JASC 5753

Service difficulty reports · 31,515

Reports filed under 5753 · Trailing Edge Flaps, newest first.

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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"

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SDR AWXA200601396Wedge · debondedMCN - FOUND LT T/E INBD MIDFLAP WEDGE IS DISBONDED AT DENT MARK PNL 7220. MAINTENANCE REPAIRED DISBONDED DENT ON LT T/E MIDFLAP WEDGE IAW B737-300 SRM 51 - 70 - 10 - 2RY FIG 201.Jul 12, 2006 · N305AW · Boeing 7373G7SDR CALA0600274Flap Track · corrodedINSPECTION FOUND NR 2 FLAP TRACK TRANSMISSION ATTACH HOLES AT AFT UPPER AND LOWER FORWARD LOCATION, RSS 330, CORRODED. A O/S REPAIR SLEEVE WAS INSTALLED IAW SOPM 20-50-03 AND CMM 57-53-15.Jul 12, 2006 · N17345 · Boeing 7373T0SDR CALA0600273Flap Track · corrodedINSPECTION FOUND NR 7 FLAP TRACK TRANSMISSION MOUNT HOLES AT BOTH AFT AND FORWARD LOWER POSITIONS, RSS 330, CORRODED. THE CORROSION WAS REMOVED AND REPAIR SLEEVES WERE INSTALLED IAW SOPM 20-50-03 AND CMM 57-53-15.Jul 12, 2006 · N17345 · Boeing 7373T0SDR UPS06247385Carriage · corrodedINSPECTION TYPE-C, 3 SEQUENCE CARRIAGE HAS CORROSION ON AFT UPPER LUGS SEQUENCE CARRIAGE REPLACED IAW MM 27-51-04.Jul 12, 2006 · N935UP · Boeing 7271A7CSDR SWAA062412Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP LOWER INBOARD CORNER DELAMINATED. REMOVED AND REPLACED FLAP PER MM.Jul 12, 2006 · N696SW · Boeing 7373T5SDR CALA0600244Flap Track · corrodedINSPECTION FOUND THE NR 8 FLAP TRACK TRANSMISSION MOUNT HOLE CORRODED AT LOWER AFT POSITION. THE CORROSION WAS REMOVED. SLEEVES WERE FABRICATED AND THE BORES AND SLEEVES WERE CAD-PLATED AND INSTALLED USING NEW BUSHINGS IAW OHM 57-53-15.Jul 12, 2006 · N17345 · Boeing 7373T0SDR 06FDEA02527Skin · damagedRT WING I/B FLAP LOWER SURFACE FOUND 01 EA EXISTING REPAIR AT I/B SIDE OF O/B HINGE (FLAP MOUNTED). EXISTING REPAIR AT RT WING I/B FLAP LOWER SURFACE AT I/B SIDE OF O/B HINGE EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED PER DELTA ENG'G REPAIR/AUTHORIZATION 268Jul 11, 2006 · N521FE · Doug MD11SDR 06FDEA02512Fairing · damagedEXISTING DOUBLER REPAIR AT RT WING INBD FLAP INBD FILLET FAIRING (ER/A401695-14) SNRM N00315: EXISTING DOUBLER REPAIR AT RT WING INBD FLAP INBD FILLET FAIRING EVALUATED AND FOUND REPAIR PREVIOUSLY ACCOMPLISHED PER DELTA ENG'G REPAIR/AUTHORIZATION 401695-14, EOJul 11, 2006 · N521FE · Doug MD11SDR 06FDEA02511Flap · damagedEXISTING REPAIR FOUND AT RT WING INBD FLAP OUTBD CLOSEOUT WEB (ER/A377084-14) SNRM N00314: EXISTING REPAIR FOUND AT RT WING INBD FLAP OUTB CLOSEOUT WEB EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED PER DELTA ENG'G REPAIR/AUTHORIZATION 377084-14, EO1- 5100-7-500Jul 11, 2006 · N521FE · Doug MD11SDR 06FDEA02509Skin · damagedEXISTING DOUBLER REPAIR FOUND AT RT WING INBD FLAP UPPER SKIN (ER/A363238-14). EXISTING DOUBLER REPAIR AT RT WING INBD FLAP UPPER SKIN EVALUATED AND FOUND PERMANENT REPAIR PREVIOUSLY ACCOMPLISHED PER DELTA ENGINEERING REPAIR/AUTHORIZATION 363238-14 REV A EO 1Jul 11, 2006 · N521FE · Doug MD11SDR 06FDEA02508Skin · damagedEXISTING REPAIR FOUND AT RT INBD FLAP LOWER SURFACE(ER/A268996-14). EXISTING REPAIR AT RT INBD FLAP LOWER SURFACE EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED PER DELTA ENGINEERING REPAIR/AUTHORIZATION 268996-14. EO 1-5100-7-5001A-PT1, TITLE: "REPAIR CATALOGJul 11, 2006 · N521FE · Doug MD11SDR UPS06247433Flap Track · corrodedINSPECTION TYPE:C CORROSION IN \1 FLAP TRACK HOLES E, D AND C. BUSHING FABRICATED IAW AAAE EO 2006-042-005. HEAT TREATMENT REFERENCE 06-42-03. CAD PLATED IAW SOPM 20-42-10. INSTALLED IAW SOPM 20-50-03.Jul 11, 2006 · N935UP · Boeing 7271A7CSDR UPS06247429Flap Track · corrodedINSPECTION TYPE:C CORROSION IN NR 6 FLAP TRACK HOLES G AND F. BUSHINGS FABRICATED IAW AAAE-EO-2006-042-08. HEAT TREATED IAW 06-42-03. CAD PLATED IAW SOPM 20-42-10. INSTALLED IAW SOPM 20-50-03.Jul 11, 2006 · N935UP · Boeing 7271A7CSDR UPS06247432Attach Fitting · corrodedINSPECTION TYPE:C CORROSION ON NR 7 FLAP TRACK ATTACH PAD HOLE E. BUSHING FABRICATED IAW EO 2006-042-0009. HEAT TREATMENT REFERENCE 06-4 2-03. CAD PLATED IAW SOPM 20-42-10. INSTALLED IAW SOPM 20-50-03.Jul 10, 2006 · N935UP · Boeing 7271A7CSDR UPS06247431Attach Fitting · corrodedINSPECTION TYPE:C NR 8 FLAP TRACK ATTACH PAD HAS CORROSION IN HOLES E, D AND C. BUSHINGS FABRICATED FOR HOLES IAW AAAE EO 2006-042-10. HEAT TREATMENT REFERENCE 06-42-03. CAD PLATED IAW SOPM 20-42-10. INSTALLED IAW SOPM 20-50-03.Jul 10, 2006 · N935UP · Boeing 7271A7CSDR 06FDEA2496Flap Track · corrodedFOUND CORROSION ON NUMBER 3 FLAP TRACK AFT MOUNTING SURFACE. REMOVED AND REPLACED #3 FLAP TRACK IAW FED EX WORK CARD 27X5705-03Jul 10, 2006 · N281FE · Boeing 727233SDR 06FDEA2497Skin · crackedFOUND LEFT WING T/E I/B MIDFLAP, CRACKED AT CUTOUT FOR INBOARD PUSHROD IN AFT CHORD. REPAIRED CRACK ON LEFT WING T/E IB MIDFLAP IAW SRM 51-30-2, 51-40-4 FIG 1Jul 10, 2006 · N281FE · Boeing 727233SDR ARWA20060704Hinge Fitting · crackedDURING DAILY CHECK INSPECTION THE FOLLOWING WAS FOUND; LT OUTBOARD WING FLAP STATION XW 219, LT HINGE BASE FITTING CRACK. REMOVED LEFT O/B WING FLAP ASSEMBLY IN ACCORDANCE WITH M/M 27-51-2. INSTALLED LT OUTBOARD WING FLAP ASSY IN ACCORDANCE WITH M/M 27-51-2.Jul 8, 2006 · N906R · Doug DC863FSDR CA060801008Torque Tube · chafed(CAN) DURING A LINE MAINTENANCE WALK-AROUND CHECK, AN ENGINEER FOUND THAT THE LT WING FLAP IB (SECTION BETWEEN NACELLE AND FUSELAGE) TORQUE TUBE HAS BEEN CHAFED THROUGH IN ONE SPOT BY ITS RETAINING BRACKET. TORQUE TUBE ASSY PN REPLACED WITH SERVICEABLE ASSY FUJul 8, 2006 · Dhav DHC8101SDR SWAA062370Skin · delaminatedDURING SCHEDULED MV2 CHECK, FOUND RT WING INBOARD AFT FLAP DELAMINATED AT T/E OUTBOARD SIDE. REMOVED AND REPLACED RT INBOARD AFT FLAP PER MM.Jul 8, 2006 · N521SW · Boeing 7375H4SDR SWAA062369Skin · delaminatedDURING SCHEDULED SERVICE CHECK, FOUND LEFT WING OUTBOARD T/E FLAP DELAMINATED INBOARD SIDE. REMOVED AND REPLACED LEFT OUTBOARD FLAP PER MM.Jul 8, 2006 · N506SW · Boeing 7375H4SDR SWAA062362Skin · delaminatedDURING SCHEDULED MV1 CHECK, FOUND RT WING INBOARD T/E AFT FLAP DELAMINATED AT OUTBOARD SIDE. REMOVED AND REPLACED INBOARD FLAP PER MM.Jul 8, 2006 · N698SW · Boeing 737317SDR UPS06447535Support · corrodedINSPECTION TYPE:C RHW I/B T/E AFT FLAP INTERNAL REAR SUPPORT CHANNEL AT WBL135 FOUND CORROSION DAMAGED. CORROSION BLEND OUT 0.080" BY 1/2" BY 1/2" EXCEED SRM LIMIT. RHW I/B T/E AFT FLAP INTERNAL REAR SUPPORT CHANNEL AT WBL130-141 AREA REPAIRED AS PER SRM 51-Jul 7, 2006 · N676UP · Boeing 747123FSDR UPS06447472Support · corrodedRHW I/B T/E AFT FLAP INTERNAL REAR SUPPORT DAMAGED AT WBL 440 FOUND CORROSION DAMAGED. CORROSION BLEND OUT 0.080" BY 1/2" BY 1" EXCEED SRM 57-50-01 FIG 3 LIMITS, RHW I/B T/E AFT FLAP INTERNAL REAR SUPPORT AT WBL 423 TO 442. REPAIRED AS PER SRM 51-40-04 FIG 1Jul 7, 2006 · N676UP · Boeing 747123FSDR IXXA06SMN216SSkin Panel · delaminatedDURING ROUTINE C CHECK INSPECTION, LT WING INBD FLAP PANEL UPPER SKIN DELAMINATED AND HOLES ELONGATED, XW 2.000.Jul 7, 2006 · N41CX · Doug DC8*SDR 06FDEA2471Carriage · gougedFOUND RT WING I/B AFT FLAP, I/B CARRIAGE GOUGED. REPAIR ACCOMPLISHED PER FED EX EA 7-5710-100554.Jul 7, 2006 · N281FE · Boeing 727233SDR QXEA200602288Skin · damagedYYC: LT WING OUTBOARD TRAILING EDGE FLAP TOP SKIN REQUIRES PAINT STRIP IN AREA LOCATED 24 INCHES FROM INBOARD END FOR FURTHER INSPECTION. MAINTENANCE REPAIRED IAW Q400 SRM 51-26-10-150-801, SRSM 57-52-30-320-801, SRM 57-52-30-992-801, SRM 51-21-10-380-801 ANDJul 6, 2006 · N424QX · Bombdr DHC8402SDR SWAA062327Skin · delaminatedDURING SCHEDULED C1 CHECK, FOUND RT WING INBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.Jul 6, 2006 · N678AA · Boeing 7373A4SDR ASAA0680726Vane · gougedRT WING OUTBOARD FLAP INBOARD VANE GOUGED ON LEADING EDGE. REMOVED DAMAGED AREA. INSTALLED FILLER AND DOUBLER PER SRM 51-70-2.Jul 6, 2006 · N972AS · Doug DC983SDR USAA060879Skin · delaminatedTEN INCHES FROM INBOARD END OF LEFT WING TRAILING EDGE, OUTBOARD FOREFLAP DELAMINATION. DEFECTIVE PART REPLACED WITH IDENTICAL PART, REPLACED FOREFLAP IAW SRM 27-51-37, DEFECT SIZE: 2 X 12 INCHES.Jul 5, 2006 · N434US · Boeing 7374B7SDR EIA2006091Fairing · damagedDURING PREFLIGHT INSPECTION, FOUND HOLE IN INBOARD FLAP FAIRING. DAMAGE APPROX 3 IN OF DAMAGE PENETRATING HONEYCOMB, PARTS AVAILABLE TO REPAIR. NR 6 FLAP CANOE FAIRING REMOVED FOR REPAIR PER CDL 27-51-2 AND MM 27-51-00.Jul 3, 2006 · N487EV · Boeing 747212BSDR 06FDEA2443Hinge Fitting · corrodedFOUND RIGHT WING OUTBOARD FLAP OUTBOARD HINGE FITTING FORWARD OUTBOARD MATING SURFACE MIDDLE HOLE WITH CORROSION. REPAIR CARRIED OUT AS PER FEDEX E.A. #1- 5750-100672,Jul 2, 2006 · N603FE · Doug MD11SDR 06FDEA2442Hinge Fitting · corrodedFOUND RIGHT WING OUTBOARD FLAP INBOARD HINGE FITTING FOUND AFT MATING SURFACE AFT HOLE WITH CORROSION. REPAIR CARRIED OUT AS PER FEDEX E.A. #1-5750-100671Jul 2, 2006 · N603FE · Doug MD11SDR 06FDEA2441Fairing · corrodedFOUND LEFT WING OUTBOARD AFT HINGE FAIRING, AFT MATING SURFACE AFT HOLE FOUND WITH CORROSION. CORROSION REPAIR CARRIED OUT AS PER FEDEX E.A. 1-5750-100670.Jul 2, 2006 · N603FE · Doug MD11SDR 06FDEA2440Fairing · corrodedFOUND LEFT WING OUTBOARD FLAP INBOARD AFT HINGE FAIRING, FORWARD MATING SURFACE OUTBOARD MIDDLE HOLE FOUND WITH CORROSION. REPAIR CARRIED OUT AS PER FEDEX E.A. #1-5750-100669, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Jul 2, 2006 · N603FE · Doug MD11FSDR IXXA06SMN207SSkin Panel · damagedDURING ROUTINE C CHECK INSPECTION, LT WING INBD FLAP PANEL UPPER SKIN HOLES ELONGATED, XW 40.000.Jun 30, 2006 · N41CX · Doug DC862FSDR IXXA06SMN206SSkin Panel · dentedDURING ROUTINE C CHECK INSPECTION, LT WING INBD FLAP PANEL UPPER SKIN DENTED, XW 45.000.Jun 30, 2006 · N41CX · Doug DC862FSDR THMN4165SQ117Skin · crackedFLAP LT IB LWR SKIN CRACKED. MADE AIRWORTHY REPAIR IAW PA-39 SERVICE MANUAL, CHAPTER 4 PG 1F6 AND AC 43.13-1B SECTION 4 PARAGRAPH 4-57 FIGURE 4-6 AND SECTION 4 PARAGRAPH 4-58 FIGURE 4-16.Jun 30, 2006 · N320GC · Piper PA39SDR AWXA200601207Skin · puncturedMCN - PUNCTURE IN LOWER SURFACE OF RT INBOARD FOREFLAP, 14.25" FROM INBOARD END. RT I/B FOREFLAP PUNCTURE REPAIRED IAW B 737-300 SRM AWA TASK CARD NR R3M27008. NOTE PUNCTURE LOCATED 14.25" FROM I/B END LOWER SURFACE.Jun 29, 2006 · N303AW · Boeing 7373G7SDR DHL2006762509Skin · delaminatedLT WING, INBD FLAP TE IS DELAMINATED ON OUTBD TE WBL 243. REMOVED PREVIOUS REPAIR AND VACUUM BAGGED FOR MOISTURE REMOVAL. FABRICATED REPAIR SKIN APPROX 6 1/2" BY 4 AND EXTERNAL DOUBLER APPROX 3" BY 4" FROM 7075T6 .016 PO NR 9003142. CLEANED, PREPPED, APPLIEJun 29, 2006 · N762AT · Boeing 7272B7SDR DHL2006762506Skin · wornLT WING INBD FLAP, FORE FLAP L/E HAS WEAR SPOT ON SKIN WBL 114. REMOVED DAMAGED DOUBLER L/WING I/B FORE FLAP L/E WBL 114 AS PER B727 SRM 51-30-2. FABRICATED NEW DOUBLER 7" BY 8" 2024T3 .063 PO NR 9003310 AS PER B727 SRM 57-50-4 FIG 1. TREATED AND PRIMED DOUJun 29, 2006 · N762AT · Boeing 7272B7SDR DHL2006762504Skin · delaminatedRIGHT O/B MID FLAP WBL 348-358 HAS UPPER T/E DELAMINATED. CUT OUT DELAMINATED AREA R/W O/B MID FLAP UPPER SKIN APPROX 3.25 X 22 INCHES IAW SRM 51-40-20 PARA 6 & 7. FABBED ONE SKIN REPLACEMENT APPROX .75 X 22 INCHES AND ONE SPLICE PLATE 3 X 3.25 INCHES USING Jun 29, 2006 · N762AT · Boeing 7272B7SDR 06FDEA2429Skin · dentedSNRM N00367: LEFT HAND WING INBOARD FLAPS OUTBOARD SEGMENT LOWER SURFACE FOUND WITH 3EA DENTS. REPAIRED AS PER SRM 57-10-00 FIGURE 2 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2- 100.Jun 29, 2006 · N603FE · Doug MD11SDR 06FDEA2428Skin · dentedSNRM N00143: LEFT HAND WING INBOARD FLAPS LOWER SURFACE FOUND WITH SEVERAL DENTS. DENTS FOUND OUT OF LIMIT AS PER SRM 57-10-00 FIGURE 17 VOLUME I. DENT AREAS TRIMMED OFF AND REPAIR IS CARRIED OUT ON TRIMMED OFF AREAS AS PER SRM 57-10-00 FIGURE 3 VOLUMEJun 29, 2006 · N603FE · Doug MD11SDR 06FDEA2425Structure · dentedRIGHT HAND WING INBOARD FLAP INBOARD SEGMENT FOUND WITH SEVERAL DENTS. DENTS ON RIGHT HAND WING INBOARD FLAP INBOARD SEGMENT REPAIRED AS PER SRM 57 -10-00 FIGURE 3 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Jun 28, 2006 · N603FE · Doug MD11SDR 06FDEA2416Flap Track · corrodedN00269 RIGHT WING NUMBER 6 FLAP TRACK CORRODED AT AFT ATTACH POINT. REPLACED R/W #6 FLAP TRACK WITH SERVICABLE TRACK, PER WORK CARD 27X5708-03.Jun 28, 2006 · N281FE · Boeing 727200SDR UIEA200600146Skin · crackedLEFT TRAILING EDGE I/B MID FLAP HAS PREVIOUS REPAIR THAT HAS CRACKED ON I/B END 6 INCHES FROM EDGE. DAMAGE REMOVED & REPAIR LAYED UP 7 CURED IAW B747-400F SRM 51-70-06 REPAIR 5A (1), PARA 4 A, C, E (1) (D) PG 13 REVISION 43.Jun 28, 2006 · N409 · Boeing 74747UFSDR DHL2006762520Angle · crackedRIGHT INBD MID FLAP REAR LWR CHORD ANGLE CRACKED WBL 105. REMOVED SEAL RETAINER AND LWR CHORD ANGLE SECTION AND LOWER SKIN IAW B727 SRM 51-30-2. FAB NEW LOWER CHORD AT RIGHT INBD MID FLAP WBL 105 FROM P/N BAC1517-1367 PO NR 501953 IAW B727 SRM 51-50-2 FIG 5 Jun 27, 2006 · N762AT · Boeing 7272B7SDR DHL2006762519Angle · crackedLEFT INBD MID FLAP REAR LWR CHORD ANGLE SHOWS CRACK WBL 220. REMOVED MID FLAP LOWER SKIN FOR ACCESS IAW B727 SRM 51-30-2. REMOVED LEFT INBD MID FLAP LWR CHORD IAW B727 SRM 51-30-2. FABRICATED NEW MID FLAP LWR CHORD ANGLE FROM P/N BAC1503-100046 PO NR 627846Jun 27, 2006 · N762 · Boeing 7272B7SDR DHL2006762518Angle · crackedLEFT INBD MID FLAP REAR LWR CHORD ANGLE SHOW CRACKS 2 WBL 105. REMOVED MID FLAP LOWER SKIN FOR ACCESS IAW B727 SRM 51-30-2. REMOVED LEFT INBD MID FLAP LWR CHORD IAW B727 SRM 51-30-2. FAB NEW MID FLAP LWR CHORD ANLGE FROM P/N BAC1503-100046 PO NR 627846 APPRJun 27, 2006 · N762AT · Boeing 7272B7
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