JASC 5753

Service difficulty reports · 31,506

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 VNAA202410163014Skin · chafedRH IB FLAP LOWER SKIN IS CHAFED AROUND IB HINGE FAIRING PERIMETER WS54.55.Oct 20, 2024 · N718PS · Cndair CL6002C10SDR SWAA2024102350731Skin · delaminatedL/H O/B AFT FLAP HAS DELAM AREA INBD END LOWER SURFACE.<[01] REMOVED L/H O/B AFT FLAP PER AMM 27-51-22.;[02] INSTALLED L/H O/B AFT FLAP UP TO RIGGING AND ADJUSTMENT PER MM 27-51-22;[03] INSTALLED L/H O/B AFT FLAP UP TO AND INCLUDING STEP 3(F)(5) RIGGING AND ADOct 19, 2024 · N8662F · Boeing 7378H4SDR CALA2024102302713Skin · crackedRT WING I/B FLAP BOTTOM SKIN CRACKED. REPAIRED RT IB FLAP BOTTOM SKIN AND INSTALLED DOUBLER IAW A319 S RM 57-52-00-300-003 A319 SRM 51-77-13-911-020 AND A319 SRM 57-52 -00-300-095 AND UAL EC/RA 5752-02019.Oct 19, 2024 · N818UA · Airbus A319131SDR FDEA202410191552Skin · dentedDENT TO INBOARD FLAP RH WING, AFT FLAP, 70 IN INBOARD TO EDGE AND 2 IN TRAILING EDGE. RH WING INBOARD FLAP, AFT FLAP WAS REPAIRED IAW B767 SRM 57-53-01-2R REP 1 FIG 201 SHEET 1 AND SHEET 4 AND SRM 51-70-03-0G FIG.16 PAR 5.L REV 90 AUG 15/2024Oct 19, 2024 · N190FE · Boeing 7673S2FSDR SWAA2024112550607Support Angle · crackedRIGHT WING UPPER T/E PANEL BULB SEAL SUPPORT ANGLE IS CRACKED AT RSS 274<[01] REMOVED; REPLACED; AND INSTALLED A NEW BULB SEAL SUPPORT ANGLE AT R/W UPPER T/E PANEL AT RSS 274 IAW SRM 51-40-02 AND IPC 57-50-00-25.;[02] VERIFIED CORRECTIVE ACTION 1Oct 18, 2024 · N7741C · Boeing 7377BDSDR SWAA2024112550614Support · crackedBULB SEAL RETAINER SUPPORT IS CRACKED AT LEFT WING FIXED T/E PANEL JUST AFT OF THE PYLON ORSS 269. MARKED<[01] REMOVED AND REPLACED BULB SEAL RETAINER SUPPORT FITTING P/N 115A2953-1; PO # 1000542/1; IAW SRM 51-40-02-0G-0 AND DWG. 115A2930; REV. -;[02] VERIFIEDOct 18, 2024 · N7741C · Boeing 7377BDSDR DALA2024102110282Skin · dentedSEVERAL DENTS ON (UPPER AND LOWER) SKIN OF FWD MOVABLE VANE AT LH WING. SUMMARY OF NRC 00630: DENTS (9 LOCATIONS) ON LOWER SKIN OF FWD MOVABLE VANE AT LH WING WERE EVALUATED WITH THE FOLLOWING DIMENTIONS WERE: DENT #1 W=0.250" Y=0.003" W/Y=83.33, DENT #2 W=0.3Oct 18, 2024 · N991AT · Boeing 717200SDR UIEA2024101501008Fuse Pin · crackedSUPPORT #6 INBOARD FLAP - FUSE PIN - UNDERWING FITTING TO FOWARD TO TENSION LINK, WITH CRACK INDICATION FOUND AND CORROSION.(<P>FUSE PIN WAS REPLACED AND TORQUE WAS APPLIED IAW AMM 27-51-02-004-001. NO FURTHER DEFECTS NOTED</P>)Oct 17, 2024 · N642GT · Boeing 7673Y0SDR UIEA2024101501010Fuse Pin · crackedSUPPORT #3 INBOARD FLAP - FUSE PIN - UNDERWING FITTING TO FOWARD TO TENSION LINK, WITH CRACK INDICATION FOUND AND CORROSION.(<P>FUSE PIN WAS REPLACED AND TORQUE WAS APPLIED IAW AMM 27-51-02-004-001. NO FURTHER DEFECTS NOTED</P>)Oct 17, 2024 · N642GT · Boeing 7673Y0SDR UIEA2024101501014Support Fitting · wornFLAP SUPPORT #1 FITTING OUTBOARD ACTUATOR SPAR FITTING WEAR FOUND 3 HOLES WITH CORROSION INDICATION (LOCATED 12:00, 08:00 AND 10:00 O´CLOCK)(<P>CORROSION WAS REMOVED, REAMING THE AFFECTED HOLES AND FREEZE PLUGS WERE INSTALLED. THIS REPAIR WAS BASED ON CMA-PAOct 17, 2024 · N642GT · Boeing 7673Y0SDR UIEA2024101501017Pin · corrodedLEFT 6-6 PIN FLAP SUPPORT #4 WITH CORROSION(<P>PIN WAS REPLACED AND TORQUE WAS APPLIED IAW AMM 27-51-04-402-135. NO FURTHER DEFECTS NOTED</P>)Oct 17, 2024 · N642GT · Boeing 7673Y0SDR DALA2024101810194Spherical Bearin · corrodedSHIP 3143 CORROSION ON HOUSING SPHERICAL BEARING TRACK 3 O/B FLAP LH WING. CORRECTIVE ACTION: COMPLIED WITH ER/A 620734-14. (0614370)Oct 17, 2024 · N343NB · Airbus A319114SDR DALA2024101810190Vane · wornWEAR ON LEADING EDGE OF AFT MOVABLE VANE LH WING. SUMMARY OF NRC 00770: WEAR ON LEADING EDGE OF AFT MOVABLE VANE LH WING WAS REPAIRED PER B717-200 SRM 57-53-01-2R PROCEDURE 1 REPAIR 1. (LP #0614293)Oct 17, 2024 · N991AT · Boeing 717200SDR DALA2024101710154Skin · wornWEAR ON UPPER SURFACE OF UPPER FIXED GUIDE VANE STA XRS=140.000 RH WING. SUMMARY OF NRC 00010: UPPER SURFACE OF UPPER FIXED GUIDE VANE STA XRS=140.000 RH WING WAS REPAIRED PER B717-200 SRM 57-53-01-2R PROCEDURE 1 REPAIR 1 PAR 4 D AND 51-70-02-0G PROCEDURE GENEOct 17, 2024 · N991AT · Boeing 717200SDR FDEA202410171534Skin · damagedPER CUSTOMER REQUEST PREVIOUS REPAIR FROM NR N00358 AT LH I/B MAIN FLAP 31.5" FROM IB EDGE (DIM. 5" ROUND) REQUIERS EXISTING REPAIR TO BE REMOVED AND REPAIR TO BE RE- ACCOMPLISHED. SEE ERS# 24-02781. PER CUSTOMER REQUEST PREVIOUS REPAIR WAS REMOVED AND REPOct 17, 2024 · N989FD · Boeing 757231SDR FDEA202410171533Skin · unknownPER CUSTOMER REQUEST PREVIOUS REPAIR FROM NR N00357 AT LH I\B MAIN FLAP 19" FROM T\E IB EDGE (DIM. W=3.300" X L=10.5") REQ EXISTING REPAIR TO BE REMOVED AND REPAIR TO BE RE- ACCOMPLISHED. SEE ERS# 24-02781. PER CUSTOMER REQUEST PREVIOUS REPAIR WAS REMOVED Oct 17, 2024 · N989FD · Boeing 757231SDR SWAA2024112549582Support Angle · crackedLEFT WING INBD. TRAILING EDGE UPPER PANEL SUPPORT ANGLE CRACKED JUST INBD. OF THE DEFLECTION CONTROL RIB.<[01] LOCATED AND DRILLED FASTENER HOLES IN NEW SUPPORT ANGLE PER SRM 51-40-05.;[02] VERIFIED WORK SIGNED IN CA#1.......LOCATED AND DRILLED FASTENER HOLES Oct 16, 2024 · N8509U · Boeing 7378H4SDR FDEA202410161529Skin · delaminatedLH WING, INBD FLAP (OUTBD SECTION), LEADING EDGE WITH DELAMINATION. LH WING INBD FLAP (OUTB SECTION) LEADING EDGE WAS REPAIRED IAW B767 SRM 57-53-01-2R REPAIR 1 FIGURE 201 (SHEET 2) AND (SHEET 5) TABLE 1 AND SRM 51-70-17-0G PAR 4.A FIGURE 10 (SHEET 1) REV Oct 16, 2024 · N170FE · Boeing 7673S2FSDR FDEA202410161528Skin · dentedRIGHT WING, INBOARD MAIN FLAP LOWER SURFACE WITH DENT AT 15" FROM OB FLAP SUPPORT AN 13" FROM LOWER EDGE RH WING INBOARD MAIN FLAP LOWER SURFACE WAS REPAIRED IAW B767 SRM 57-53-01-2R REPAIR 1 FIGURE 201 (SHEET 2) NOTE "A" AND SRM 51-70-03-0G PAR 5.L FIGUREOct 16, 2024 · N170FE · Boeing 7673S2FSDR SWAA2024111448785Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED DEFLECTION CONTROL RIB ORSS271 APROX AT RT WING 2024-634509<[01] REPLACED ANGLE TRAILING EDGE LOCATED DEFLECTION CONTROL RIB ORSS271 APROX AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: 115A2930 SHEET: 7 REOct 15, 2024 · N273WN · Boeing 7377H4SDR IXXA202411070101Skin · damagedLH WING INBD AFT FLAP OTBD END UPPER SURFACE SKIN HAS EDGE DAMAGE. HAECO WO 320009 NON ROUTINE 46446Oct 15, 2024 · N499AZ · Boeing 767323SDR FDEA202410151509Hinge Bracket · corrodedRIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE (HOLE #3) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. REPAIR BUSHING FABRICOct 15, 2024 · N618FE · Doug MD11FSDR FDEA202410151507Hinge Bracket · corrodedLEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE (HOLE #3) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. REPAIR BUSHING FABRICATOct 15, 2024 · N618FE · Doug MD11FSDR SWAA2024120648421Angle · crackedCRACK ANGLE TRAILING EDGE ACCESS PANEL 651FB RT WING 2024-633808<[01] REPLACED ANGLE TRAILING EDGE ACCESS PANEL 651FB RT WING IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DRAWING 115A2710<BR>REV A.;[02] REPLACED ANGLE TRAILING EDGE ACCESS PANEL 651FB RT Oct 14, 2024 · N269WN · Boeing 7377H4SDR SWAA2024120648419Angle · crackedCRACK ANGLE TRAILING EDGE ACCESS PANEL 551FB LT WING 2024-633809<[01] REPLACED ANGLE TRAILING EDGE ACCESS PANEL 551FB LT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND INSTALLED FASTENERS IAW B737-700 SRM 51-40-02 AND DRAWING # 115A2710; SHEET 8; REV A . TOOL USED Oct 14, 2024 · N269WN · Boeing 7377H4SDR SWAA2024112648495Skin · debondedCUSTOMER REQUEST - DEBONDED OB AFT FLAP LOWER SURFACE AT RT WING. PERFORMED INTERIM REPAIR AT O/B AFT FLAP AT RT WING IAW B737-700 SRM 57-53-01-2R-16 REPAIR 16. AND THE REPAIR REQUIRED TAP TEST INSPECTION EVERY 6;875 CYCLES OR 30 MONTHS. WHICHEVER COMES FIRSOct 14, 2024 · N204WN · Boeing 7377H4SDR SWAA2024112548637Skin · debondedCUSTOMER REQUEST - DEBONDED EXTERNAL SKIN IB MAIN FLAP TRAILING EDGE WEDGE LOWER SURFACE AT LT WING 2024-645390<[01] TOOL USED HOT BONDER P/N HCS9200B-AV S/N 18175478 DUE DATE 25/JAN/25. POSITECTOR P/N NSA S/N 110098 DUE DATE 05/SEP/25.;[02] CORRECTIVE ACTION Oct 14, 2024 · N8328A · Boeing 7378H4SDR SWAA2024112048638Flap · debondedCUSTOMER REQUEST - DEBONDED EXTERNAL SKIN IB MAIN FLAP TRAILING EDGE WEDGE LOWER SURFACE AT RT WING 2024-645392<[01] TOOL USED; CALIPER PN: 500-196-30; SN: A19317217; DUE DATE: 16-MAY-25.;[02] TOOL USED CALIPER PN: 500-196-30; SN: A19317217; DUE DATE: 16-MAY-2Oct 14, 2024 · N8328A · Boeing 7378H4SDR SWAA2024112048640Flap · debondedCUSTOMER REQUEST - DEBONDED EXTERNAL SKIN OB AFT FLAP LOWER SURFACE IB SIDE AT LT WING 2024-645399<[01] TOOL USED: CALIPER P/N:500-197-30 S/N:B20189521 DUE DATE: 26-JAN-25;[02] STEP 3. TOOL USED ULTRASONIC EQUIPMENT PN: USM GO+ ; SN: USMGO11040089; DUE DATE: 2Oct 14, 2024 · N8328A · Boeing 7378H4SDR DALA2024101510103Flap Track · corrodedSHIP 3134 CORROSION ON INTERNAL AREA LOC. BTW RIB5 AND RIB6 FLAP TRACK 3 ON LH WING. CORRECTIVE ACTION: REMOVED O/B FLAP ON L/H WING ON UNSERVICEABLE CONDITION. (0608894)Oct 14, 2024 · N334NB · Airbus A319114SDR SWAA2024111448083Support Angle · corrodedCORROSION SUPPORT ANGLE TRAILING EDGE LOCATED ORSS338 TO ORSS439 AT LT WING 2024-634422<[01] REPLACED SUPPORT ANGLE TRAILING EDGE LOCATED ORSS338 TO ORSS439 AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: 115A3700 SHEET: 43 REV A SEE INDIVIDOct 13, 2024 · N273WN · Boeing 7377H4SDR SWAA2024111448081Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED DEFLECTION CONTROL RIB IRSS271 APROX AT LT WING 2024-634426<[01] REPLACED BLADE XXX IAW B737-700 SRM 51-10-02-0G-0 ITEM 9; SRM 51-40-02-0G-0 AND DWG 186A3005-4 SHEET:2 REV:B AND MEASURES OF CRACK IS :L= 0.176? INCHES TOOL USEDOct 13, 2024 · N273WN · Boeing 7377H4SDR SWAA2024110648128Skin · delaminatedLEFT WING OUTBOARD AFT FLAP; THE INBOARD UPPER SURFACE HAS AN AREA OF DELAMINATION. (MARKED)<[01] REMOVED L/H OUTBD AFT FLAP PER AMM 27-51-22;[02] INSTALLED SERVICEABLE REPLACEMENT L/H OUTBD AFT FLAP IAW AMM 27-51-22-400-801.;[03] INSPECTED WORK PERFORMED ON COct 13, 2024 · N8671D · Boeing 7378H4SDR DALA2024101410090Fairing · delaminatedSHIP 3157 LH WING OTBD FLAP INBD MOVEABLE FAIRING INBD IS DELAMINATED. CORRECTIVE ACTION: REPAIR AND OR REPLACEMENT WITHIN 250 FH, REF SRM 57-55-11-283-001. REPAIR REF SRM 51-77-13. (0605777)Oct 12, 2024 · N357NB · Airbus A319114SDR DALA2024101410072Housing · corrodedSHIP 3144 CORROSION ON HOUSING SPHERICAL BEARING OF INBOARD FLAP RH WING. CORRECTIVE ACTION: COMPLIED BY ER/A 620763-14. (0604237)Oct 11, 2024 · N344NB · Airbus A319114SDR DALA2024101410067Flap Track · corrodedSHIP 3133 CORROSION ON BORE BEARING TRACK 2 I/B FLAP ON L/H WING. CORRECTIVE ACTION: COMPLIED WITH ER/A 621041-14. (0604420)Oct 11, 2024 · N333NB · Airbus A319114SDR DALA2024101410066Flap Track · corrodedSHIP 3133 CORROSION ON BORE BEARING TRACK 2 I/B FLAP ON L/H WING. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS ON ATTACHMENT FITTING OF TRACK 2 I/B FLAP ON L/H WING AS PER ER/A 621041-14. (0604416)Oct 11, 2024 · N333NB · Airbus A319114SDR DALA2024101410043Vane · dentedDENTS ON UPPER SURFACE OF AFT MOVABLE FLAP VANE ON RIGHT WING. SUMMARY OF NRC 00623: DENTS (9 LOCATIONS) ON UPPER SURFACE OF AFT MOVABLE FLAP VANE ON RIGHT WING WERE DENT #1 W=0.400" Y=0.001" W/Y=400 DENT #2 W=0.350" Y=0.001" W/Y=350 DENT #3 W=0.343" Y=0.001" Oct 11, 2024 · N991AT · Boeing 717200SDR DALA2024101410042Vane · dentedDENTS ON LWR SURFACE OF FWD MOVABLE FLAP VANE ON RIGHT WING. SUMMARY OF NRC 00624: DENTS (7 LOCATIONS) ON LWR SURFACE OF FWD MOVABLE FLAP VANE ON RIGHT WING (DENT #1 W=0.218" Y=0.005" W/Y=43.6, DENT #2 W=0.320" Y=0.012" W/Y=26.66, DENT #6 W=0.250" Y=0.008" W/YOct 11, 2024 · N991AT · Boeing 717200SDR SWAA2024120647162Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED ORSS 270 DEFLECTION CONTROL RIB AREA AT RT WING 2024-633618<[01] REPLACED ANGLE TRAILING EDGE LOCATED ORSS 270 DEFLECTION CONTROL RIB AREA AT RT WING I.A.W B737-700 SRM 51-40-02 AND 51-10-02 ITEM 9.<BR>TOOK MEASURES OF CRACK: Oct 10, 2024 · N269WN · Boeing 7377H4SDR SWAA2024110747347Skin · delaminatedLEFT WING INBOARD MAIN FLAP TRAILING EDGE WEDGE IS DELAMINATED ON TRAILING EDGE.<[01] REMOVED LEFT WING INBOARD MAIN FLAP TRAILING EDGE WEDGE PER SRM 51-40-02.;[02] PART REMOVAL ONLY;[03] DRILL NEW LEFT WING INBOARD MAIN FLAP TRAILING EDGE WEDGE (TOP SIDE ONLYOct 10, 2024 · N8671D · Boeing 7378H4SDR DALA2024101109995Plate · corrodedSHIP 3133 CORROSION DAMAGES WERE FOUND AFFECTING THE IB AND OB AL PLATES AT TRACK #2 LEVEL, RIB 9, BEARING HOUSING AREA.CORRECTIVE ACTION: COMPLIED WITH ER/A 621041-14. (0602573)Oct 10, 2024 · N333NB · Airbus A319114SDR FDEA202410101479Skin · dentedRH WING, OUTBOARD TRAILING EDGE FLAP AT OTEF 351 APPROX, LOWER SURFACE, MIDDLE SKIN WITH DENT RH WING, OUTBOARD TRAILING EDGE FLAP AT OTEF 351 APPROX, MIDDLE SKIN WAS REPAIRED IAW B767 SRM 57-53-01-2R REP 1 FIG 201 (SHEET 3) AND SRM 51-70-10-2R REP 4 FIG 2Oct 10, 2024 · N274FE · Boeing 7673S2FSDR FDEA202410101478Skin · dentedLH WING, INBOARD AFTER FLAP, LOWER SKIN SURFACE, WITH DENT, AT IFS 162, AND 7 FROM THE AFT EDGE LH WING, INBOARD AFTER FLAP, LOWER SKIN SURFACE, AT IFS 162, AND 7 FROM THE AFT EDGE WAS REPAIRED IAW B767 SRM 57-53-01-2R REP 1 FIG 201 (SHEET 4) PAG 1-4 ANDOct 10, 2024 · N274FE · Boeing 7673S2FSDR FDEA202410101477Skin · dentedLH WING, INBOARD AFTER FLAP, LOWER SKIN SURFACE, WITH DENT, AT IFS 162.75 AND 1.5 FROM THE AFTER EDGE. LH WING, INBOARD AFTER FLAP, LOWER SKIN SURFACE, AT IFS 162.75 AND 1.5 FROM THE AFTER EDGE WAS REPAIRED IAW B767 SRM 57-53-01-2R REP 1 FIG 201 (SHEET 4Oct 10, 2024 · N274FE · Boeing 7673S2FSDR FDEA202410101476Skin · dentedLH WING, INBOARD AFTER FLAP, LOWER SKIN SURFACE, WITH DENT, AT IFS 162.5, AND 6.5 FROM THE AFTER EDGE. LH WING, INBOARD AFTER FLAP, LOWER SKIN SURFACE, AT IFS 162.5, AND 6.5 FROM THE AFTER EDGE WAS REPAIRED IAW B767 SRM 57-53-01-2R REP 1 FIG 201 (SHEET 4Oct 10, 2024 · N274FE · Boeing 7673S2FSDR FDEA202410101467Bracket · corrodedRIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE (HOLE #3) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-07. REPAIR BUSHING FABRICOct 10, 2024 · N596FE · Doug MD11FSDR FDEA202410101466Bracket · corrodedLEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE (HOLE #3) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-07. REPAIR BUSHING FABRICATOct 10, 2024 · N596FE · Doug MD11FSDR SWAA2024110746936Angle · crackedLT WING L-ANGLE CRACKED AT DEFLECTION RIB O/B #3 FLAP TRACK AT FWD WEB SUPPORT<[01] REMOVED ANGLE FROM AIRCRAFT I.A.W SRM 51-40-02.;[02] REMOVED AND REPLACED DEFLECTION RIB CLIP I.A.W SRM 51-40-02.;[03] DUSTIN WYATT (TECHNICIAN); 17-OCT-2024 20:21 UTC<BR>REMOVOct 9, 2024 · N8671D · Boeing 7378H4SDR SWAA2024102846825Skin · delaminatedL/H WING O/B AFT FLAP HAS LARGE AREA OF DELAMINATION LWR SURFACE I/B AFT END<[01] CERTIFY STEP 1 ITEM 7.;[02] REMOVED AND INSTALLED SERVICABLE L/W O/B AFT FLAP AND VERIFEID PROPER ADJUSTMENT IAW AMM 27-51-22;[03] TASK COMPLETE;[04] VERIFIED CORRECTIVE ACTION IOct 9, 2024 · N431WN · Boeing 7377H4
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