JASC 5753

Service difficulty reports · 31,496

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 DALA2025010600081Roller · out of limitsSHIP 3147 OUT LIMIT 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 SUB TASK 57-53-21-000-006-A01 AND TASK 57-53-21-400-810-A01 SUB TASK 57-53-21-440-010-A01. (Jan 5, 2025 · N347NB · Airbus A319114SDR DALA2025010600080Roller · out of limitsSHIP 3147 OUT LIMIT CRUISE ROLLER IS 0.40MM OB FLAP ON LH WING. CORRECTIVE ACTION: REPLACED CRUISE ROLLER OB FLAP ON LH WING AS PER AIRBUS CMM 57-53-21 AND TASK 57-53-21-400-810-A01. (0746529)Jan 5, 2025 · N347NB · Airbus A319114SDR DALA2025010600079Bearing · corrodedSHIP 3147 CORROSION O/B SPHERICAL BEARING ON O/B LH FLAP. CORRECTIVE ACTION: REPLACED O/B SPHERICAL BEARING ON O/B LH FLAP AS PER A320 AMM 57-53-21-000-001-A AND AMM 57-53-21-400-001-A. (0746491)Jan 5, 2025 · N347NB · Airbus A319114SDR SWAA2025021183007Wedge · debondedCUSTOMER REQUEST - DEBONDED EXTERNAL SKIN IB MAIN FLAP TRAILING EDGE WEDGE LOWER SURFACE AT LT WING 2024-779218<[01] ON STEP 2: TOOL USED AUDIBLE BOND TESTER PN: S-3; SN: 064; DUE DATE: 27 AUG 25.;[02] REPAIRED IB MAIN FLAP TRAILING EDGE WEDGE LOWER SURFACE ATJan 4, 2025 · N8611F · Boeing 7378H4SDR SWAA2025021183008Wedge · debondedCUSTOMER REQUEST - DEBONDED EXTERNAL SKIN IB MAIN FLAP TRAILING EDGE WEDGE LOWER SURFACE AT RT WING 2024-779222<[01] TOOL USED: HOT BONDER P/N: HCS9200B; S/N: 18165044; DUE DATE: 11-APR-25.<BR>POSITECTOR PN: NS2; S/N: 110098; DUE DATE: 05-SEP-25.;[02] TOOL USEJan 4, 2025 · N8611F · Boeing 7378H4SDR SWIA20250430103Hinge Arm · looseR/H WING O/B FLAP O/B HINGE ARM AFT FITTING (ON FLAP) FWD FAIRING MOUNT BRACKET LOOSE (C-CHECK RO 04/30/2025)ACCOMPLISHED REO NO 670-57-53-401 REV --. 2025-02-22. AT BLENDED CORROSION DAMAGE TO R/H WING I/B & O/B HIGNE FITTING HALF AT WS 264.00 (FOR WORK INPRJan 3, 2025 · N765SK · Cndair CL6002C10SDR SWAA2025012382572Skin · delaminatedL/H O/B AFT FLAP DELAMINATED AT UPPER AND LOWER SKINS BETWEEN 72' INCHES AND 110' INCHES FROM I/B EDGE.<[01] 01 - REMOVED AND REPLACED PER [AMM 27-51-22-400-801-NG (OUTBOARD AFT FLAP INSTALLATION - PERMANENT)];[02] 02 - INSPECTED PER [AMM 27-51-22-400-801-NG (Jan 3, 2025 · N8673F · Boeing 7378H4SDR SWI2025F00303Vane · wornWEAR MARKS NOTED AT L/H INBD FLAP VANE ACTUATOR COMMON TO PANEL #584DB (MARKED) (C-CHECK RO 3/5/2025) REPAIRED LH INBD FLAP VANE ACTUATOR COMMON TO PANEL 584DB REF REO 670-57-52-257 REV.-A DATED 2024-08-20. COMPLIED WITH 51-900-1002-SKY. OPS CHECK GOOD.Jan 2, 2025 · N764SK · Cndair CL6002C10SDR SWI2025F00302Vane · wornWEAR MARKS NOTED AT L/H INBD FLAP VANE ACTUATOR COMMON TO PANEL #584CB (MARKED) (C-CHECK RO 3/5/2025) REPAIRED LH INBD FLAP VANE ACTUATOR COMMON TO PANEL 584CB REF REO 670-57-52-257 REV. -A DATED 2024-08-20. COMPLIED WITH 51-900-1002-SKY. OPS CHECK GOODJan 2, 2025 · N764SK · Cndair CL6002C10SDR SWI2025F00301Valve Spring · wornWEAR MARKS NOTED AT L/H INBD FLAP VANE ACTUATOR COMMON TO PANEL #584BB (MARKED) (C-CHECK RO 3/5/2025) REPAIRED LH INBD FLAP VANE ACTUATOR COMMON TO PANEL 584BB REF REO 670-57-52-257 REV. -A DATED 2024-08-20. COMPLIED WITH 51-900-1002-SKY. OPS CHECK GOODJan 2, 2025 · N764SK · Cndair CL6002C10SDR SWIA20250306102Vane · wornWEAR MARKS NOTED AT L/H INBD FLAP VANE ACTUATOR COMMON TO PANEL #584AB (MARKED) (C-CHECK RO 3/5/2025) REPAIRED LH INBD FLAP VANE ACTUATOR COMMON TO PANEL 584AB REF REO 670-57-52-257 REV.-A DATED 2024-08-20. COMPLIED WITH 51-900-1002-SKY. OPS CHECK GOOD.Jan 2, 2025 · N764SK · Cndair CL6002C10SDR DALA2025010900180Skin · corrodedSHIP 3136 CORROSION LOWER SKIN BTW RIB 17 TO RIB 19 TRAILING EDGE LH WING. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS AS PER A319 SRM 57-21-11-283-026. (0738505)Dec 31, 2024 · N336NB · Airbus A319114SDR DALA2025010200014Bearing · wornSHIP 3409 OUTBOARD FLAP. THE OUTBOARD FLAP OUTBOARD SIDE ROLLER/BEARING IS WORN. CORRECTIVE ACTION: REPLACED ROLLER ASSY PER A330 AMM 27-54-73. OK FOR SVC. (0738147)Dec 31, 2024 · N409DX · Airbus A330941SDR DALA2024123012072Flap Track · brokenSHIP 3327 LH WING NO.3 FLAP TRACK REAR LINK BEARING FOUND BROKEN. CORRECTIVE ACTION: LH WING NO.3 FLAP TRACK REAR LINK REMOVED AND REPLACED AS PER A330 AMM 27-54-75, FLAP SYSTEM OPERATIONAL TEST PERFORMED AS PER A330 AMM 27-54-00 AND FOUND SATISFACTORY. (07339Dec 29, 2024 · N827NW · Airbus A330302SDR DALA2024123012066Vane · dentedSEVERAL DENTS ON LOWER SKIN LH AFT MOVEABLE FLAP VANE. SUMMARY OF NRC 00250: DENTS (8 EA) ON LOWER SKIN LH AFT MOVABLE FLAP VANE WERE EVALUATED AND DENTS #1 TO #7 ARE OUT OF LIMITS PER B717-200 SRM 57-53-01-1A PROCEDURE 1 ALLOWABLE DAMAGE 1 PAR 3. A. AND WERE Dec 27, 2024 · N995AT · Boeing 717200SDR SWAA2025020381017Flap · debondedCUSTOMER REQUEST - DEBONDED OB AFT FLAP ON IB SIDE AT LT WING 2024-773695<[01] EQUIPMENT USED P/N: BONDMASTER 600M; S/N: 230106912; DUE DATE: 09-JAN-25;[02] TOOL USED; HOT BONDER PN: HCS9200B; SN: 15102320; DUE DATE: 25-JAN-25. CALIPER PN: 500-197-30; SN: A18Dec 26, 2024 · N213WN · Boeing 7377H4SDR AALA202412309509Skin · delaminatedAIRCRAFT IN BASE MAINTENANCE: LEFT WING INBOARD TRAILING EDGE FLAP UPPER SURFACE DELAMINATED. REPAIRED FLAP PER SRM 51-70-04-2R REPAIR 2.Dec 26, 2024 · N787AL · Boeing 777223SDR VNAA202412240020Skin · chafedHN00180225 DISCREPANCY: L/H WING, LOWER SKIN IS CHAFED JUST FORWARD OF THE INBOARD FLAP, INBOARD HINGE BOX. DAMAGE FROM CONTACT WITH FLAP FAIRING. CORRECTIVE ACTION: REPAIRED IAW MHIRJ REO 670-57-21-990 REV-- DATED 2024-09-10 CC670-10046/10045Dec 24, 2024 · N703PS · Cndair CL6002C10SDR VNAA202412240019Skin · chafedHN00180224 DISCREPANCY: L/H WING, LOWER WING SKIN IS CHAFED JUST FORWARD OF INBOARD FLAP, OUTBOARD HINGE BOX. DAMAGE FROM CONTACT WITH FLAP FAIRING. CORRECTIVE ACTION: REPAIRED IAW MHIRJ REO 670-57-21-990 REV-- DATED 2024-09-10 CC670-10046/10045Dec 24, 2024 · N703PS · Cndair CL6002C10SDR VNAA202412240018Skin · chafedHN00180223 DISCREPANCY: L/H WING, LOWER SKIN IS CHAFED JUST FORWARD OF THE OUTBOARD FLAP, INBOARD HINGE BOX. DAMAGE FROM CONTACT WITH FLAP FAIRING. CORRECTIVE ACTION: REPAIRED IAW MHIRJ REO 670-57-21-990 REV-- DATED 2024-09-10 CC670-10046/10045Dec 24, 2024 · N703PS · Cndair CL6002C10SDR SWIA202504301223Vane · gougedRH WING I/B FLAP FOUR FLAP VANE ACTUATOR ROLLER TRACKS (4EA) MULTIPLE AREA GOUGES, DAMAGED AS MARKED (C-CHECK RO 04/30/2025)R/H WING, INBD FLAP VANE ACTUATORS WITHIN LIMITS (4 EA) IAW MHIRJ REO 670-57-52-598 DATED: 2025-03-03. REWORKED AREAS REFINISHED PER SAMDec 23, 2024 · N765SK · Cndair CL6002C10SDR CALA2024123003189Skin · damagedRIGHT WING INBOARD TRAILING EDGE FLAP HAS IMPACT DAMAGE FROM THROWN TREAD OF NO.7 MLG TIRE. C/W RII INSP. OF R/H WING TE I/B FLAP ATTACH POINTS AND HARDWARE CW RII FOR OK TO INSTALL ALL ATTACH POINTS NO OBVIOUS DEFECTS NOTED AT THIS TIME. NEW ATTACH HARWARE ORDec 23, 2024 · N76064 · Boeing 767424ERSDR DALA2024122411969Housing · corrodedSHIP 3145 CORROSION WAS FOUND IN TRACK 2 SUPPORT BEARING HOUSING AT RIB 9 LEVEL. CORRECTIVE ACTION: REPAIRED PER ER/A 622551-14. (0725784)Dec 23, 2024 · N345NB · Airbus A319114SDR AALA202502036018Bracket · corrodedAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ON BEARING AFT ATTACH FITTING INB FLAP LH WING (DURING INSPECTION WAS FOUND CORROSION) L=0.586 INCH W=0.167 INCH D=0.001 INCH. MAINTENANCE REPLACED BRACKET ASSY LOC INB FLAP BTW RIB 14 AND WX4476.559 LH WING IAW A3Dec 21, 2024 · N122US · Airbus A320214SDR AALA202502032715Bracket · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ON BEARING AFT ATTACH FITTING INB FLAP RH WING. MAINTENANCE REPLACED BRACKET ASSY LOC. INB FLAP BTW RIB 14 AND WX4476.559 RHWING, I.A.W A320 SRM 51-42-11-801 AND A320 SRM 51-72-11-911-001 AND DWG D57570280. FORM Dec 21, 2024 · N122US · Airbus A320214SDR AALA202501091118Skin · delaminatedAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND OUTBOARD AFT FLAP IS DELAMINATED AT LOWER INBOARD END. REMOVED AND INSTALLED SERVICEABLE RIGHT HAND OUTBOARD AFT FLAP, PER B737NG AMM 27-51-22. PERFORMED SATISFACTORY RIGHT HAND OUTBOARD AFT FLAP RIG AND ADJUSTMENT ANDec 21, 2024 · N981NN · Boeing 737823SDR AALA202501071118Skin · delaminatedAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND OUTBOARD AFT FLAP IS DELAMINATED AT LOWER INBOARD END. **SUPPLEMENTAL REPORT WILL BE SUBMITTED**(OPEN).Dec 21, 2024 · N981NN · Boeing 737823SDR SWAA2024123180161Fairing · pulled#4 FLAP CANOE FAIRING AS NUMEROUS PULLED THROUGH RIVETS<[01] R&R'D #4 FLAP CANOE FAIRING TAIL CONE IAW AMM 27-51-18;[02] VERIFIED THE FOLLOWING:<BR>R&R'D #4 FLAP CANOE FAIRING TAIL CONE IAW AMM 27-51-18Dec 21, 2024 · N8301J · Boeing 7378H4SDR SWAA2024122379712Flap · delaminatedRT WING I/B MAIN FLAP WEDGE LOWER SKIN DELAMINATED STARTING FROM 2.4 IN. FROM O/B EDGE. MEASURES APPROX. 7.6 IN. LENGTH; 4.2 IN. WIDTH.<[01] PERFORMED TEMPORARY REPAIR ON RH MAIN INBOARD FLAP TRAILING EDGE REF SRM 57-53-01-1A-1 SECTION 4. A (7) ZONE 3 LOWER SKDec 20, 2024 · N7821L · Boeing 7377CTSDR SWAA2025012879155Fairing · delaminated#1 CANOE FAIRING PANEL544BB DELAMINATED AREA ON OUTERM SKIN I/B SIDE 12.5' FROM FWD. END AND 4.4' FROM UPPER END.<[01] RECIEVED NEW FAIRING; INSTALLATION OF FAIRING TO BE ACCOMPLISHED ON FAULT TTG8Q00X5HUNDec 19, 2024 · N8606C · Boeing 7378H4SDR SWAA2025010879484Skin · delaminatedR/H WING O/B AFT FLAP DELAMINATED AT THE I/B AFT CORNER.<[01] ACCOMPLISHED TASK CARD R/H WING O/B AFT FLAP DELAMINATED AT THE I/B AFT CORNER. [TTG8Q00XQKUQ].<BR>B737-800 AMM 27-51-22;[02] VERIFIED ACCOMPLISHED TASK CARD R/H WING O/B AFT FLAP DELAMINATED AT THEDec 19, 2024 · N8659D · Boeing 7378H4SDR WRXR20241219002Skin · gougedLH WS54.55 FLAP SKIN GOUGED DUE TO AFT HINGE FAIRING SEAL. REMOVED AND REPLACED 48 (EA) DAMAGED FASTENERS AFTER BLENDING WAS PERFORMED ON L/H WS54.55 LOWER FLAP SKIN IAW REO 670-57-52-585. RESTORED FINISH OF THE REWORKED AREAS ON L/H WS54.55 LOWER FLAP SKIN IADec 19, 2024 · N540EG · Cndair CL6002C10SDR DALA2024121911827Bearing · wornWORN BEARING OF FLAP AND ELONGATED HOLES ON OUTB HINGE OF LH FLAP WERE FOUND. SUMMARY OF NRC 00684: OUTB HINGE OF LH FLAP WAS REPAIRED PER ER/A 622136-14 REV ORIG, SECTION I: PERMANENT REPAIR. "DTE" TIME CONTROLLED ITEM WITH LOG PAGE #0701683. ASSOCIATED ER/A Dec 19, 2024 · N978AT · Boeing 717200SDR SWIA202502261218Guide Fitting · gougedLEFT OUTBOARD FLAP, INBOARD GUIDE FITTING GOUGED. (C-CHECK RO 2/25/2025) PERFORMED REPAIR AREA ON LH OB FLAP IB GUIDE FITTING IAW REO 670-57-51-587 REV-- DATE 2025-01-17, CRJ700 SRM 51-24-11, 53-00-00, 51-12-00.Dec 18, 2024 · N750EV · Cndair CL6002C10SDR CALA2025011500121Doubler · corrodedLH WING O/B FLAP INTERNAL DOUBLER AT RIB 5 HAS CORROSION AROUND 2 FASTENERS. R & R LT WING O/B FLAP IAW A319 AMM 27-54-62-400-001-A 27-54-62-000-001-A RIG AND OPS GOOD.Dec 18, 2024 · N829UA · Airbus A319131SDR CALA2025011300094Doubler · corrodedRH WING I/B FLAP INTERNAL DOUBLER AT L/E RIBS 9 AND 10 HAS CORROSION AROUND FEW FASTENERS. REMOVED AND REPLACED RW IB FLAP IAW A319 AMM 27-54-01-000-001-A, 27-54-61-400-001-A. OPS CHECK GOOD.Dec 18, 2024 · N829UA · Airbus A319131SDR CALA2025011300095Doubler · corrodedRH WING O/B FLAP INTERNAL DOUBLER AT RIBS 5 AND 6 HAS CORROSION AROUND SEVERAL FASTENERS PER HAECO LCQ N/R 9296639/20639. REMOVED AND REPLACED R/W O/B FLAP IAW AMM 319 27-54-62-000-001-A AND 27-54-62-400-001-A(RIG LOPS CHECK GOOD).Dec 18, 2024 · N829UA · Airbus A319131SDR CALA2024122001588Repair · missingPDA 2 - PREVIOUS REPAIR ON LEFT WING INBOARD FLAP LOWER SURFACE MEASURING APPROX. 7 1/4 X 6 3/4 IS MISSING REF LOG 3217434 FOR CORRECTIVE ACTION OF MISSING REPAIR. LEFT WING INBOARD FLAP LOWER SURFACE PREVIOUS REPAIR IS MISSING. CLEANED AREA AND APPLIED 2 LAYDec 17, 2024 · N35236 · Boeing 737824SDR SWAA2024122777915Skin · delaminatedL/H WING O/B AFT FLAP DELAMINATED AT THE I/B AFT CORNER AT LOWER SKIN. MARKED<[01] 01 - REMOVED AND REPLACED PER [AMM 27-51-22-400-801-NG (OUTBOARD AFT FLAP INSTALLATION - PERMANENT)];[02] VERIFIED 01 - REMOVED AND REPLACED PER [AMM 27-51-22-400-801-NG (OUTBOADec 16, 2024 · N8674B · Boeing 7378H4SDR WRXR20241213005Skin · chafedRH WS128.00 FLAP SKIN HAS GOUGING DUE TO AFT FAIRING 686BB SEAL. BLENDED GOUGES COMMON TO FAIRING 686BB RH WS128.00 FLAP SKIN IAW CRJ 700 SRM 51-12-00-001-001-A01. PERFORMED REPAIR ON RH WS128.00 FLAP SKIN GOUGING COMMON TO FAIRING 686BB IAW REO 670-57-52-584Dec 13, 2024 · N540EG · Cndair CL6002C10SDR SWAA2025012376792Skin · debondedCUSTOMER REQUEST - DEBONDED OB AFT FLAP ON IB SIDE AT RT WING 2024-764357<[01] TOOL USED CALIPER: PN: 500-196-30; SN: A23325649; DUE DATE: 31-DEC-24;[02] TOOL USED: BOND TESTING UNIT; P N: BONDMASTER 600M; S N: 230106912; CAL DUE DATE: 09-JAN-25;[03] TOOL USEDDec 12, 2024 · N8610A · Boeing 7378H4SDR SWAA2025012376793Skin · debondedCUSTOMER REQUEST - DEBONDED OB AFT FLAP ON IB SIDE AT LT WING 2024-764363<[01] TOOL USED CALIPER PN: 500-196-30; SN: A23325649; DUE DATE: 31-DEC-24;[02] TOOL USED: BOND TESTING UNIT; P N: BONDMASTER 600M; S N: 230106912; CAL DUE DATE: 09-JAN-25;[03] TOOL USED:Dec 12, 2024 · N8610A · Boeing 7378H4SDR AALA202412278012Skin · delaminatedAIRCRAFT IN BASE MAINTENANCE: LEFT WING INBOARD MAIN FLAP AFT OUTBOARD TRAILING EDGE WEDGE LOWER SURFACE DELAMINATED. MAINTENANCE REPAIRED LEFT WING INBOARD MAIN FLAP AFT OUTBOARD TRAILING EDGE WEDGE LOWER SURFACE PER SRM 57-53-01-2R-7 AND SRM 51-70-10-2R-4.Dec 12, 2024 · N820NN · Boeing 737823SDR SWAA2024121676600Skin · pulledDURING WALK AROUND FOUND PULLED FASTENERS ON RT MAIN FLAP<[01] REMOVED RIGHT WING INBOARD TRAILING EDGE MAIN FLAP PER AMM. 27-51-11.;[02] REMOVED AND REPLACED PER [AMM 27-51-11-401-NG (INBOARD TRAILING EDGE FLAP - REMOVAL/INSTALLATION - PERMANENT)];[03] REMOVEDec 12, 2024 · N234WN · Boeing 7377H4SDR DALA2024121311706Bearing · corrodedSHIP 3145 CORROSION ON SPHERICAL BEARING I/B FLAP TRACK 2 ON RH WING. CORRECTIVE ACTION: REPLACED SPHERICAL BEARING I/B FLAP TRACK 2 RH WING AS PER A320 FAM AMM 57-52-21-000-001-A AND AMM 57-52-21-400-001-A. (0707359)Dec 12, 2024 · N345NB · Airbus A319114SDR DALA2024121611738Hinge Fitting · corrodedCORROSION ON ALL INNER CAVITY LUGS (9 EA) OF THE INBOARD WING FLAP HINGE FITTING AT LH WING, AND WEAR ON FAIRING SUPPORTS OF THE INBOARD WING FLAP HINGE FITTING AT LH WING. ALSO WEAR ON INNER CAVITY (4 EA) SUPPORT AT LH WING. CORROSION ON ACTUATOR SUPPORT LUGSDec 11, 2024 · N981AT · Boeing 717200SDR ASAA2024121055135Skin · delaminatedL/H OUTBOARD AFT FLAP LOWER SKIN HAS A 10"X12" AREA OF DISBOND LOCATED AT INBOARD CORNER. GROUNDED - YES. REMOVED 10"X12" AREA OF DAMAGED SKIN LH OUTBD AFT FLAP LWR SKIN & REPAIRED IAW B737-900ER SRM 57-53-01-2R-16 & B737-900ER SRM 51-70-10-2R-0. RESTORED FINIDec 10, 2024 · N236AK · Boeing 737990ERSDR SWAA2025012875267Flap · debondedCUSTOMER REQUEST - DEBONDED EXTERNAL SKIN OB AFT FLAP LOWER SURFACE AT LT WING 2024-758672<[01] TOOL USED CALIPER PN: 500-196-30; SN: A23325649; DUE DATE: 31/DEC/24.;[02] TOOL USED ON ITEM 3: ULTRASONIC FLAW DETECTOR; P/N: EPOCH 600; S/N: 120357005; DUE DATE: Dec 9, 2024 · N279WN · Boeing 7377H4SDR SWAA2025011575290Skin · debondedCUSTOMER REQUEST - DEBONDED IB MAIN FLAP WEDGE PANEL LOWER SURFACE AT LT WING 2024-759336<[01] TOOL USED CALIPER PN: 500-196-30; SN: A23325649; DUE DATE: 31/DEC/24.;[02] TOOL USED CALIPER PN: 500-197-30; SN: A189508; DUE DATE: 14/JAN/25.;[03] CORRECTIVE ACTIONDec 9, 2024 · N7713A · Boeing 7377BDSDR SWAA2025011575292Skin · debondedCUSTOMER REQUEST - DEBONDED IB MAIN FLAP WEDGE PANEL LOWER SURFACE AT RT WING. TOOL USED: POSITECTOR PN: NS2; SN: 110098; DUE DATE: 05/SEP/25.<BR>TOOL USED: HOT BONDER PN: HCS9200B-AV; SN: 18185733; DUE DATE: 25/JAN/25.;[02] TOOL USED ON STEP 11 ULTRASONIC FLDec 9, 2024 · N7713A · Boeing 7377BD
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