus A319114SDR IPXA2024062627236Attach Angle · crackedAGING FINDING - (AA023) RIGHT WING OUTBOARD FLAP INBOARD FLAP CARRIAGE HAS A CRACKED ATTACH ANGLE AT THE FORWARD SIDE. DRILLED AND INSTALLED CLIP ANGLE ON RIGHT WING OUTBOARD FLAP INBOARD FLAP CARRIAGE IAW MD-11 SRM 51-31-01-0G-0. REVIEWED.May 30, 2024 · N292UP · Doug MD11FSDR SWAA2024061891700Skin · delaminatedLEFT WING O/B MAIN FLAP AFT FLAP; I/B LOWER SKIN SECTION DELAMINATED DOT 223-LWAF11.<[01] REMOVED AND INSTALLED NEW LEFT WING O/B AFT FLAP. AS PER AMM 27-51-22-000-801 AND AMM 27-51-22-400-801.;[02] RII:<BR>VERIFIED STEP 1<BR>AUDITED PER MPM 52.02.02May 30, 2024 · N8692F · Boeing 7378H4SDR SWAA2024061891706Skin · delaminatedRIGHT WING O/B MAIN FLAP AFT FLAP; I/B LOWER SKIN SECTION DELAMINATED DOT 223-LWAF18.<[01] REMOVED AND INSTALLED NEW RIGHT WING O/B AFT FLAP. AS PER AMM AMM 27-51-22-000-801 AND AMM 27-51-22-400-801.;[02] RII:<BR>VERIFIED STEP 1<BR>AUDITED CW PER MPM 52.02.02May 30, 2024 · N8692F · Boeing 7378H4SDR SWAA2024060391488Fairing · delaminated#6 CANOE FAIRING AFT CONE LOWER SECTION DELAMINATED<[01] 05 - OK TO CONTINUE PER [CDL 57-10-4 XB;RIGHT - FLAP TRACK FAIRING TAIL CONES- INBOARD FLAPS]. WITH SP 1. INSTALLED NEW AFT FAIRING TAILCONE IAW AMM 27-51-18 THIS CLEARED CDL;[03] REPLACED #6 AFT FLAP FMay 30, 2024 · N914WN · Boeing 7377H4SDR DALA2024053105693Roller · excess playSHIP 3137 EXCESSIVE PLAY CRUISE ROLLER OB FLAP ON RH WING. CORRECTIVE ACTION: REPLACED CRUISE ROLLER OB FLAP ON RH WING AS PER AIRBUS CMM. 57- 53-21 TASK 57-53- 21-000-810-A01 AND TASK 57-53-21-400-810-A01. (0368209)May 30, 2024 · N337NB · Airbus A319114SDR VNAA202407100007Skin · nickedINITIAL ISPECTION:SEVERAL NICKS ON INBD FLAP FLS 15.00 TO FLS 75.60 AT LH WINGSEVERAL NICKS ON INBO FLAP FLS 15.00 TO FLS 75.60 AT LH WING WERE BLENOEO OUT PER CRJ900 SRM 51-12-00-001-001-A01 ANO WERE EVALUATEO BTW FLS15 TO FLS45 OUT OF LIMITS ANO BTW FLS45 TOMay 29, 2024 · N584NN · Cndair CL6002D24SDR SWAA2024062691159Skin · delaminatedL/WING O/B AFT FLAP I/B LOWER T/EDGE SKIN AREA DELAMINATED FOUND OUT-LIMIT<[01] REMOVED & INSTALLED LEFT WING O/B AFT FLAP AS PER AMM 27-51-22-400-801. ACCOMPLISHED ADJUSTMENT FOUND TO BE WITHIN LIMITS. <BR>DIGITAL CALIPER USED BC 175307 DUE DATE 05-DEC-24<BR>May 29, 2024 · N464WN · Boeing 7377H4SDR DALA2024053005664Roller · excess playSHIP 3137 EXCESSIVE PLAY CRUISE ROLLER IB FLAP ON LH WING. CORRECTIVE ACTION: REPLACED CRUISE ROLLER IB FLAP ON LH WING AS PER AIRBUS CMM 57- 52-21 TASK 57-52-21-000-805-A01 AND TASK 57-52-21-400-803-A01. (0366852)May 29, 2024 · N337NB · Airbus A319114SDR DALA2024053005663Roller · excess playSHIP 3137 EXCESSIVE PLAY CRUISE ROLLER IB FLAP ON RH WING. CORRECTIVE ACTION: REPLACED CRUISE ROLLER IB FLAP ON RH WING AS PER AIRBUS CMM 57- 52-21 TASK 57-52-21-000-805-A01 AND TASK 57-52-21-400-802-A01. (0366813)May 29, 2024 · N337NB · Airbus A319114SDR DALA2024053005662Roller · excess playSHIP 3137 EXCESSIVE PLAY CRUISE ROLLER OB FLAP ON LH WING. CORRECTIVE ACTION: REPLACED CRUISE ROLLER OB FLAP ON LH WING AS PER AIRBUS CMM. 57- 53-21 TASK 57-53- 21-000-810-A01 AND TASK 57-53-21-400-810-A01. (0366860)May 29, 2024 · N337NB · Airbus A319114SDR IXXA2024052901Skin · dentedRIGHT INBOARD AFT FLAP 2 SHARP DENTS ON UPPER SURFACEMay 29, 2024 · N307AZ · Boeing 767338SDR FDEA202405280879Skin · cracked3EA CRACKS (5MM&8MM&12MM) WERE FOUND AT L/H WING CENTER FLAP RIB26 OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE FLANGE REPAIR AT RIB26 S-2.6~R/S AND DOUBLER REPAIR AT RIB26~27 S- 2.3~R/S LH CENTER FLAP I.A.W FEDEX EA NO:T6-5750-T0379330 P1, SEQ NO:1249, TITLMay 28, 2024 · N729FD · Airbus A300B4622R
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