JASC 5753
Service difficulty reports · 31,515
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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR UIEA200600036Structure · crackedRT WING OUTBOARD T/E MID-FLAP HAS A CRACK IN COMPOSITE STRUCTURE APPROX 25 INCHES LONG. REPAIRED IAW SRM 51-40-12 PARA 4D AND FIG 11.SDR UIEA200600033Skin · delaminatedLT WING OUTBOARD T/E FORE-FLAP HAS DELAMINATION BETWEEN NR 1 AND NR 2 TRACKS. REPAIRED IAW SRM 51-40-15 PARA 4N.SDR UIEA200600032Skin · delaminatedLT WING INBOARD T/E FORE-FLAP HAS DELAMINATION ON LOWER SIDE OF L/E BETWEEN NR 3 AND NR 4 TRACKS. REPAIRED IAW SRM 51-40-12 PARA 4C AND 51-40-14 PARA 4D.SDR UIEA200600031Skin · delaminatedLT WING INBOARD T/E MID-FLAP HAS DELAMINATION BETWEEN FLAP TRACKS NR 3 AND NR 4. REPAIRED IAW OHM 57-52-35 BY REPLACEMENT OF MID-FLAP LEADING EDGE SECTION BETWEEN NR 3 AND NR 4 TRACKS.SDR UIEA200600030Skin · delaminatedRT WING INBOARD T/E MIDFLAP HAS A LARGE SPOT OF DELAMINATION. REPAIRED IAW SRM 51-40-14 FIG 9.SDR UIEA200600029Skin · delaminatedRT WING INBOARD AFT T/E FLAP HAS DELAMINATION APPROX 15 INCHES. FLAP REPAIRED IAW SRM 51-40-14 REPAIR 4D.SDR SWAA060809Skin · delaminatedDURING SCHEDULED 10Y CHECK, FOUND LEFT WING INBOARD T/E FOREFLAP DELAMINATED AT UPPER SURFACE. REPAIRED FOREFLAP PER SRM.SDR DHL2006750506Support Bracket · crackedNR 1 LE FLAP ACTUATOR TRUNNION SUPPORT BRACKET IS CRACKED OUTBOARD END. CONFIRMED CRACK. REMOVED SUPPORT BRACKET AT NR 1 L/E FLAP ACTUATOR TRUNNION OUTBOARD END FABBED NEW SUPPORT BRACKET FROM 7075 T6 .040 PO 9002590 DIM 8 1/8 BY 3 3/4 AND TREATED PRIMED ANDSDR 06FDEA1008Skin · dentedLEFT INBOARD TRAILING EDGE FLAP LOWER SURFACE FOUND WITH DENTS AT OUTBOARD MID AREA. REPAIRED AS PER SRM 57-10-00 VOLUME I, FIGURE 2. CLASSIFIED AS MAJOR REPAIR PER GMM 6-2-100.SDR 2006UALA00732Skin · damagedRIGHT HAND TRAILING EDGE MAIN INBD FLAP HAS PREVIOUS REPAIR COMING OFF TOP SIDE OF FLAP ACCOMPLISHED INTERIM REPAIR PER EVA UA-EVA-60124 WITH NEW PATCH RIVETED AND COVERED WITH SPEED TAPE ON TOP OF INBD MIDFLAP. MUST INSPECT EVERY 3SV. PERMANENT REPAIR MUST SDR SWAA060797Skin · delaminatedDURING SCHEDULED C2 CHECK, FOUND RT WING INBOARD T/E FORE FLAP DELAMINATED AT UPPER SURFACE. REMOVED AND REPLACED FLAP ASSY PER MM.SDR IXXA06SMN096SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, RIGHT WING OUTBOARD. FLAP LOWER AFT SKIN NON STANDARD REPAIR, AT STATION XF 350.000. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-7-1 FIG 4 TR NR 57-94 DATE 10-01-02. REMOVED DAMAGED PANEL PLATING IAW DC8 SRM 57-1-0, DC8 SRM 51-1-SDR IXXA06SMN077SStructure · dentedDURING ROUTINE C-CHECK INSPECTION, LT WING FLAP L/E INBOARD PANEL LWR PART DENTED 3 INCHES, STA XW 79.000. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-7-1 FIG 1. REMOVED DAMAGED PANEL PLATING IAW DC8 SRM 57-1-0, DC8 SRM 51-1-21. FABRICATED PLATING (AL 2024T3 0.0SDR IXXA06SMN078SSkin · dentedDURING ROUTINE C-CHECK INSPECTION, LT WING INBOARD FLAP L/E LWR FWD PART DENTED, XW 40.000. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-2-5 FIG 2 (SHEET 2, 4) TR 57-91 DATE 09-30-01. REMOVED FASTENERS IAW DC8 SRM 51-1-21. TRIMMED OUT DAMAGED AREA. FABRICATED REPSDR QXEA200600721Skin · canningYYC - C4 LEFT HAND AILERON TRAILING EDGE HAS DAMAGE AND BOTTOM SURFACE IS OIL CANNING. REPAIRED IAW DHC-8-200 SRM 51-40-00, PAGE 1-5 AND SRM 57-60-71, PAGES 1-4.SDR TAMF20060008SSkin · chafedDURING C-CHECK INSPECTION WAS FOUND A CHAFING ON LT AFT FLAP INBOARD TRAILING EDGE STA IFS 108.25. DAMAGE WILL BE REPAIRED IAW EWO 767 57-008 AND BOEING SERVICE REQUEST ID: 1-171370438. FAA FORM 8100-9 MUST BE ISSUED APPROVING THIS REPAIR.SDR TAMF20060007SSkin · chafedDURING C-CHECK INSPECTION, FOUND CHAFING ON RT AFT FLAP INBOARD TRAILING EDGE WS 108.25. DAMAGE WILL BE REPAIRED IAW EWO 767 57-007 AND BOEING SERVICE REQUEST ID: 1-171370438. FAA FORM 8100-9 MUST BE ISSUED APPROVING THIS REPAIR.SDR ASAA0640235Skin · chafedRT WING IB MID FLAP UPPER SKIN CHAFED. REPAIRED PER SRM 57 53 01 FIG 201 REPAIR 3.SDR ASAA0640233Skin · dentedLT IB MID FLAP AFT TE PANEL 7220 HAS CLUSTER OF DENTS ON LWR SURFACE. PREPPED AREA OF DAMAGE FABED AND INSTALLED REPAIR DOUBLERS IAW SRM 51 70 10 REPAIR 2.SDR UIEA200600018Skin · delaminatedDURING A-4 CHECK, LEFT HAND INBOARD T/E MID FLAP HAS IMPACT DAMAGE WITH DELAM ON LOWER AFT INBOARD SURFACE AS MARKED. REPAIR CARRIED OUT IAW SRM 51-70-06 AND SRM 57-53-01.SDR ASAA0640232Panel · dentedRT IB MID FLAP AFT T/E PANEL 7420 HAS CLUSTER OF DENTS ON LWR SURFACE. PREPPED AREA OF DAMAGE FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM 51 70 10 REPAIR 3.SDR 03082006CFitting · crackedDURING FLAP INSPECTION FOUND THE FLAP FITTING (THE THICK STYLE) TO BE CRACKED APPROX 5 INCHES ON ONE SIDE AND 8 INCHES ON THE OTHER, AND THE FLAP HINGE TO ALSO BE CRACKED AT THE AFT BOLT ATTACHMENT POINT WING STATION 123.38. INSPECTED CRACK BY DYE PENETRANT ISDR 06FDEA0944Repair · unknownLEFT WING O/B FLAP T/E AREA FOUND AN EXTERNAL DOUBLER REPAIR BETWEEN WING STA XOF 563 AND XOF 575. REMOVED T/E IAW SRM 51-35-01 PAGE 1-13 VOL 2 AND DWG ARC1653, CUT AND REMOVED CRACKED SECTION AND REPAIRED IAW SRM 57-00-01 FIG 10 SHT 2 VOL 1 AND SRM 51-00-01 SDR 06FDEA0942Skin · crackedLEFT WING O/B FLAP UPPER SKIN SURFACE STA XOF 575 FOUND CRACK 2 INCHES LONG BETWEEN INTERCOSTAL PLANE NR 1 AND NR 2. REMOVED AND REINSTALLED SECTION T/E IAW SRM 51-31-01 PAGE 36/41 VOL 2 AND REPAIRED SKIN DAMAGE IAW SRM 57-10-00 FIG 65 VOL 1. FABRICATED PARTSDR 2006UALA00398Hinge Fitting · crackedLEFT INBD FLAP-CENTER HINGE FITTING CRACKED ON INBD AND OTBD FLANGES. THE SUBJECT HINGE FITTING WAS FOUND CRACKED ON THE INBOARD AND OUTBOARD FLANGE. REPAIRED PER 767-300 STRUCTURAL REPAIR MANUAL 57-53-02.SDR 06FDEA0935Hinge Bracket · corrodedINSTRUCTED TO REMOVE AND REPLACE INBOARD TRAILING EDGE FLAP OUTBOARD HINGE BRACKET WITH P/N: ARC2512-501 BUT ITEM CAME WITH P/N: ARC2512-1. REVISION B REVISES FEDEX EA 1-5750-79754A P2 BY DELETING REMOVAL AND REPLACEMENT REQUIREMENT, SCHEDULING PART II AND PASDR A6WA200640096Skin · unserviceableRT IB FLAP VANE LEADING EDGE SKIN AT MID STOP MEASURES 1.1 INCH L X .30 INCH WIDE X .22 INCH DEEP. REMOVED (PN 601R1430352) RT IB FLAP VANE MID LEADING EDGE SKIN AND INSTALLED (PN 601R14303-52) RT IB FLAP VANE MID LEADING EDGE SKIN (NEW SERVICEABLE) IAW SRM. SDR DHL2006760513Skin · crackedRIGHT INBOARD MID FLAP LOWER T/E AT PUSH-ROD CUTOUT WBL 107 HAS BOTH CORNERS CRACKED. REMOVED DAMAGED AREA DIM 46.75 X 2.25 INCHES ON RIGHT INBOARD MID FLAP LOWER T/E AND FAB NEW PART MAT BAC 1517-1367-6511. EXTRUSION DIM 46.75 X 2.25 INCHES IAW B727SRM 57-5SDR SWAA060690Skin · delaminatedDURING SCHEDULED C3 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR AWXA200600577Skin · debondedMCN - DURING C16 CHECK DISCOVERED DISBONDED AREA ON LOWER SURFACE OF LEFT HAND OUTBOARD FOREFLAP APPROX 60 INCHES FROM INBOARD END AT WS 262.69L. MAINTENANCE REMOVED DISBONDED AREA IAW BOEING 737-300 SRM 51-20-10-2R4 FIG 201. FABRICATED REPAIR DOUBLER IAW BOSDR ASAA0680224Skin · dentedLEFT INBOARD FLAP LOWER SURFACE IS DENTED. CUT OUT DAMAGED AREA. INSTALLED FILLER AND DOUBLER PER SRM 57 01 FIG 5 SHT 2.SDR 06FDEA0899Doubler · damagedDISCREPANCY RT WING OB FLAP UPPER SKIN XOFH 599 EXTERNAL DOUBLER. REMOVED AND REPLACED FASTENERS IAW SRM 57-10-00 VOL 1.SDR 06FDEA0906Skin · crackedRIGHT WING O/B FLAP T/E FROM STA XOF 458 TO XOF 467 FOUND 1EA CRACK 2 INCHES LONG ON UPPER SURFACE SKIN, 1EA CRACK ON INT CHANNEL REF SRM 57-52-01 PG 52, MANY RIVETS LOOSE ON UPPER AND LOWER SURFACE. CUT AND REMOVED T/E CHANNEL AND REPAIRED IAW SRM 57-20-00 FSDR ASAA0640220Skin · dentedLT IB FORE FLAP LWR SURFACE HAS NUMEROUS DENTS. REMOVED DAMAGED AREA FAB`D AND INSTALLED FILLERS SKIN AND DOUBLERS IAW SRM 51 70 10.SDR AWXA200600570Skin · debondedMCN - DURING C16 CHECK DISCOVERED DISBOND AREA ON LOWER SURFACE OF LEFT HAND OUTBOARD FOREFLAP, 54 INCHES FROM INBOARD END AT WS 256.69L. MAINTENANCE REMOVED DISBONDED AREA ON LOWER SURFACE OF LEFT HAND OUTBOARD FOREFLAP, 54 INCHES FROM INBOARD END IAW BOEINGSDR AMTA200600147Flap · gougedDEEP GOUGE MARKS WERE FOUND ON LT FLAP NR 3 IB RIB ASSY. REPAIRED IAW RS L57-50-34. (K)SDR 06FDEA0869Attach Bracket · corrodedDURING AIRPLANE'S CONVERSION FROM P TO F/ACF FOUND RT WING, OUTBD FLAP, INBD ATTACH BRACKET, CORROSION ON LOWER ATTACK SURFACE, INSIDE THE BORES AND IN THE LATERAL BORE OF THE FITTING. REMOVED FAIRING ATTACHING STRUCTURE IAW SRM 51-35-01. SENT OUT FOR IRAN/OSDR UPS06446386Rib · crackedINSPECTION TYPE:C LT WING O/B MID FLAP SLIDING TRACK RIB FOUND CRACKED, CRACK LENGTH 1 INCH. LT WING O/B MID FLAP SLIDING TRACK RIB REPLACED AS PER SRM 51-10-01 PG 9.SDR QXEA200600655Skin · chafedPDX-C4 CHECK, RIGHT OUTBOARD FLAP HAS A 4" CHAFE ON TOP EXTERIOR SKIN AT WS YW236.000 AND FORWARD OF TRAILING EDGE. REPAIRED IAW RD 8-57-1022 AND SRM 51-20-36, SRM 51-20-16, AND SRM 51-20-26.SDR SWAA060652Skin · delaminatedDURING SCHEDULED HC2 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP INBOARD T/E DELAMINATED. REPAIRED FLAP PER SWA EA.SDR QXEA200600594Fairing · chafedPDX: AFT SECTION OF FLAP TRACK FAIRING PANEL 626AB CHAFED. MAINTENANCE REPAIRED IAW HORIZON EA 6-57-443 AND RD 8/4-57-635.SDR SWAA060625Flap · delaminatedDURING SCHEDULED 1/4D CHECK, FOUND RIGHT WING OUTBD T/E AFT FLAP INBOARD T/E DELAMINATED. REPAIRED AFT FLAP PER SRM.SDR 2006UALA00419Flap Track · shearedFRACTURE OF LT OTBD T/E FLAP DETECTION CONTROL TRACK. LT OTBD T/E FLAP DEFLECTION CONTROL TRACK IS COMPLETELY SHEARED JUST AFT OF TIE ROD SUPPORT LUG. PER BOEING, THIS TYPE OF INCIDENT IS UNUSUAL, BUT NOT UNCOMMON. BOEING HAS RELEASE SB 767-27-0184 TO EXAMISDR QXEA200600598Skin · chafedRIGHT OUTBOARD FLAP TOP SKIN CHAFED 2 INCHES FROM INBOARD END, 15.5 INCHES FWD OF TRAIL EDGE, APPROX .375 X .25 INCH. MAINTENANCE REPAIRED IAW Q400 SRM 51-26-10, SRM 57-52-30-320-801, NDTM PART 6, 51-00-02, NDTM PART 1, 51-00-04, HORIZON EA 6-57-437, RD 6-57-SDR QXEA200600597Skin · chafedPDX: RIGHT OUTBOARD FLAP TOP SKIN CHAFED 58 INCHES FROM INBOARD END, 14 INCHES FWD OF TRAIL EDGE, APPROX 10 INCHES LONG. MAINTENANCE REPAIRED IAW Q400 SRM 51-26-10, SRM 57-52-30-370-801, NDTM PART 6, 51-00-02, HORIZON EA 6-57-437 AND RD 8/4-57-437 AND SRM 51-SDR QXEA200600596Skin · chafedPDX: RIGHT INBOARD FLAP TOP SKIN CHAFED 6 INCHES FROM INBOARD END, 19 INCHES FWD OF TRAIL EDGE, APPROX 1.25 X 0.5 INCH. MAINTENANCE REPAIRED IAW Q400 SRM 51-26-10, SRM 57-51-30-320-701, NDTM PART 6, 51-00-04, HORIZON EA 6-57-439 AND SRM 51-25-370-801.SDR QXEA200600595Hinge Fitting · chafedPDX: LEFT WING OUTBOARD FLAP FWD HINGE FITTINGS (BOTH) ARE CHAFED AT TOP OF FITTINGS NR 4 TRACK LOCATION. MAINTENANCE REPAIRED IAW RD 8/4-57-228 AND NDTM PART 6, 51-00-02-250-801.SDR SWAA060635Bolt · brokenDURING WALKAROUND INSP, FOUND LEFT INBOARD T/E FLAP OUTBOARD ROLLER BEARING BOLT BROKEN. REMOVED AND REPLACED BOLT PER MM.SDR SWAA060616Structure · delaminatedDURING SCHEDULED A2 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.SDR QXEA200600631Flap Track · corrodedPDX - C4 CHECK, RIGHT HAND NR 3 FLAP TRACK HAS PITTING CORROSION ALONG THE LENGTH OF THE TRACKS, ALONG THE PATHS OF THE ROLLERS. REPAIRED IAW RD 8-57-987.
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