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 AALA202405071224Bracket · wornAIRCRAFT IN BASE MAINTENANCE: LEFT WING INBOARD TRAILING EDGE FLAP INTERCONNECTING STRUT ATTACH FITTING / BRACKET WORN AND BEARING HAS EXCESSIVE PLAY. REPLACED NTERCONNECTING STRUT ATTACH FITTING / BRACKET PER SRM 51-42-11.Apr 18, 2024 · N738US · Airbus A319112SDR AALA202404302126Skin · delaminatedAIRCRAFT IN BASE MAINTENANCE: RIGHT WING OUTBOARD FLAP LOWER SURFACE IS DELAMINATED. REPLACED RIGHT WING OUTBOARD AFT FLAP PER AMM 27-51-22.Apr 18, 2024 · N964NN · Boeing 737823SDR AALA202404308860Skin · delaminatedAIRCRAFT IN BASE MAINTENANCE: RIGHT WING OUTBOARD FLAP LOWER SURFACE IS DELAMINATED. REPLACED RIGHT WING OUTBOARD AFT FLAP PER AMM 27-61-22.Apr 18, 2024 · N991NN · Boeing 737823SDR SWIA20240712417Hinge · nickedLH FLAP HINGE BOX AT WS 54.55 AFT O/B HINGE, I/B LUG HAS NICKS. (C-CHECK RO 7/12/2024) PERFORMED REPAIR AT L/H FLAP HINGE BOX AT WS 54.55 AFT O/B HINGE I/B LUG IAW CRJ 700 SRM 51-12-00 AVIATION GROUP E-MAIL TICKET # 23677,SRM 51-24-11,REO 670-57-21-973 Apr 17, 2024 · N762SK · Cndair CL6002C10SDR SWAA2024042676051Skin · delaminatedRIGHT WING OTBD AFT FLAP INBD EDGE LOWER SIDE DELAMINATED.<[01] 02 - INSPECTED PER [AMM 27-51-22-400-801-NG (OUTBOARD AFT FLAP INSTALLATION - PERMANENT)]Apr 17, 2024 · N8629A · Boeing 7378H4SDR YENA2024041800643Skin · dentedDURING HEAVY MAINTENANCE: DENTS ON OB FLAP LOWER SURFACE ON LH WING; REPAIRED OB FLAP TAB LOWER SURFACE ON LH WING AS PER EC NO. A24-467-01 AEROMAN EA 57-0092-24 COVER AND PART 1-2 AND AIRBUS RDAF 81376877/003/2024 ISSUE A. MAJOR REPAIR CATEGORY A WORK ACCOMPLApr 17, 2024 · N950JT · Airbus A321231SDR SWAA2024050275363Skin · delaminatedR/H O/B AFT FLAP UPPER AND LOWER SKINS ARE DELAMINATED @ T/E I/B CORNER/<[01] REMOVED AND REPLACED R/H O/B AFT FLAP IAW AMM 27-51-22-400-801. WORK CARD COMPLETEApr 16, 2024 · N8684F · Boeing 7378H4SDR SWAA2024050275364Skin · delaminatedL/H O/B AFT FLAP UPPER SKIN IS DELAMINATED AT AFT I/B CORNER. (MARKED)<[01] REMOVED AND REPLACED L/H O/B AFT FLAP IAW AMM 27-51-22-400-801. WORK CARD COMPLETEApr 16, 2024 · N8684F · Boeing 7378H4SDR DALA2024041804527Vane · debondedSEVEN DISBONDS WERE FOUND ON LH AFT MOVABLE VANE LOWER SKIN, 1) LENGTH 1.550IN AND WIDTH 1.125IN, 2) LENGTH 1.000IN AND WIDTH 0.850IN, 3) LENGTH 1.250IN AND WIDTH 0.850IN, 4) LENGTH 1.250IN AND WIDTH 1.250IN, 5) LENGTH 1.250IN AND WIDTH 1.250IN, 6) LENGTH 1.37Apr 16, 2024 · N996AT · Boeing 717200SDR AALA202404224178Skin · delaminatedAIRCRAFT WAS GROUNDED: DURING PHASE 1 INSPECTION FOUND RIGHT HAND OUTBOARD AFT FLAP TRAILING EDGE TO HAVE DISBONDED SKIN APPROXIMATELY 57 IN ACROSS BY 10 IN HIGH. **SUPPLEMENTAL REPORT FOR AALA202404164178: REPLACED RIGHT HAND OUTBOARD AFT FLAP PER AMM 27-51-Apr 15, 2024 · N913NN · Boeing 737823SDR DALA2024041804526Guide Vane · damagedDAMAGE T DURING TEST OF FLIGHT SPOILER ACTUATOR. FLAPS WAS RETRACTED AND RH FLAP GUIDE VANE WAS DENTED WITH INDB FLAP INGE SUPPORT BRACKET (HINGE FAIRING REMOVAL). SUMMARY OF NRC 00077: RH FLAP GUIDE VANE WAS REPAIRED PER PRI 616775-14 REV 2 AND ER/A 616775-14Apr 15, 2024 · N996AT · Boeing 717200SDR AALA202404164178Skin · debondedAIRCRAFT WAS GROUNDED: DURING PHASE 1 INSPECTION FOUND RIGHT HAND OUTBOARD AFT FLAP TRAILING EDGE TO HAVE DISBONDED SKIN APPROXIMATELY 57 IN ACROSS BY 10 IN HIGH. **SUPPLEMENTAL REPORT WILL BE SUBMITTED**(OPEN).Apr 15, 2024 · N913NN · Boeing 737823SDR AALA202404268524Skin · debondedAIRCRAFT IN BASE MAINTENANCE: RIGHT WING OUTBOARD TRAILING EDGE FLAP EXISTING REPAIR PLATE DEBONDED. DEBONDED BETWEEN RIB 7 AND RIB 8. REPAIRED FLAP PER SRM 57-53-00-300-121.Apr 13, 2024 · N756US · Airbus A319112SDR FDEA202404130462Skin · dentedDENT ON LOWER SKIN OF INBOARD TRAILING EDGE MAIN FLAP AT LH WING. LH WING INB. T/E MAIN FLAP LOWER SKIN WAS REPAIRED I.A.W. B767 SRM 57-53-01-2R REPAIR 1 FIG. 201 SHEET 2 NOTE A AND B767 SRM 51-70-03-0G PARAGRAPH 5.L. FIG. 16 REV. 88.Apr 13, 2024 · N162FE · Boeing 7673S2FSDR FDEA202404130461Skin · dentedDENT ON LOWER SKIN OF INBOARD TRAILING EDGE AFT FLAP AT LH WING. LH WING, LOWER SKIN OF INBOARD TRAILING EDGE AFT FLAP WAS REPAIRED I.A.W. B767 SRM 57- 53-01-2R REP. 1 AND SRM 51-70-03-0G PAR. 5.L. FIG. 16 PAG. 27-52 REV. 88.Apr 13, 2024 · N162FE · Boeing 7673S2FSDR FDEA202404130460Skin · dentedSEVERAL DENTS, LOWER SURFACE, INBOARD TRAILING EDGE FLAP, RH WING. RH WING INB. T/E AFT FLAP LOWER SURFACE WAS EVALUATED AND FOUND 3 DENTS WITHIN LIMITS I.A.W. B767 SRM 57-53-01-1A FIG. 101 SHEET 4 NOTE C DET. IV. ONE DENT WAS FOUND OUT OF LIMITS AND WAS RApr 13, 2024 · N162FE · Boeing 7673S2FSDR UIEA2024041300273Skin · damagedLHW T/E I/B MID FLAP L/E FOUND BIRD STRIKE(<P>LHW T/E I/B MID FLAP L/E BIRD STRIKE AREA, PERFORMED TIME LIMIT REPAIR AS PER EA-1957A0103 REV 0. NO FURTHER DEFECTS NOTED.</P>)Apr 13, 2024 · N451PA · Boeing 74746NFSDR YENA2024041600581Skin · dentedDURING HEAVY MAINTENANCE: WINGS / LH WING / INBD FLAP / LOWER SKIN / DENTS / PERMANENT REPAIR. (CONSIDERED A MAJOR REPAIR)Apr 11, 2024 · N249JB · Emb ERJ190100IGWSDR YENA2024041600567Skin · debondedDURING HEAVY MAINTENANCE: WINGS-RH/ OB FLAP/ LOWER SURFACE RIB 10/ DEBONDING- PERMANENT REPAIR. (CONSIDERED A MAJOR REPAIR)Apr 11, 2024 · N249JB · Emb ERJ190100IGWSDR DALA2024041204335Flap Track · brokenSHIP 3139 BROKEN FLAP TRACK FAIRING 631CB BONDING PLATE ON RH WING. CORRECTIVE ACTION: REPAIRED PER ER/A 616309-14. (0288691)Apr 11, 2024 · N339NB · Airbus A319114SDR FDEA202404110454Skin · damagedRH WING OB FLAP LWR SURFACE 2 IN AWAY TO AFT EDGE,4 IN AWAY TO OB FOUND A REPAIR IN POOR CONDITION. RE-REPAIRED RH WING OB FLAP LWR SURFACE AT OTEF STA514 EXISTING REPAIR AS PER B777 SRM 57-53-01-2R REPAIR 2 ,SRM 51-70-04-2R REPAIR 1,SRM 51-70-04-2R REPAIRApr 11, 2024 · N895FD · Boeing 777FS2SDR SWAA2024043073057Fairing · crackedRIGHT WING FORWAR4D FAIRING FLAP#642AB FOUND CRACK O/B LOWER SURFACE<[01] APPLIED TOPCOAT AT RIGHT WING FORWARD FAIIRING FLAP #642AB O/B LOWER SUEFACE REF B 737 AMM 51-21-73-370-802;[02] APPLIED PERMANENT REPAIR AT FAIRING #642AB PER B737 SRM 51-70-042R-0 PARAApr 10, 2024 · N8701Q · Boeing 7378SDR SWAA2024043072965Skin · delaminatedL/H O/B AFT FLAP DELAMINATED LOWER I/B CORNER LOWER SURFACE<[01] REMOVED L/H O/B AFT FLAP IAW AMM 27-51-22;[02] OK TO INSTALL;[03] INSTALLED L/H OB AFT FLAP PER AMM 27-51-22 THROUGH STEP 3.(5)(G).;[04] C/W RII INSPECTION OF OUTBD FLAP INSTALL;[05] REMOVED AND Apr 9, 2024 · N8685B · Boeing 7378H4SDR UIEA2024040200233Skin · delaminatedLHW O/B FORE FLAP FOUND DELAMINATED(<P>PERFORMED REPAIR AT DELAMINATION AREA AS PER SRM 51-70-17 PAR 5.A.(1). NO FURTHER DEFECTS NOTED</P>)Apr 9, 2024 · N496MC · Boeing 74747UFSDR DALA2024040804186Hinge Fitting · wornCORROSION AND WEAR IN THE HINGE BOLT BORE OF THE OUTBOARD FLAP IDLER HINGE ON THE RH WING. ER/A 541841-14 ISSUED FOR REPAIR. THIS IS THE LOG PAGE THAT TRACKS THE DTA REQUIREMENTS FOR ER/A 541841-14. DTA MUST BE ACCOMPLISHED WITHIN 24 MONTHS. ENGINEERING PURPOSApr 8, 2024 · N965AT · Boeing 717200SDR DALA2024040804185Hinge Fitting · wornCORROSION AND WEAR IN THE HINGE BOLT BORE OF THE OUTBOARD FLAP IDLER HINGE ON THE RH WING. ER/A 541845-14 ISSUED FOR REPAIR. THIS IS THE LOG PAGE THAT TRACKS THE DTA REQUIREMENTS FOR ER/A 541845-14. DTA MUST BE ACCOMPLISHED WITHIN 24 MONTHS. ENGINEERING PURPOSApr 8, 2024 · N965AT · Boeing 717200SDR DALA2024040804168Track · corrodedSHIP 3139 CORROSION SUPPORT-SELF-ALIGNING TRACK 4 O/B FLAP ON L/H WING. CORRECTIVE ACTION: REPAIRED PER ER/A # 616667-14. (0282412)Apr 8, 2024 · N339NB · Airbus A319114SDR SWIA2024061900407Skin · dentedLH INBD FLAP LOWER SKIN HAS A CLUSTER OF SMALL DENTS ON INBD SIDE (C-CHECK RO 6/17/2024) L/H I/B FLAP LOWER SKIN HAS BEEN REPAIRED REF CRJ 700 SRM 57-52-01-201-005-A01. SEE CONTINUATION SHEET FOR DETAILS. COMPLIED FULLY W/SKYCARD 51-900-1002-SKY.Apr 7, 2024 · N722EV · Cndair CL6002C10SDR SWAA2024041071578Fairing · crackedLEFT WING #1 FWD FLAP SUPPORT FAIRING INBOARD SIDE HAS A 2.6' LONG CRACK; 12' FROM FWD EDGE AND 4' FROM TOP SURFACE<[01] CRACK ON LEFT WING FWD FAIRING MEASURES 2.6' LONG AND LESS THAN ONE PLY DEEP;LOOKING TO USE SRM 57-53-70-1A-1 TO APPLY A SPEED TAPE TEMP SEApr 7, 2024 · N8859Q · Boeing 7378SDR SWAA2024041071701Flap · off trackON WALK AROUND FOUND LEFT OTBD AFT FLAP OFF TRACK<[01] REMOVED AND REPLACED L/H OUTBOARD TRAILING EDGE AFT FLAP REF MM 27-51-22;[02] C/W;[03] REMOVED AND REPLACED L/H OUTBOARD TRAILING EDGE AFT FLAP REF MM 27-51-22Apr 7, 2024 · N8617E · Boeing 7378H4SDR DALA2024040804169Bearing · corrodedSHIP 3139 CORROSION ON SUPPORT BEARING ON FLAP TRACK 2 OF THE INBOARD FLAP ON LH WING. CORRECTIVE ACTION: REPAIRED PER ER/A # 616560-14. (0282393)Apr 7, 2024 · N339NB · Airbus A319114SDR IPXA2024061071382Rib · crackedONE CRACK FOUND ON RIB FLANGE 17 RIGHT WING FLAP. ACCOMPLISH PERMANENT REPAIR PER EO-90101-REQ1 AND EA 300-5750-27-A3570 REV -.Apr 6, 2024 · N160UP · Airbus A300F4622RSDR IPXA2024050271382Rib · cracked**SDR FILED OPEN** FAULT: 1 CRACK FOUND ON RIB FLANGE 17A RIGHT WING FLAP. VERIFIED STEP # 31 COMPLETED .Apr 6, 2024 · N160UP · Airbus A300F4622RSDR IPXA2024050271374Rib · crackedTWO CRACKS FOUND ON RIB FLANGE 18 RIGHT WING FLAP. ACCOMPLISH PERMANENT REPAIR PER EO-90101-REQ1 AND EA 300-5750-27-A3570 REV -.Apr 6, 2024 · N160UP · Airbus A300F4622RSDR IPXA2024050271247Rib · crackedTWO CRACKS FOUND ON RIB FLANGE 27 RIGHT WING FLAP. ACCOMPLISH PERMANENT REPAIR PER EO-90101-REQ1 AND EA 300-5750-27-A3570 REV -.Apr 6, 2024 · N160UP · Airbus A300F4622RSDR IPXA2024050271299Rib · crackedTWO CRACKS FOUND ON RIB FLANGE 25 RIGHT WING FLAP. ACCOMPLISH PERMANENT REPAIR PER EO-90101-REQ1 AND EA 300-5750-27-A3570 REV -.Apr 6, 2024 · N160UP · Airbus A300F4622RSDR IPXA2024050271412Rib · crackedTWO CRACKS FOUND ON RIB FLANGE 11 RIGHT WING FLAP. COMPLIED WITH UPS EO-90101 AND VTMAE FINAL EA 300-5750-27-A3570 REV-.Apr 6, 2024 · N160UP · Airbus A300F4622RSDR IPXA2024050271410Rib · crackedONE CRACK FOUND ON RIB FLANGE 12 RT WING FLAP. COMPLIED WITH UPS EO-90101 AND VTMAE FINAL EA 300-5750-27-A3570 REV-.Apr 6, 2024 · N160UP · Airbus A300F4622RSDR IPXA2024050271406Rib · crackedTWO CRACKS FOUND ON RIB FLANGE 13 RT WING FLAP. ACCOMPLISH PERMANENT REPAIR PER EO-90101-REQ1 AND EA 300-5750-27-A3570 REV -.Apr 6, 2024 · N160UP · Airbus A300F4622RSDR IPXA2024050271311Rib · crackedCRACK FOUND ON RIB FLANGE 19 RIGHT WING FLAP. ACCOMPLISH PERMANENT REPAIR PER EO-90101-REQ1 AND EA 300-5750-27-A3570 REV -.Apr 6, 2024 · N160UP · Airbus A300F4622RSDR IPXA2024050271279Rib · crackedONE CRACK FOUND ON RIB FLANGE 26 RIGHT WING FLAP. ACCOMPLISH PERMANENT REPAIR PER EO-90101-REQ1 AND EA 300-5750-27-A3570 REV -.Apr 6, 2024 · N160UP · Airbus A300F4622RSDR IPXA2024050271249Rib · crackedTWO CRACKS FOUND ON RIB FLANGE 26 RIGHT WING FLAP. ACCOMPLISH PERMANENT REPAIR PER EO-90101-REQ1 AND EA 300-5750-27-A3570 REV-.Apr 6, 2024 · N160UP · Airbus A300F4622RSDR IPXA2024050271400Rib · crackedONE CRACK FOUND ON RIB FLANGE 15 RIGHT WING FLAP. ACCOMPLISH PERMANENT REPAIR PER EO-90101-REQ1 AND EA 300-5750-27-A3570 REV -.Apr 6, 2024 · N160UP · Airbus A300F4622RSDR IPXA2024041371234Skin · crackedCRACK FOUND RIB FLANGE 27A LEFT FLAP TOP SKIN. ACCOMPLISH PERMANENT REPAIR PER EO-90102-REQ1 AND EA 300-5750-27-A3568 REV -.Apr 6, 2024 · N160UP · Airbus A300F4622RSDR SWIA20240712405Skin · chafedLH IB FLAP VANE SKIN HAS CHAFE DAMAGE AT APROX WS80.00 (C-CHECK RO 7/12/2024) REMOVED AND REPLACE NEW CAP VANE P/N CC670-14022-1 AT LH IB FLAP VANE SKIN APROX. WS80.00 IAW CRJ 200 SRM 51-42-10 AND SRM 51-42-13,SRM 57-52-01,SRM 51-25-06, SRM 51-21-11, SRApr 5, 2024 · N762SK · Cndair CL6002C10SDR FDEA202404050649Skin · cracked2EA CRACKS (MAX:20MM) WERE FOUND AT LH WING CENTER FLAP RIB25 AFT AREA OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE FLANGES REPAIR AT RIB25 UPPER FLANGE S-2.7~REAR SPAR AND EXTERNAL DOUBLERS REPAIR AT RIB26~25 S-2.2~REAR SPAR PLUS 10 INCHES, THE REPAIR CLApr 5, 2024 · N661FE · Airbus A300F4605RSDR FDEA202404050648Skin · cracked1EA CRACK (75MM) WAS FOUND AT LH WING CENTER FLAP RIB20 AFT AREA OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE FLANGE REPAIR AT RIB 20 BETWEEN UPPER SKIN S-2.8 TO REAR SPAR AND EXTERNAL DOUBLER REPAIR ENCLOSED BY LOWER SKIN RIB 19 TO RIB 20 AND S-2.1 TO REARApr 5, 2024 · N661FE · Airbus A300F4605RSDR FDEA202404050646Skin · cracked1EA CRACK (25MM) WAS FOUND AT LH WING CENTER FLAP RIB13 AFT AREA OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE FLANGE REPAIR AT RIB 13 UPPER FLANGE S-2.7~S-2.8, THE REPAIR CLASSIFIED AS CAT.A MAJOR PER GMM 6-2-100 I.A.W FEDEX EA NO:T6-5750-T0378801 P1, SEQ Apr 5, 2024 · N661FE · Airbus A300F4605RSDR FDEA202404050638Skin · cracked3EA CRACKS (MAX70MM) WERE FOUND AT LH WING FLAP OF CENTER RIB12 AFT AREA OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE FLANGES REPAIR AT RIB12 UPPER FLANGE S-2.7~REAR SPAR, THE REPAIR CLASSIFIED AS CAT.A MAJOR PER GMM 6-2-100 I.A.W FEDEX EA NO:T6-5750-T03788Apr 5, 2024 · N661FE · Airbus A300F4605RSDR FDEA202404050637Skin · cracked4EA CRACKS (MAX50MM) WERE FOUND AT LH WING CENTER FLAP RIB11 AFT AREA OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE FLANGE REPAIR AT RIB 11 UPPER FLANGE S-2.7~REAR SPAR AND EXTERNAL DOUBLER REPAIR AT RIB11~RIB13 S-2.2~REAR SPAR, THE REPAIR CLASSIFIED AS CAT.Apr 5, 2024 · N661FE · Airbus A300F4605R
Back to JASC 5753