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 FDEA200912144444Hinge Bracket · corrodedCORROSION - RT WING OTBD FLAP INBD HINGE (FLAP SIDE) PIVOT POINT NR3 INBD HOLE. REWORKED AND FOUND LIMIT IAW EA 1-5750-135690. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV. 109.SDR FDEA200912144443Hinge Bracket · corrodedCORRODED RT WING INBD FLAP OTBD HINGE (FLAP SIDE) PIVOT POINT NR1 INBD HOLE. REPAIRED IAW EA 1-5750-135692. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 109.SDR FDEA200912144442Hinge Bracket · corrodedCORROSION - RT WING INBD FLAP OTBD HINGE (FLAP SIDE) PIVOT POINT NR 1 OTBD HOLE. REPAIRED IAW EA 1-5750-135692. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 109.SDR FDEA200912114422Skin · misrepairedLT WING INBD FLAP UPPER AFT SKIN AT STA XIFH 190 FOUND WITH EXISTING REPAIR. EXISTING REPAIR AT LT WING INBD FLAP UPPER AFT SKIN AT STA XIFH 190 EVALUATED AND FOUND NOT IAW SRM REPAIR. REPAIR CARRIED OUT IAW EA NR 1-5750-137510, TITLE: WINGS - FLIGHT SURFSDR FDEA200912114421Rib · misrepairedLT WING INBD FLAP OTBD RIB AT STA XIFH 303.445 FOUND WITH EXISTING REPAIR. EXISTING REPAIR AT LT WING INBD FLAP OTBD RIB AT STA XIFH 303.445 EVALUATED AND FOUND NOT IAW SRM 57-00-00 FIGURE 205 REPAIR GENERAL REV 42. EXISTING REPAIR AT LT WING INBD FLAP OTSDR ASAA0947162Skin · delaminatedRIGHT I/B AFT FLAP O/B END IS DELAMINATED. REMOVED EXISTING REPAIR AND ACCOMPLISHED LARGE REPAIR.SDR AALA20091210TUL05Structure · corrodedCORROSION ON TOP OF RIGHT INBOARD FLAP SPAR AREA IN SEVERAL PLACES. INSTALLED TWO DOUBLERS PER ENGINEERING AUTHORIZATION COMP 57-008337.SDR 2010FA0000007Vane · brokenRT NR 3 FLAP VANE DEPARTED ACFT IN OR AROUND 12/6/2009. ACFT LANDED AND CREW DISCOVERED THAT THE FLAP VANE BROKE OFF OF THE FLAP AT THE BOLT HEAD OF THE ATTACHING BRACKET.SDR FDEA200912104404Skin · delaminatedPREVIOUSLY INSTALLED REPAIR REQUIRES REPLACEMENT. REPAIR IDENTIFIED AT RT WING, OTBD AFT FLAP, LWR SURFACE, 103" FROM INBD EDGE. REPAIRED AREA IAW SRM 51-70-05. REMOVED DAMAGE, CLEANED AND PREPPED AREA FOR REPAIR. FABRICATED REPAIR PLIES, BONDED REPAIR PLIESDR FDEA200912104403Skin · damagedPREVIOUS REPAIR INSTALLED REPAIR REQUIRES REPLACEMENT, REPAIR INDENTIFIED AT RT WING OB AFT FLAP LWR SURFACE 40" FROM IB EDGE REMOVED DAMAGE ON RT WING OB AFT FLAP LWR SURFACE AT WS 397-459. CLEANED AND PREPED AREA, FABRICATED REPAIR PN 04-009-0022 BATCH NR 0SDR 2010FA0000026Vane · brokenACFT WAS ARRIVING OR DEPARTING WHEN RT FLAP VANE BROKE OFF. THE AREA SUSPECTED WAS THE RT HINGE OF THE FLAP VANE THAT ATTACHES TO L/E OF THE FLAP AT THE ATTACHING HARDWARE.SDR ASAA0947133Skin · delaminatedLEFT I/B FLAP TRAILING EDGE WEDGE DELAMINATED ON UPPER SURFACE AT I/B AND OB ENDS. REMOVED DAMAGED SKIN AND INSTALLED FILLERS AND DOUBLERS.SDR SWAA097678Flap · delaminatedDURING SCHEDULED 2HC2 CHECK, FOUND LT WING I/B FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.SDR SWAA097677Flap · delaminatedDURING SCHEDULED 2HC2 CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR SWAA097676Flap · delaminatedDURING SCHEDULED 2HC2 CHECK, FOUND RT WING I/B FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.SDR SWAA097675Flap · delaminatedDURING SCHEDULED 2HC2 CHECK, FOUND RT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR SWAA097640Flap · delaminatedDURING SCHEDULED HC2 CHECK, FOUND RT WING T/E FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.SDR ASAA0947123Skin · dentedLT WING I/B TRAILING EDGE MID FLAP, TRAILING EDGE WEDGE NUMEROUS SHARP DENTS 38 TO 39 INCHES FROM I/B EDGE. BONDED REPAIR DOUBLER.SDR ASAA0947122Skin · dentedLT WING I/B TRAILING EDGE MID FLAP TRAILING EDGE WEDGE LOWER SURFACE SHARP DENT AT I/B EDGE. BONDED 2EA REPAIR DOUBLER.SDR ASAA0947121Skin · delaminatedRT WING O/B MID FLAP HAS DELAMINATED DENT ON LOWER SURFACE OF THE TRAILING EDGE 34 INCHES O/B OF I/B TRACK. BONDED DOUBLER AND FILLER.SDR ASAA0947120Skin · delaminatedRT WING I/B MID FLAP WEDGE LOWER SURFACE HAS DELAMINATION AT PREVIOUS REPAIR 18 INCHES FROM I/B EDGE. BONDED DOUBLER AND FILLER.SDR ASAA0947119Skin · gougedRIGHT WING I/B MID FLAP WEDGE LOWER SURFACE GOUGED JUST ABOVE THE O/B PUSH/PULL ROD. INSTALLED DOUBLER AND FILLER AND BONDED.SDR CA091207005Support Bracket · buckled(CAN) UNCOMMANDED RETRACTION OF FLAPS FROM 20 DEG TO 10 DEG ON APPROACH, RESULTING IN A DROP OF 50 FT. FLAP MOTOR CIRCUIT BREAKER POPPED. INSP FOUND THAT THE FLAP TRANSMISSION SUPPORT BRACKET PN 2611144-1 HAD BUCKLED & TWISTED PULLING THE FLAP TRANSMISSION OSDR FDEA200912044360Skin · chafedRT WING INBD FOREFLAP CHAFING UNDER NR 9 SPOILER PANEL WS 265 REMOVED DAMAGED AREA (7 1/2" X 5") SANDED, CLEANED AND PREPPED AREA IAW REV 102 SRM 51-40-20 PARAGRAPH NR 7. REPAIRED RT WING INBD FOREFLAP UPPER SURFACE BY HOT-BONDING REPAIR ON IAW SRM 51-40-20SDR SWAA097604Flap · delaminatedLT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER EA.SDR SWAA097568Flap · delaminatedDURING SCHEDULED 2HC2 CHECK, FOUND RT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR FDEA200911294217Skin · chafedLT WING OTBD T/E FLAP OTBD L/E SKIN AT WBL 561.0 FOUND WITH CHAFE MARK. LT WING OTBD T/E FLAP OTBD L/E SKIN AT WBL 561 REPAIRED IAW EA F-5750-133443 (LT TRAILING FLAP CHAFING REPAIR). REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.SDR FDEA200911294216Skin · chafedLT WING OTBD T/E FLAP INBD L/E SKIN AT WBL 302.0 FOUND WITH CHAFE MARK. LT WING OTBD T/E FLAP INBD L/E SKIN AT WBL 302 REPAIRED IAW EA F-5750-133443 (LT T/E CHAFING REPAIR). REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.SDR SWAA097481Flap · delaminatedDURING SCHEDULED MV1 CHECK, FOUND RT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR USAA2009113093259Flap · debondedPHX - B02 - MAJOR REPAIR - LEFT WING OUTBOARD FORE FLAP LEADING EDGE DISBOND ON AFT FACE AT FLAP MID SPAN. REMOVED LEFT OUTBOARD FORE FLAP ASSEMBLY IAW JOB CARD R3M22022.SDR CA091201005Structure · cracked(CAN) PILOT REPORTED VIBRATION IN LT FLAP AFTER SECOND FLIGHT OF THE DAY. UPON INSPECTION BY MAINTENANCE PERSONNEL, CRACKS WERE FOUND ON THE LT FLAP. THE CRACKS WERE LOCATED ON THE TOP OF THE FLAP TOWARDS THE LEADING EDGE ON BOTH THE RT SIDE OF THE FLAP AND SDR DHLA2010807508Skin · crackedLT INBD FLAP LWR SKIN CRACKED STA XCW 64.000. PERFORMED MAJOR REPAIR IAW SRM 57-7-1-FIG1 PG2.SDR FDEA200911264201Skin · crackedLT WING OTBD FLAP FOUND CRACK ON UPPER SKIN. REPAIRED SKIN IAW SRM 57-00-01 FIG 4, SHT 2, VOL I.SDR FDEA200911264200Skin · crackedLT WING OTBD FLAP FOUND CRACK ON UPPER SKIN. REPAIRED SKIN IAW SRM 57-00-01 FIG 4, SHT 2, VOL I.SDR FDEA200911264199Skin · dentedLT WING OTBD FLAP LWR SKIN FOUND MANY DEEP NICKS. REPAIRED SKIN IAW SRM 57-10-00, FIG 85, VOL I.SDR USAA2009120393297Support · wornSAL - BC6 - MAJOR REPAIR - WEAR ON RIGHT WING FLAP DRIVE TORSION SUPPORT ASSEMBLY LOWER AREA BETWEEN WING RIB 1 TO RIB 2. REPLACED RIGHT WING FLAP DRIVE TORSION SUPPORT ASSEMBLY IAW JOB CARD R3M57302.SDR SWAA097525Flap · delaminatedDURING SCHEDULED HC2 CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR SWAA097418Flap · delaminatedDURING SCHEDULED 14Y CHECK, FOUND RT WING O/B AFT FLAP O/B END DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR SWIA200923177Flap · crackedNACELLE FLAP CRACKED. (C-CHECK) REPLACED FLAP PER AMM.SDR SWAA097370Skin · delaminatedDURING SCHEDULED SPV CHECK, FOUND RT WING O/B AFT FLAP T/E DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR SWAA097363Skin · delaminatedDURING SCHEDULED 12Y CHECK, FOUND LT WING O/B AFT FLAP I/B UPPER SKIN DELAMINATED. REPAIRED SKIN PER SRM.SDR UALA2009112303640Carriage · damagedFLAP OUTBOARD CARRIAGE HAS DAMAGE. FLAP OTBD CARRIAGE HAS DAMAGE. REMOVED RT OTBD T/E FOREFLAP. INSTALLED RT OTBD FORE FLAP. ACCMP'D INSTALLATION TO COMPLETION.SDR MALA090148Skin · dentedDURING 2 YEAR INSP, DENT NOTED IN THE LT FLAP L/E AT WS 79.3. REPAIRED DENT ON L/E LT FLAP AT WS 78.68 IAW EO S57060.SDR ASAA0947057Rub Strip · damagedRIGHT I/B MIDFLAP T/E WEDGE RUBSTRIP & REPAIR ON CORNER ARE DAMAGED. REMOVED DAMAGED REPAIR & RUBSTRIP, FABBED FILLER & DOUBLER & BONDED REPAIR & RUBSTRIP IAW B737 400 SRM 51 70 10 REP 4.SDR AALA20091120TUL05Vane · crackedRIGHT NUMBER 2 FLAP VANE HAS A DENT WITH CRACK ON BOTTOM OF VANE. REMOVED DAMAGE AREA AND INSTALLED HOT BOND DOUBLER PER ESO 80095.SDR AALA20091120TUL04Bumper Block · damagedLEFT WING NUMBER 1 FLAP VANE HAS DEEP NICK ON RUBBER BUMPER. REMOVED DAMAGE AND INSTALLED HOT BOND REPAIR PER SRM 51-70-02.SDR AALA20091120TUL03Rib · crackedLEFT WING INBOARD FLAP INBOARD WEDGE INBOARD RIB IS CRACKED OUT AT FORWARD END. REMOVED RIB, INSTALLED NEW MANUFACTURED MODIFIED RIB REF SRM 57-01-00 FIG 3 SHEET 2 AND 51-01-00.SDR ASAA0947061Skin · gougedRT INBOARD MID FLAP LEADING EDGE UPPER SURFACE IS GOUGED. REMOVED DAMAGED AREA, FABBED FILLER & DOUBLER AND INSTALLED REPAIR PARTS IAW EA 13673.SDR ASAA0947058Skin · damagedRT INBOARD FORE FLAP LOWER SURFACE HAS A DENT WITH A CREASE & GOUGE ON PREVIOUS REPAIR. REMOVED PREVIOUS REPAIR, FABBED DOUBLER AND BONDED NEW REPAIR IAW B737 400 SRM 51 70 10 REPAIR 2.SDR FDEA200911204103Skin · dentedLT WING INBD FOREFLAP INBD L/E DENTED AND GOUGED. REMOVED 2 EACH ACCESS PANELS IAW SRM 51-30-2, CUT OUT DAMAGED AREA DIM 3/4" X 3/4" IAW SRM 51-10-1, FABRICATED REPAIR DOUBLER IAW SRM 57-50-4 FIG 1 AND 57-50-2 FIG 3, TREATED AND PRIMED PARTS IAW SRM 51
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