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.
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 FDEA202408161135Rib · crackedRRH WING CENTER FLAP RIB UPPER FLANGE FOUND 2EA CRACKS AT RIB27 BETWEEN REAR SPAR AND STGR2.7 COMPLIED WITH EA: 6-5750-T0380295 P1 REPAIRED THE RH WING CENTER FLAP CRACKED RIB UPR FLANGE AT RIB27 BETWEEN REAR SPAR AND STGR2.7. TITLE: WING - FLIGHT SURFACESDR FDEA202408161134Rib · crackedLH WING CENTER FLAP RIB UPPER FLANGE FOUND 3EA CRACKS AT RIB26 BETWEEN REAR SPAR AND STGR2.6 COMPLIED WITH EA: 6-5750-T0380294 P1 REPAIRED THE LH WING CENTER FLAP CRACKED RIB UPR FLANGE AT RIB26 BETWEEN REAR SPAR AND STGR2.6. TITLE: WING - FLIGHT SURFACESSDR FDEA202408161133Rib · crackedLH WING CENTER FLAP RIB UPPER FLANGE FOUND 1EA CRACK AT RIB17 BETWEEN REAR SPAR AND STGR2.8 COMPLIED WITH EA: 6-5750-T0380294 P1 REPAIRED THE LH WING CENTER FLAP CRACKED RIB UPR FLANGE AT RIB17 BETWEEN REAR SPAR AND STGR2.8. TITLE: WING - FLIGHT SURFACES SDR IPXA2024081698753Roller · worn**SDR FILED OPEN**FAULT - AGING A/C INSPECTION: FOUND NO.2 FLAP TRACK GENEVA CAM SUPPORT ROLLER WORN OUT 1EA. (REPLACE) COMPLETED SDRSDR IPXA2024081698500Roller · wornAGING A/C INSPECTION: FOUND NO.1 FLAP TRACK GENEVA CAM SUPPORT ROLLER WORN OUT 1EA. (REPLACE) COMPLETED SDR. OPENSDR UIEA2024080900817Skin · dentedTRAILING EDGE, INBOARD FLAP LH, WITH DENTS.(<P>TRAILING EDGE, INBOARD FLAP, MAIN FLAP WAS REPAIRED IAW SRM 57-53-01-2R-1 FIG. 201. SHEET 5. PAG 1-6 AND 51-70-17-0G-0 PAR. 4H. FIG 19. PAG 16,17 AND 47. REV 125. 15APR2024. NO FURTHER DEFECTS NOTED</P>)SDR CALA2024081902238Flap · damagedRH WING OB FLAP JUST IB OF #4 FLAP TRACK HAS DAMAGE TO COMPOSITE . GEN BY V892442 ON HAECO LCQ NR 9298895 / 26895SDR SWIA2024112500813Skin · dentedRH IB FLAP BOTTOM SURFACE HAS A DENT EVAL (C-CHECK RO 11/24/2024) PERFORMED REPAIR ON RH IB FLAP BOTTOM SURFACE PER BOMBARDIER REO 670-57-52-160. REV. -A. DATE: 2016-10-21. AND CRJ-700 SRM 51-26-01, SRM 57-52-01, SRM 51-40-11, SRM 51-26-00, SRM 51-25-01SDR SWIA202411120812Fitting · scratchedRH WING, I/O FLAP, AFTER HINGE BOX, I/O FITTING, OUTER SIDES WITH SCRATCHES (C-CHECK RO 11/9/2024) COMPLETED REPAIR OF FLAP FITTING PER REO 670-57-21-994.SDR DALA2024081308078Structure · damagedSHIP 3157 FOUND O/B FLAP DAMAGED JUST O/B OF FLAP MOVEABLE FAIRING, LEFT FLAP. CORRECTIVE ACTION: REPAIRED PER ER/A 620092-14. (5665036)SDR DALA2024081308076Roller · excess playSHIP 3149 EXCESSIVE PLAY ON CRUISE ROLLER ON O/B FLAP, RH AND LH WING 2. CORRECTIVE ACTION: REMOVED AND REPLACED CRUISE ROLLER ON O/B FLAP, RH AND LH WING 2 (E/A) AS PER AIRBUS CMM 57-53-21. (0495627)SDR AALA202410035719Tab · debondedAIRCRAFT IN BASE MAINTENANCE: DEBONDED OUTBOARD FLAP TAB ON LEFT-HAND WING. PERFORMED PERMANENT REPAIR ON UPPER SKIN OUTBOARD FLAP TAB LEFT-HAND WING PER EA #326690A.SDR SWAA2024092424871Skin · debondedDEBONDED OB AFT FLAP LOWER SURFACE IB SIDE AT RT WING 2024-512149<[01] TOOL USED: CALIPER P/N: 500-197-30 S/N: A18229508 DUE DATE: 14-JAN-25.;[02] ON STEP 3: TOOL USED BOND TESTING UNIT PN: BONDMASTER 600M; SN: 220052310; DUE DATE: 17 NOV 24;[03] TOOL USED; HOSDR FDEA20240810125Skin · misrepairedEXISTING DOUBLER REPAIR FOUND ON RH I/B FLAP UPPER SKIN AT NOSE RIB5~10, FRONT SPAR~S-2.3 COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, INSPECTION OF EXISTING DOUBLER REPAIR WAS EVALUATED AND DETERMINED IT NOT CONFORMITY PER A300-600F SRM 57-50-00 FSDR FDEA202408101252Skin · damagedEXISTING DOUBLER REPAIR FOUND ON RH I/B FLAP UPPER SKIN AT NOSE RIB 5-10, FRONT SPAR-S-2.3 COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, INSPECTION OF EXISTING DOUBLER REPAIR WAS EVALUATED AND DETERMINED IT NOT CONFORMITY PER A300-600F SRM 57-50-SDR FDEA202408101251Skin · no discrepancyEXISTING DOUBLER REPAIR FOUND ON RT I/B FLAP UPPER SKIN AT NOSE RIB 10-16, S-1.1-2.3 COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, INSPECTION OF EXISTING DOUBLER REPAIR WAS EVALUATED AND DETERMINED IT NOT CONFORMITY PER A300-600F SRM 57-50-00 FIGSDR AALA202408278484Wedge · puncturedAIRCRAFT WAS GROUNDED: RIGHT HAND INBOARD FLAP TRANSLATING WEDGE HAS PUNCTURE REQUIRES REPLACEMENT. Ï¿½ **SUPPLEMENTAL REPORT FOR (AALA202408138484): INSTALLED NEW WEDGE ASSEMBLY RIGHT HAND INBOARD, PER 27-51-22 AND EA 356992**(CLOSED).SDR AALA202408138484Wedge · puncturedAIRCRAFT WAS GROUNDED: RIGHT HAND INBOARD FLAP TRANSLATING WEDGE HAS PUNCTURE REQUIRES REPLACEMENT. Ï¿½ **SUPPLEMENTAL REPORT WILL BE SUBMITTED**(OPEN).SDR DALA2024081207999Flap Track · crackedSHIP 3149 CORROSION FLAP TRACK FAIRING 633CB BONDING PLATE ON RH WING. CORRECTIVE ACTION: REPAIRED PER ER/A 619625-14. (0495208)SDR DALA2024081207998Flap Track · crackedSHIP 3149 CORROSION FLAP TRACK FAIRING 632CB BONDING PLATE ON RH WING. CORRECTIVE ACTION: REPAIRED PER ER/A 619625-14. (0495204)SDR DALA2024081207997Flap Track · crackedSHIP 3149 CORROSION FLAP TRACK FAIRING 531CB BONDING PLATE ON LH WING. CORRECTIVE ACTION: REPAIRED PER ER/A 619625-14. (0495200)SDR DALA2024081207996Flap Track · crackedSHIP 3149 CORROSION FLAP TRACK FAIRING 532CB BONDING PLATE ON LH WING. CORRECTIVE ACTION: REPAIRED PER ER/A 619625-14. (0495195)SDR DALA2024081207995Flap Track · crackedSHIP 3149 CRACK FLAP TRACK FAIRING 533CB BONDING PLATE ON LH WING. CORRECTIVE ACTION: REPAIRED PER ER/A 619625-14. (0495186)SDR FDEA202408091095Skin · delaminatedRH WING OB FLAP LWR SURFACE FOUND DENT WITH DISBOND AT 275 IN AWAY FROM OB, 10 IN AWAY TO AFT EDGE. REPAIRED RH WING OB FLAP LWR SURFACE DENT AT OTEF STA 251 AS PER B777 SRM 57-53-01-2R REPAIR 2, SRM 51-70-04-2R REPAIR 1 REV 46.3 AND EA: G-5750-T0380234 P1, SDR SWAA2024091924103Wedge · debondedCUSTOMER REQUEST - DEBONDED IB MAIN FLAP TRAILING EDGE WEDGE PANEL LOWER SKIN AT LT WING 2024-503970<[01] TOOL USED: CALIPER PN: 500-197-30; SN: A18229508; DUE DATE: 14-JAN-25.;[02] TOOL USED: HOT BONDER P/N:HCS9200B-AV; S/N:18196127; DUE DATE:25-JAN-25.;[03] SDR SWAA2024080924346Fairing · delaminatedR/H I/B (#6) AFT FLAP FAIRING TAIL CONE IS DELAMINATED R/H I/B (#5) AFT FLAP FAIRING TAIL CONE IS DELAMINATED<[01] REMOVED AND REPLACED PER [AMM 27-51-18-400-802-NG (INBOARD FLAP SUPPORT AFT FAIRING INSTALLATION - PERMANENT)]SDR DALA2024081908247Skin · missing(LOG 5723746) ON MEET AND GREET FOUND LT WING OUBOARD AFT FLAP, I/B TE LOWER SKIN MISSING. REPLACED LT WING AFT FLAP OUTBOAIRD PER B737 AMM 27-51-22-400-801.SDR ASAA2024080751749Skin · debondedLEFT WING INBOARD MAIN FLAP LOWER SKIN OUTBOARD EDGE DISBOND 3"X1". GROUNDED - YES. REMOVED DISBONDED LWR SKIN & REPAIRED IAW B737-800 SRM 57-53-01-2R-7, B737-800 SRM 51-70-10-2R-4 & B737-800 SRM 51-70-10-2R-0. SEALED DOUBLER IAW B737-800 SRM 51-70-10-2R-0. RESDR SWAA2024082923292Skin · delaminatedL/H O/B TRAILING EDGE FLAP I/B LOWER SURFACE IS DELAMINATED.<[01] OK TO INSTALL NEW L/H O/B AFT FLAP S/N 001118;[02] INSTALLED NEW L/H O/B AFT FLAP PER AMM 27-51-22;[03] RII INSPECTED AS REQUIRED. CORRECTIVE ACTION #2; VERIFIED TORQUES AND SAFETIES.SDR UIEA2024073100763Fairing · delaminatedLHW I/B FORE FLAP L/E FAIRING FOUND DELAMINATION(<P>PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024073100762Fairing · delaminatedRHW O/B FORE FLAP MID L/E FAIRING FOUND DELAMINATION(<P>PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024073100761Fairing · delaminatedRHW I/B FORE FLAP MID L/E FAIRING FOUND DELAMINATION. PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5A. NO FURTHER DEFECTS NOTED.SDR SWAA2024082922537Wedge · crackedL/H WING I/B MAIN FLAP TRAILING EDGE WEDGE HAS DELAM AREA ON UNDERSIDE OF WEDGE. (MARKED)<[01] REMOVED DAMAGE PER SRM 57-53-01-2R-7 AND SRM 51-70-10-2R-4.;[02] INSPECTED C/A 1.;[03] APPLIED REPAIR PER SRM 57-53-01-2R-7 AND SRM 51-70-10-2R-4;[04] 02 - PERFORMEDSDR DALA2024080707864Skin · dentedMTC TASK- RH WING I/B FLAP LOWER SURFACE FOUND WITH MULTIPLE DENTS. RH WING I/B FLAP LOWER SURFACE REPAIRED AS PER ER/A 619792-14 PRI REV 0. ER/A 619792-14 PRI REV 0 COMPARED WITH ER/A 619792-14 REV ORIGINAL AND FOUND IN COMPLIANCE. ASSOCIATED ER/A 14-619792 ASDR SWAA2024082922208Skin · delaminatedR/H O/B AFT FLAP I/B UPPER SURFACE DELAMINATED. MARKED.<[01] REMOVED DAMAGE TO AREA PER SRM 51-70-10-2R-0.;[02] VERIFIED 1. RYAN ROGERS (TECHNICIAN); 07-AUG-2024 14:13 UTC<BR>REMOVED DAMAGE TO AREA PER SRM 51-70-10-2R-0.;[03] ACCOMPLISHED REPAIR TO AREA PER SRSDR SWAA2024082822217Angle · crackedON THE LEFT WING OTBD FIXED TRAILING EDGE PANEL; THE LOWER BULB SEAL BRACKET ATTACHED TO FWD END OF THE PANEL HAS A CRACK NOTED AT THE OTBD ATTACH FASTENER.<[01] REMOVED DAMAGED WEB (ANGLE) IAW SRM 51-40-02;[02] REMOVED AND REPLACED BRACKET PER SRM 51-40-02;[0SDR SWAA2024082822207Skin · delaminatedLEFT WING OUTBD AFT FLAP INBD LWR CORNER IS DELAMED ON UPPER SURFACE.<[01] REMOVED AFT FLAP PER MM 27-51-22.;[02] OK TO INSTALL NEW FLAP (RII);[03] TOOLING;[04] INSTALLED NEW LH OT AFT FLAP. IAW AMM 27-51-22. ADJUSTMENT CHECK REQUIRED.;[05] INSTALLED NEW LH OTSDR SWI2024F01217Skin · chafedL/H I/B FLAP, HAS CHAFING ON THE CENTER OF THE LEADING EDGE OF THE FLAP VANE (C-CHECK RO 11/9/2024) AFTER EVAL FOUND DAMAGE TO BE OUT OF LIMITS VANE CAP WAS REPLACED AND PAINT FINISH RESTORED IAW CRJ700 SRM 51.42.73, 51.21.11, 51.25.06 AND 51.25.16.SDR SWIA202411120802Skin · gougedRIGHT WING OUTBOARD FLAP HAS MULTIPLE GOUGED VANE MOUNTS AND STRUCTURES AS MARKED (C-CHECK RO 10/26/2024) (FILED CLOSED)BLENDED GOUGES ON RIGHT WING OUTBOARD FLAP HAS MULTIPLE VANE MOUNTS AND STRUCTURES. REF CRJ200 SRM 51-12-00. FOUND TO BE OUT OF LIMITS. RECESDR SWIA2024102802Vane · gougedRIGHT WING OUTBOARD FLAP HAS MULTIPLE GOUGED VANE MOUNTS AND STRUCTURES AS MARKED (C-CHECK RO 10/26/2024) (FILED OPEN)BLENDED GOUGES ON RIGHT WING OUTBOARD FLAP HAS MULTIPLE VANE MOUNTS AND STRUCTURES. REF CRJ200 SRM 51-12-00. FOUND TO BE OUT OF LIMITS. RECEIVSDR SWAA2024080621519Skin · delaminatedLH WING; OUTBOARD AFT FLAP; LOWER SKIN DELAMINATED. 7 1/2 INCH X 7 1/2 INCH; 5 INCHES FROM TRAILING EDGE; 6 INCHES FROM INBOARD EDGE.<[01] REPLACED LH WING; O/B AFT FLAP PER AMM 27-51-22. OPS CHECK GOOD;[02] 02 - INSPECTED PER [AMM 27-51-22-401-NG (OUTBOARD AFSDR DALA2024080607803Skin · corroded(LOG 0481225) CORROSION ON LEFT WING I/B T/E FLAP I/B EDGE LOWER SURFACE FASTENER HOLE SHOW SIGNS OF CORROISION 7TH FASTENER FROM I/B BOTTOM SIDE. ACCOMPLISHED REPAIR PER ER/A 619636-14 REV O.SDR HNAA2024091100766Bonding Strap · corroded57-2271 RH IB FLAP HAS CORROSION ON BONDING STRIP AT FLAP ROOT. RAR BONDING STRIP IAW SRM 51-40-02SDR IXXA20240807001Skin · delaminatedRIGHT WING, OUTBOARD FLAP, OUTBOARD LEADING EDGE SECTION IS DELAMINATED. POSSIBLE CAUSE UNDETERMINEDSDR IXXA2024073105Skin · dentedLEFT WING INBD AFT FLAP DENTS 16,17,18SDR IXXA2024073104Skin · dentedLEFT WING TRAILING EDGE INBD AFT FLAP DENTEDSDR SWAA2024080519929Panel · delaminatedRIGHT WING INBOARD TRAILING EDGE FLAP IS DELAMINATED AT O/B AFT TRAILING EDGE APPROX 240 SQ/IN.<[01] REMOVED R/H INB FLAP TRAILING EDGE WEDGE PANEL PER SRM 51-40-02.;[02] REMOVED RIGHT I/B AFT FLAP WEDGE PANEL PER CMM 57-53-09.;[03] VERIFIED MECHANIC REMOVED RSDR SWAA2024080519931Panel · delaminatedLEFT WING I/B FLAP HAS A DELAMINATED AREA ON O/B AFT WEDGE APPROXIMATELY 9.6 X 8<[01] REMOVED AND REPLACES LEFT I/ B FLAP WEDGE PANEL PER CMM57-53-09.;[02] VERIFIED REMOVED AND REPLACED LEFT I/ B FLAP WEDGE PANEL PER CMM57-53-09.;[03] PAINTED I/B FLAP WEDGE PASDR IXXA2024073005Skin · dentedLW AFT FLAP DENTEDSDR SWAA2024082318661Wedge · delaminatedLEFT WING I/B MAIN FLAP TRAILING EDGE WEDGE HAS LARGE DELAMINATION. (MARKED)<[01] REMOVED DELAMINATED LEFT WING I/B MAIN FLAP TRAILING EDGE WEDGE PER SRM 51-40-02.;[02] INSTALLED LEFT WING I/B MAIN FLAP TRAILING EDGE WEDGE IAW SRM 51-40-02. INFO REFERENCE BOEI
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