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 SWAA2023082992070Panel · elongatedR/W T/E PANEL 651GB 5EA I/B HOLES ARE ELONGATED. (MARKED)<[01] R/W T/E PANEL 651GB I/B AREA WITH 5 ELONGATED HOLES WERE REPAIRED IAW SRM 51-70-04-2R-9.;[02] VERIFIED JOB COMPLETE AND MEASUREMENT TABLE.Aug 21, 2023 · N420WN · Boeing 7377H4SDR IPXA2025022659129Structure · damagedLH INBRD MID FLAP BIRD STRIKE **FLAP R&R** INSTALLED REMOVED CARRIAGE ONTO NEW MID FLAP, TORQUED AND SAFETY APPLIED IAW AMM 27-51-23. INSTALLED RIGHT INBOARD FLAP ASSAY PER MM 27-51-01-404-030 UP TO STEP H(10). VERIFIED OPERATION CHECK OF FLIGHT CONTROLS (FLAPAug 20, 2023 · N575UP · Boeing 74744AFSDR FDEA202308191463Bracket · corrodedRIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG HOLE BORE FOUND CORROSION. RIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG HOLE BORE (F AND G HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-03. OVERSIZAug 19, 2023 · N631FE · Doug MD11FSDR FDEA202308191462Bracket · corrodedRIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT LUG HOLE BORE FOUND CORROSION. RIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT LUG HOLE BORE (A AND B HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-03. OVEAug 19, 2023 · N631FE · Doug MD11FSDR FDEA202308191461Bracket · corrodedLEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT LUG HOLE BORE FOUND CORROSION. LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT LUG HOLE BORE (A AND B HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-03. OVERSAug 19, 2023 · N631FE · Doug MD11FSDR FDEA202308191460Bracket · corrodedLEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG HOLE SURFACE FOUND CORROSION. LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG HOLE SURFACE (J LUG) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-03. REPAIR EVAug 19, 2023 · N631FE · Doug MD11FSDR CALA2023082102605Skin · delaminatedPDA 1 RH OUTBD TE FLAP TOP SKIN DELAM 23" X 8.25" LOG PAGE HAS BEEN LOCKED FOR MX FERRY. UNLOCKING FOR MX PHOTOS ATTACHED VERIFIED THRU THE IPC THAT P/N 113A3700-24 IS EFF FOR THIS A/C. INSP ALL ATTACHMENT POINTS & HARDWARE WITH NO DEFECTS NOTED. OK TO INSTALLAug 19, 2023 · N38479 · Boeing 737900ERSDR CALA2023082102589Skin · dentedSUPPORT TASK- R/H WING I/B FLAP I/B LOWER SURFACE DENTS DOT 49-0 19. W/C:69171 REPAIRED R/H WING I/B FLAP I/B LOWER SURFACE IAW SRM 57-52-00-30 0-095 FIG 1. W/C:69171Aug 19, 2023 · N824UA · Airbus A319131SDR DALA2023082106760Unknown · unknownDENT #9 OUT OF LIMITS ON LOWER SURFACE OF AFT MOVABLE FLAP VANE AT RH WING. SEPARATE ITEMS ON NRC 00101. SUMMARY OF NRC 563: DENT #9 ON LOWER SURFACE OF AFT MOVABLE FLAP VANE AT RH WING WAS REPAIRED PER B717-200 SRM 57-53-01-2R REPAIR 1. (LP #2925376)Aug 19, 2023 · N922AT · Boeing 717200SDR VNAA202310090013Skin · nickedSEVERAL NICKS AND DENTS ON LOWER SKIN OF RH INBOARD FLAP FLS 15.00 TO FLS 65.5. SEVERAL NICKS ON LOWER SKIN OF RH INBOARD FLAP FLS 15.00 TO FLS 65.5 WERE REMOVED PER CRJ900 SRM 51-12-00-001-001-A01; WERE EVALUATED WITHIN LIMITS BTW FLS 45 TO FLS 65 AND WERE EAug 17, 2023 · N555NN · Cndair CL6002D24SDR DALA2023082306860Unknown · unknownSHIP 3126 CORROSION INTERCONNECTING STRUT OB FLAP ON RH WING. CORRECTIVE ACTION: REPLACED INTERCONNECTING STRUT OB FLAP ON RH WING PER AMDS 2750-6010-RT. (2922798)Aug 17, 2023 · N326NB · Airbus A319114SDR FDEA202308161448Skin · dentedLH OB FLAP LOWER SURFACE FROM IB TO OB 15.5 INCH CROSS TE TO LE 4 INCH FOUND ONE DENT. EVALUATED LH OB FLAP LOWER SURFACE FROM IB TO OB 15.5 INCH CROSS TE TO LE 4 INCH ONE DENT DAMAGE SIZE L X W=4"X2" WITH DISBOND WITHIN REPAIR LIMIT AS PER B777 SRM 57-53Aug 16, 2023 · N884FD · Boeing 777FS2SDR SWAA2023092589581Flap · crackedRIGHT OUTBOARD FLAP LEADING EDGE WEB CRACKED BETWEEN STA 378 AND STA 353<[01] REMOVED AND REPLACED RT WING O/B MAIN FLAP. REF. 27-51-22-00-801/ 27-51-22-400-801Aug 15, 2023 · N447WN · Boeing 7377H4SDR SWAA2023090190020Angle · crackedCRACK INTERNAL AREA INBOARD TRAILING EDGE TEE ANGLE LOCATED IRSS 214 LT WING 2023-508516<[01] REPLACED TEE ANGLE ON INTERNAL AREA INBOARD TRAILING EDGE LOC. IRSS 214 LT WING IAW B737-700 SRM 51-40-02; SRM 51-10-02 AND DWG 115A2001 REV: ?.;[02] TASK CARD COMPLEAug 15, 2023 · N410WN · Boeing 7377H4SDR FDEA202308151433Flap · dentedLH OB FLAP LWR SURFACE FROM IB TO OB 330 INCH CROSS LE TO TE 43 INCH FOUND ONE DENT. EVALUATED LH OB FLAP LWR SURFACE FROM IB TO OB 330 INCH CROSS LE TO TE 43 INCH ONE DENT WITH DAMAGE SIZE L*W=3"*2.75" WITHIN REPAIR LIMIT AS PER B777 SRM 57-53-01-1A ALLOWAug 15, 2023 · N855FD · Boeing 777FS2SDR SWAA2023091989059Panel · crackedCRACK ACCESS PANEL 661BB TRAILING EDGE AROUND HOLES RT WING 2023-506795<[01] TOOL USED CALIPER PN:500-197-30; SN:15120589; DUE DATE: 13-FEB-24.;[02] EQUIPMENT P/N EPOCH 650; S/N 201036102; DUE DATE 16-SEP-23 WAS USED.;[03] TOOL USED: HOT BONDER P/N: HCS9200B SAug 13, 2023 · N7831B · Boeing 7377CTSDR CALA2023081602538Flap · dentedSUPPORT TASK- R/H WING I/B FLAP I/B LOWER SURFACE DENTS DOT 49-0 19. W/C:69171 REPAIRED R/H WING I/B FLAP I/B LOWER SURFACE IAW SRM 57-52-00-30 0-095 FIG 1. W/C:69171Aug 13, 2023 · N824UA · Airbus A319131SDR SWAA2023092588474Support · crackedRIGHT WING CORRUGATED PANEL CRAKED AT T/E B/W ACCESS DOOR 651DB AND FLAL TRACK<[01] REMOVED AND REPLACED CORRUGATED PANEL SUPPORT AT ACCESS PANEL 651DB AS PER REF SRM 51-40-02-OG-0;[02] VERIFIED STEP 1;[03] COMPLETED BONDING CHECK AS PER REF SOPM20-20-00 TOOL Aug 11, 2023 · N8301J · Boeing 7378H4SDR SWAA2023090188444Panel · crackedCRACK ACCESS PANEL 661BB AT RT WING 2023-508347<[01] TOOL USED: CALIPER P/N: 500-197-30; S/N: 15120589; DUE DATE: 13-FEB-24.;[02] TOOL USED: UT EQUIPMENT P/N: EPOCH 650; S/N: 190859705; CAL DUE DATE: 16-SEP-23;[03] TOOL USED: HOT BONDER: P/N:HCS9200B-AV S/N:18Aug 11, 2023 · N410WN · Boeing 7377H4SDR SWAA2023090188445Panel · crackedCRACK ON BRACKET ACCESS PANEL 651FB AT RT WING 2023-508349<[01] REPLACED BRACKET ON ACCESS PANEL 651FB AT RT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02.;[02] TASK CARD COMPLETEDAug 11, 2023 · N410WN · Boeing 7377H4SDR SWAA2023082988451Retainer · crackedRIGHT WING T/E VERTICAL SEAL RETAINER IS CRACKED AT ORSS 268 JUST ABOVE AFT PYLON FAIRING TIP<[01] REMOVED AND REPLACED RIGHT WING T/E VERTICAL SEAL RETAINER IAW SRM 51-40-02 AND DWG NO. 115A2930;[02] CERTIFIED STEP 1 AND THE MEASUREMENT TABLE;[03] INSPECTED AAug 11, 2023 · N420WN · Boeing 7377H4SDR SWAA2023082988452Retainer · crackedLEFT WING T/E VERTICAL SEAL RETAINER IS CRACKED AT ORSS 268 JUST ABOVE AFT PYLON FAIRING TIP<[01] REMOVED AND REPLACED LEFT WING T/E VERTICAL SEAL RETAINER IAW SRM 51-40-02 AND DWG NO. 115A2930;[02] CERTIFIED STEP 1 AND THE MEASUREMENT TABLE;[03] INSPECTED ANDAug 11, 2023 · N420WN · Boeing 7377H4SDR SWAA2023082488453Support · crackedLEFT WING T/E PANEL SOPPORT IS CRACKED AT ORSS 278<[01] REMOVED AND REPLACED L/W T/E PANEL SUPPORT BRACKET IAW SRM 51-40-02-0G-0;[02] CERTIFIED STEP 1 AND MEASUREMENT TABLE;[03] VERIFIED MEASUREMENTS TABLE.<BR>VERIFIED CORRECTIVE ACTIONS 1 & 2. CARD COMPLETE.Aug 11, 2023 · N420WN · Boeing 7377H4SDR SWAA2023090188256Flap · debondedCUSTOMER REQUEST - DEBONDED EXTERNAL SKIN OB AFT FLAP LOWER SURFACE IB AREA AT LT WING 2023-508262<[01] TOOL USED: CALIPER P/N:500-197-30 S/N:B20189416 DUE DATE: 19-DEC-23.;[02] TOOL USED BOND TESTING UNIT PN: BONDMASTER 600M; SN: 220052310; DUE DATE: 31 OCT 2Aug 10, 2023 · N410WN · Boeing 7377H4SDR SWAA2023090188253Flap · debondedCUSTOMER REQUEST - DEBONDED EXTERNAL SKIN OB AFT FLAP UPPER SURFACE IB CORNER AT RT WING 2023-508263<[01] TOOL USED: CALIPER P/N:500-197-30 S/N:B20189416 DUE DATE: 19-DEC-23.;[02] TOOL USED: CALIPER P/N:500-464 S/N:B17030933 DUE DATE:17-OCT-23.;[03] TOOL USED Aug 10, 2023 · N410WN · Boeing 7377H4SDR SWAA2023083087655Fairing · elongated#6 FLAP SUPPORT FAIRING (CANOE) HAS ELONGATED FASTENER HOLES AT O/B CENTER BULB SEAL.<[01] REPAIRED DAMAGED FASTENER HOLES PER SRM 57-53-70-2R-2.Aug 10, 2023 · N8549Z · Boeing 7378H4SDR I5EA2023081100011Unknown · unknownR/H FWD FLAP HAS RUB DAMAGE AT LOWER O/B END OF FLAP. CUT OUT DAMAGED SECTION AND INSTALLED REPAIR DOUBLER IAW B737-300 SRM 51-40-02 AND B737-300 SRM 57-53-01 REPAIR 1.Aug 10, 2023 · N629SW · Boeing 7373H4SDR CALA2023081102490Skin · unknownGENERATING ITEM EA5100-0234 REV E: REENFORCEMENT REPAIR FOUND ON LEFT WING OUTBOARD MAIN FLAP BOTTOM SIDE SKIN OUTBOARD AFT LOWER CORNER MEASURING APPROX. 10 INCHES BY 5 INCHES. FOUND REPAIR NOT MATCHING THE CURRENT SRM. B757 SRM-57-53-01-2R-4 AND PER PAGE 2 OAug 9, 2023 · N33103 · Boeing 757224SDR DALA2023081106559Unknown · unknown(LOG 2909732) RH WING, REAR SPAR INBOARD TRAILING EDGE FLAP STA 253.00, UNDER FIXED UPPER PANEL, RH SIDE, DEFLECTION CONTROL RIB WITH CRACK. RH WING, REAR SPAR INBOARD TRAILING EDGE FLAP STA 253.00, UNDER FIXED UPPER PANEL, RH SIDE, DEFLECTION CONTROL RIB WAS Aug 8, 2023 · N380DA · Boeing 737832SDR DALA2023080906495Unknown · unknownSHIP 3122 CORROSION SPOTS FOUND ON OUTB'D AND INB'D SURFACES OF LUG FITTING AT FLAP TRACK 2 LEVEL OF INB'D FLAP ON LH WING. CORRECTIVE ACTION: REPAIRED PER 604916-14. (2907512)Aug 8, 2023 · N322NB · Airbus A319114SDR DALA2023090807361Unknown · unknownSHIP 3117 CORROSION FLAP TRACK 3 RIB6 AND FLAP TRACK 4 RIB15 ON INTERNAL AREA O/B FLAP RH WING. CORRECTIVE ACTION: REPLACED OUTBOARD FLAP RH WING AS PER AMDS CARD 2750-1020-RT AND AMDS CARD 2750-6020-RT. (2906226)Aug 7, 2023 · N317NB · Airbus A319114SDR SWAA2023082886357Panel · pulledR/W T/E PANEL 661AB HAS SEVERAL PULLED FASTENER HOLE ON AFT END (MARKED)<[01] R/W T/E PANEL 661AB WITH SEVERAL PULLED FASTENER HOLE ON AFT ENDWAS REPAIRED IAW SRM 51-70-04-2R-9.;[02] DAMAGE WAS REPAIRED IAW SRM 51-70-04-2R-9.VERIFIED CURE TAPES UPLOADED.JOB COAug 6, 2023 · N413WN · Boeing 7377H4SDR SWAA2023080986421Fairing · out of limits#6 FLAP CANOE FAIRING; TAIL CONE ASSY; #6 FLAP CANOE FAIRING TAIL CONE ASSY TEMP. RIVET HOLE IS OUT OF LIMITS PER SRM.<[01] R AND R #6 FLAP CANOE TAIL CONE FAIRING PER AMM 27-51-18.Aug 6, 2023 · N8649A · Boeing 7378H4SDR FDEA202308051525Flap · cracked2EA CRACKS (30MM & 4MM) WERE FOUND AT L/H WING CENTER FLAP RIB26 AFT AREA OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE RIB FLANGE REPAIR AND LOWER SKIN EXTERNAL DOUBLERS REPAIR (LOWER SKIN CUT OUT WAS FOR ACCESS REQUIREMENT) I.A.W FEDEX EA NO:T6-5750-T03283Aug 5, 2023 · N652FE · Airbus A300*SDR FDEA202308051522Flap · cracked2EA CRACKS (30MM & 7MM) WERE FOUND AT L/H WING CENTER FLAP RIB25 AFT AREA OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE RIB FLANGES AND LOWER SKIN CUT OUT, REPAIRED WITH REPAIR ANGLES AND DOUBLERS (LOWER SKIN CUT OUT WAS FOR ACCESS REQUIREMENT) I.A.W FEDEX EAug 5, 2023 · N652FE · Airbus A300*SDR DALA2023082106815Unknown · unknownSHIP 3126 CORROSION INTERCONNECTING STRUT OB FLAP ON LH WING. CORRECTIVE ACTION: REPLACED INTERCONNECTING STRUT OB FLAP ON LH WING AS PER A320 FAM AMM 27-51-44-000-001-A AND AMM 27-51-44-400-001-A. (2902847)Aug 5, 2023 · N326NB · Airbus A319114SDR FDEA202308031383Flap · unknownAIRCRAFT REPAIR ASSESSMENT : EXISTING DOUBLER REPAIR FOUND ON LH I/B FLAP LWR SKIN AT T/E RIB 14A,T/E-10" COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFRAug 3, 2023 · N652FE · Airbus A300*SDR FDEA202308031380Flap · unknownAIRCRAFT REPAIR ASSESSMENT : EXISTING DOUBLER REPAIR FOUND ON RH CENTER FLAP LWR SKIN BTW RIB 9~10,REAR SPAR DATUM 12" COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIRAug 3, 2023 · N652FE · Airbus A300*SDR DALA2023080306283Unknown · unknownCRACK ON FLAP VANE INBOARD SIDE STA XFLS 127 APPROX AT RIGHT WING. (AD) SUMMARY OF NRC 00051: FLAP VANE INBOARD SIDE STA XFLS 127 APPROX AT RIGHT WING WAS REPAIRED PER ER/A 610662-14 REV. ASSOCIATED ER/A 14-610662 ADDED FOR AC 9576. (LP #2898258)Aug 2, 2023 · N608AT · Boeing 717200SDR DALA2023080306279Unknown · unknownDENT ON INBD LH FLAP FIXED VANE, BTW XRS 162 TO 166 AT LH WING. SUMMARY OF NRC 00104: INBD LH FLAP FIXED VANE, BTW XRS 162 TO 166 AT LH WING, WAS REPAIRED PER B717-200 SRM 57-53-01-2R-1 REPAIR 1. (LP #2897695)Aug 2, 2023 · N978AT · Boeing 717200SDR SWAA2023090784733Retainer · crackedCRACK FLAP TRACK FAIRING 8 ON RETAINER SEAL AT RT WING 2023-477583<[01] REPLACED FLAP TRACK FAIRING 8 ON RETAINER SEAL AT RT WING IAW B737-700 SRM 51-40-02-0G-0 AND DWG 113A9130 SHEET 1 REV B;[02] REPLACED FLAP TRACK FAIRING 8 ON RETAINER SEAL AT RT WING IAW BAug 1, 2023 · N449WN · Boeing 7377H4SDR CALA2023080202409Flap · damagedPDA 2 REF LOG PAGE5332880, FOA RIGHT HAND OUTBOARD FLAP, TRAILING EDGE INBOARD SIDE MISSING ALUMINUM COVER OVER HONEYCOMB. APPROX 10 INCHES X 10 INCHES EXPOSED. QC ACCOMPLISHED PREINSTALLATION INSPECTION INTERFACE AND NEW PART NUMBER IAW AMM 27-51-21. REMOVED Aug 1, 2023 · N68843 · Boeing 737924ERSDR FDEA202308011343Flap · delaminatedLH OB FLAP LWR SURFACE FROM IB TO OB 12 INCH CROSS TE TO LE 11.8 INCH FOUND ONE DENT EVALUATED LH OB FLAP LWR SURFACE FROM IB TO OB 12 INCH CROSS TE TO LE 11.8 INCH ONE DENT WITH DELAMINATION DAMAGE SIZE LXW=1.8"X1.0" OUT OF ALLOWABLE LIMIT AS PER B777 SRAug 1, 2023 · N891FD · Boeing 777FS2SDR DALA2023080106212Unknown · unknownDENT ON LOWER SURFACE OF AFT MOVABLE VANE AT LH FLAP. SUMMARY OF THE NRC 00359: AFT MOVABLE VANE AT LH FLAP WAS REMOVED PER B717 AMM 27-50-03 AND DENT REPAIRED PER B717 SRM 51-70-02-0G PROCEDURE GENERAL AND SRM 57-53-01 FIG 201. REFER TO AMDS 2750-4007 FOR COMAug 1, 2023 · N922AT · Boeing 717200SDR IXXA2024073101Skin · dentedLEFT WING TRAILING EDGE INBD AFT FLAP DENTEDJul 31, 2023 · N359AZ · Boeing 767323SDR DALA2023080106210Unknown · unknownDISBOND ON RH CENTER FIXED VANE, UPPER SURFACE OF 0.700IN LENGTH X 0.600IN WIDTH AT DENT #1, (53.25" FROM IB EDGE, 5" FROM TE) IN REF MON JOB 032-0001 LOG 1549344. SUMMARY OF NRC 00407: RH CENTER FIXED VANE, UPPER SURFACE WAS REPAIRED PER B717-200 SRM 57-53-01Jul 31, 2023 · N959AT · Boeing 717200SDR CALA2023073102384Doubler · missingFOUND REPAIR DOUBLER MISSING FROM LOWER TRAILING EDGE SURFACE OF LEFT INBD FLAP. DOUBLER WOULD BE ALUMINUM, MEASURING ROUGHLY 5X5 INCHES. CONTACTED ENGINEERING AND TOMC. REF LP 5308893 FOR DISPOSITION OF DISCREPANCY. C/W ECRA 5750-05395 INTERIM REPAIR TO DISPAJul 30, 2023 · N16217 · Boeing 737824SDR SWI2023F00401Unknown · damaged*L/H INBD FLAP HINGE BOX @ WS54.55 OTBD LUG HAS TOOLING MARKS (MARKED),MX#26956246 (C-CHECK RO 10/4/2023) BLENDED AND FOUND OUT OF LIMITS. REPAIRED PER BOMBARDIER REO 670-57-54-058 REV-- DATE 2023-08-14. SEE CONTINUATION CARD FOR DETAILS.COMPLIED WITH TJul 29, 2023 · N728SK · Cndair CL6002C10SDR SWAA2023082283846Flap · delaminatedR/H WING; OUTBOARD AFT FLAP; DELAMINATED.<[01] REMOVED ' R/H WING; OUTBOARD AFT FLAP' IAW AMM 27-51-22.;[02] OK TO INSTALL FLAP 113A3700-28 SERIAL 005289.;[03] INSTALLED AND TORQUED O/B AFT FLAP IAW AMM 27-51-22. FOR TRACK REPLACEMENT SEE FAULT TTG8Q00LHSD7 (#Jul 29, 2023 · N8671D · Boeing 7378H4SDR SWIA20231027028Unknown · chafedLEFT INBOARD FLAP VANE LEADING EDGE IS CHAFED AT WS97. S/N 111 (C-CHECK RO 10/29/2023) REMOVED AND INSTALLED NEW L/H INBOARD FLAP VANE LEADING EDGE CRJ 200 SRM 51-42-13 AND DRAWING 601R14302 REV E. COMPLIED WITH 51-900-1003-SKY AND SEE CONTINUATION CARD Jul 28, 2023 · N953SW · Cndair CL6002B19
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