JASC 5753
Service difficulty reports · 31,513
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 UIEA2021030200458Skin · puncturedRH O/B FLAP FORE FLAP O/B TOP PANEL FOUND PUNCH HOLE.(<P>PERFORMED PERMANENT METAL TO METAL HOT BOND REPAIR AS PER SRM 51-70-10 REPAIR 2 FIG 203.</P>)SDR UIEA2021030200459Fairing · delaminatedRHW O/B MID FLAP L/E FAIRING FOUND DELAMINATE FORM I/B 116".(<P>PERFORMED PERMANENT COMPOSITE HOT BOND REPAIR AT RHW O/B MID FLAP L/E FAIRING AS PER SRM 51-70-07 PAR 5A.</P>)SDR UIEA2021030200460Fairing · delaminatedRHW O/B MID FLAP L/E FAIRING FOUND DELAMINATION FROM I/B 192".(<P>PERFORMED PERMANENT COMPOSITE HOT BOND REPAIR AS PER SRM 51-70-07 PAR 5A.</P>)SDR UIEA2021030200461Skin · damagedRH O/B MID FLAP UPPER SURFACE SCREW HOLE ELONGATED.(<P>PERFORMED PERMANENT COMPOSITE HOT BOND REPAIR AS PER SRM 51-70-09 PAR 5K.</P>)SDR IPXA2021031766954Support · crackedINSPECTION TYPE:3CR/H O/B FLAP I/B HINGE STOP SUPPORT ASSEMBLY IS CRACKED.REPLACED R/H O/B FLAP I/B HINGE STOP SUPPORT ASSEMBLY IAW VT-SAA EA 011-5700-01-A8938 REV. I/R AND UPS EO MD11-5750-79660-A. (MAJOR)SDR DALA2021031001373Cover · missingCREW REPORTS LT WING I/B FLAP TRACK FAIRING I/B PIVIT COVER MISSING. CORRECTIVE ACTION: INSTALLED LT WING I/B FLAP TRACK FARING I/B PIVOT COVER "CAP" PER A321 IPC 57-55. OK FOR SVC. CDL/PLAC RMVD. (LP# 7559608)SDR IPXA2021041068021Doubler · chafedINSPECTION TYPE:SEGRH WING INBOARD FLAP EXISTING REPAIR DOUBLER ON UPPER SURFACE OF FLAP HAS 3 EACH AREAS CHAFFED.COMPLIED WITH EO A300-5750-79595-ASDR SWIA202157199Skin · dentedRH INBD FLAP LWR SURFACE HAS SEVERAL DENTS OUT OF LIMITS AFTER EVAL REQUIRES A CUT-OUT DOUBLER REPAIRS. (C-CHECK RO 4/1/2021) REPAIRED R/H I/B FLAP LOWER SKIN, REF. CRJ700 SRM 57-52-01, REPAIR 005-A01 & CRJ700 SRM FIG. 57-52-01-995-802. CW 51-900-1002-SSDR FDEA202103040568Skin · dentedRIGHT WING O/B FLAP LOWER SURFACE ABOUT 24" FROM O/B END SKIN HAS DENT REPAIRED R/W O/B FLAP LOWER SKIN DENT IAW B767 SRM 57-53-01-2R FIG. 201 DET. 2, 51-70- 10 AND AMM 51-21-01/701. MAJOR REPAIRSDR SWIA202157195Skin · dentedLH INBD FLAP LWR SURFACE HAS SEVERAL DENTS OUT OF LIMITS AFTER EVAL REQUIRES A CUT-OUT DOUBLER REPAIRS. (C-CHECK RO 4/1/2021) PERFORMED FLAP LOWER SKIN REPAIR IAW CRJ 700 SRM 57-52-01-201-005-A01, FIGURE 57-52-01-995-802.AND COMPLIED WITH 51-900-1002 SKYSDR FDEA202103030546Flap Track · looseR/H O/B MAIN FLAP TRACKS #7 AND #8 ARE LOOSE AT AFT ATTACH POINTS REPLACED AFT ATTACH POINTS HARDWARE ON R/H O/B MAIN FLAP TRACKS #7 AND #8 IAW AMM 27-51-15SDR FDEA202103030544Flap Track · looseL/H O/B MAIN FLAP TRACKS #1 AND #2 ARE LOOSE AT AFT ATTACH POINTS. REPLACED AFT ATTACH POINTS HARDWARE ON L/H O/B MAIN FLAP TRACKS #1 AND #2 IAW AMM 27-51-15SDR SWIA202157335Skin · gouged*RH WING INBD FLAP HAS GOUGE ON LOWER EXTERIOR SKIN TRAILING EDGE BETWEEN APPROX WS 68.00 - 88.00. AREA MARKED. (C-CHECK RO 4/3/2021) INSTALLED -1 REPAIR DOUBLER AND -2 REPAIR FILLER ON R/H WING INBOARD FLAP LOWER SKIN REF CRJ 700 SRM 57-52-01-201-001-A01SDR SWIA202157334Skin · nicked*LH WING INBD FLAP HAS NICKS ON LOWER EXTERIOR SKIN BETWEEN FLS 15.00 - 38.00 APPROX 8 INCHES FROM TRAILING EDGE. AREAS MARKED. (C-CHECK RO 4/3/2021) REPAIRED DENT AND NICK (OUT OF LIMIT) ON LH WING INBD FLAP LOWER SKIN AT FLS 15.0 - FLS 38.0 REF CRJ 700 SDR AALA202103029002Strut · corrodedAIRCRAFT WAS GROUNDED: RIGHTHAND FLAP INTERCONNECT STRUT HAS CORROSION. REPLACED STRUT PER AMM 27-51-44.SDR AALA202103029001Strut · corrodedAIRCRAFT WAS GROUNDED: LEFTHAND FLAP INTERCONNECT STRUT HAS CORROSION. REPLACED STRUT PER AMM 27-51-44.SDR SWIA2021071459563Nut · corrodedLEFT OUTBOARD FLAP, OUTBOARD FLAP HINGE AFT ATTACHING NUT CORRODED (C-CHECK RO 7/10/2021) REMOVED AND REPLACED LEFT O/B FLAP, O/B FLAP HINGE ARM AFT ATTACHING NUT IAW CRJ700 AMM 57-53-27-000/ 400-803-A01.SDR SWIA202157022Thrust Washer · brokenRH OUTBOARD (R-1) FLAP ACTUATOR FITTING THRUST WASHER BROKEN. (C-CHECK) RO 3/24/2021 REMOVED BROKEN THRUST WASHER AND INSTALLED NEW THRUST WASHER ABOVE R-4 OTBD FLAP ACTUATOR. REF. CRJ200 SRM 51-41-02.SDR SWAA2021030352190Bracket · brokenLH MLG HOSE GUIDE ATTACH BRACKET (LOWER) BROKEN. / R/R L/H MLG HOSE GUIDE ATTACH BRACKET IAW SRM 51-40-02.SDR UIEA2021022400413Spar · cracked(5) FASTENERS HOLES HAVE INDICATIONS. MARKED IN RED MARKER ON THE FLAP.(<P>UPON DAMAGE REMOVAL EVALUATION, RIB AND SPAR CHORD FOUND OUT OF LIMITS IAW B767 SRM 57-53-1A-1. REPAIRED LH IB AFT FLAP RIB AND SPAR CHORD IAW FAS EA 21013 REV. IR</P>)SDR UIEA2021022500420Rib · crackedRH WING TRAILING EDGE INBD FLAP - 7EA HOLES HAVE CRACK INDICATIONS, MARKED AND CLOCKED INDICATIONS ON FLAP(<P>UPON DAMAGE REMOVAL, RIB AND CHORD FOUND OUT OF LIMITS IAW B767 SRM 57-53-02-1A-1. REPAIRED RH IB AFT FLAP RIB AND SPAR CHORD IAW FAS EA 21014 REV. ISDR UIEA2021022100367Skin · debondedLHW I/B FORE FLAP MID LWR PNL MID AREA 1EA EXISTING REPAIR PATCH DISBOND AS MARK.(<P>PERFORMED PERMANENT METAL TO HOT BOND REPAIR AT LHW I/R FORE FLAP MID LWR PNL MID AREA DISBOND REPAIR PATCH AREA AS PER SRM 51-70-10 REPAIR 4 FIG 201 AND REFER TO HX PROCESS CSDR UIEA2021022100368Fairing · delaminatedLHW O/B MID FLAP L/E FAIRING FOUND DELAMINATED(<P>PERFORMED PERMANENT COMPOSITE HOT BOND REPAIR</P>)SDR UIEA2021022100369Fairing · puncturedLHW O/B MID FLAP L/E FAIRING FOUND PUNCTURE(<P>PERFORMED PERMANENT COMPOSITE REPAIR</P>)SDR FDEA202102240673Bracket · crackedR/H WING OUTB FLAP INB HINGE ARC2151-3 TEE BRACKET CRACKED. REMOVED AND REPLACED R/H WING OUTB FLAP INB HINGE ANGLE ARC2151-3 PER DAC ARC2151 AND SRM 51-31-01 VOL. 2.SDR SWIA202157754Skin · dented* LH INBD FLAP LOWER SKIN HAS 2 DENTS (MARKED) (C-CHECK RO 4/22/2021) NDT DENTS DEFECT FREE. EVAL INBD DENT IS WITHIN LIMITS. EVAL OTBD DENT IS OUT OF LIMITS. RECEIVED ENGINEERING DISPOSITION TO REPAIR SKIN FOR LH I/B FLAP LWR SKIN. REPAIRED DAMAGE SDR DALA2021081104601Roller · wornPD: WORN/LOOSE, OUTBD ROLLER FITTING AT ROLLER. WORN, INBD FWD ATTACH BEARING. ELONGATED HOLES, SLIDER ON INBD ROD. WORN, INBD ROD. ELONGATED, INBD FITTING AT UP STOP ATTACHMENT. BULGING, LOWER SKIN AT TRAILING EDGE 23" FROM INBD (SDR). / CA: REPAIRED UNIT. THSDR SWIA202157719Hinge Arm · chafed* RH OTBD FLAP HINGE ARM AT WS220 GOUGED ON FWD OTBD SIDE & CHAFED ON FWD INBD SIDE (C-CHECK RO 4/21/2021) .REMOVED GOUGES ON RH OTBD FLAP HINGE ARM AT WS220 REF CRJ700 SRM 51-12-00-001-001-A01. FOUND OUT OF LIMITS. RECEIVED AND COMPLIED WITH ALL STEPS SDR SWIA202157718Hinge Arm · chafed* RH INBD FLAP HINGE ARM AT WS128.00, INBD SIDE PLATE CHAFED (C-CHECK RO 4/21/2021) R/H INBD FLAP HINGE ARM AT WS128.00, INBD SIDE PLATE REPLACED. / REF: CRJ700 SRM 51-42-06-001-001-A01SDR SWIA202157717Hinge Arm · chafed* LH INBD FLAP HINGE ARM AT WS128.00, INBD SIDE PLATE CHAFED (C-CHECK RO 4/21/2021) REPLACED LH INBD FLAP HINGE ARM SIDE PLATE AS PER CRJ 700 SRM 51-42-06-001-001-A01.SDR SWIA202157817Vane · chafedR/H I/B FLAP VANE O/B END CAP IS CHAFED IN RADIUS INTO BARE METAL APPROX 1.5" X 1.5". (C-CHECK RO 4/25/2021) PERFORMED A MAJOR REPAIR TO LH INBD FLAP VANE BY REMOVING AND REPLACING THE OUTBOARD LEADING EDGE SKIN IAW CRJ 200 SRM TASKS 51-40-11 AND 51-42-SDR SWIA202156467Flap · corrodedREPLACE CORRODED L/H WING OUTBD FLAP INBD BUTE DOOR SERRATED STOP ASSY P/N 601R10353-1 (C-CHECK) RO 2/25/2021. RECIEVED L/H WING OUTBD FLAP INBD BUTE DOOR SERRATED STOP ASSY P/N 601R10353-1 REF CRJ 200 SRM 51-77-00.SDR IPXA2021022165893Skin · dentedINSPECTION TYPE: N/ART WING OTBD AFT FLAP LWR SKIN DENT REPAIRED PER EO B747-5750-78731-B.SDR MK1Y20210221039Skin · dentedDURING MAINTENANCE INSPECTIONS AT IAI, 2 EXISTING DENTS WERE FOUND ON UNDERSIDE OF THE RT WING OUTBOARD TRAILING FLAP. THE DENTS WERE MEASURED AS HAVING WIDTHS OF 1.8" AND 1.7" AS DEPTHS OF 0.027" AND 0.029" RESPECTIVELY. THE DAMAGES WERE FOUND ABOVE LIMITS SDR 2021FA0000132Flap Track · bindingFAILURE OF THE FLAPS AT 10 DEGREES. CORRECTIVE ACTION WAS LUBRICATION OF THE FLAP ACTUATORS IN ACCORDANCE WITH BOMBARDIER MAINTENANCE MANUALS FOLLOWED BY AN OPERATIONAL CHECKSDR SWIA202156982Vane · wornRH INBD FLAP VANE INBD LEADING EDGE SKIN WORN FROM BUMPER STOP (C-CHECK) RO 3/24/2021 COMPLIED WITH REO 601R-57-52-004 REV-D DATE 2012-12-19 REPAIRS TO LEADING EDGE SKIN - INBOARD FLAP VANE. FOUND TO BE OUT OF LIMITS, REPLACED SKIN WITH NEW P/N 601R14303SDR DALA2021022201001Flap Track · corrodedSHIP 3252 CORROSION FLAP TRACK 2 PIVOT BOLT ON RT WING (1EA). CORRECTIVE ACTION: REMOVED AND INSTALLED NEW FLAP TRACK 2 PIVOT BOLT RT WING CARRIAGE BOLT AS PER A320 FAM AMM 27-54-61. (1734488)SDR DALA2021022201000Bushing · corrodedSHIP 3252 CORROSION BUSHING FITTING ATTACH FLAP TRACK 3 CARRIAGE ON LT WING (2EA). CORRECTIVE ACTION: REPLACED BUSHINGS PER AIRBUS CMM 27-54-46. (1734469)SDR DALA2021022200999Bearing · corrodedSHIP 3252 CORROSION OB FLAP AT MAIN ECCENTRIC BEARING ON RT WING (1 EA). CORRECTIVE ACTION: REMOVED AND REPLACED ATTACHMENT BEARING PER A320 FAM AMM 57-53-21. (1734479)SDR DALA2021021900982Bolt · corrodedSHIP 3252 CORROSION PIVOT BOLT OB FLAP TRACK 4 ON LT WING (1EA). CORRECTIVE ACTION: REMOVED AND REPLACED PIVOT BOLT PER A320 FAM AMM 27-54-62. (1733668)SDR DALA2021021900981Flap Track · corrodedSHIP 3252 CORROSION FLAP TRACK 3 PIVOT BOLT OB FLAP ON RT WING (1EA). CORRECTIVE ACTION: REPLACED FLAP TRACK 3 PIVOT BOLT PER A320 FAM AMM 27-54-62. (1733664)SDR DALA2021021900973Bearing · corrodedSHIP 3252 CORROSION BEARING IB FLAP (MAIN ECCENTRIC BEARING) ON RT WING (1 EA). CORRECTIVE ACTION: REPLACED BEARING PER AIRBUS CMM 57-52-21. (1733632)SDR SWIA202157443Mount · corroded* RH INBD FLAP VANE ACTUATOR MOUNT FITTINGS AT APPROXIMATELY FLS24.00 HAS CORRODED HARDWARE (C-CHECK RO 4/4/2021) REPLACED SUSPECT HARDWARE WITH NEW REF CRJ 700 AMM 20-21-00-910-801-A01, AND 20-51-00-400-807-A01. TUC6229 DUE 31-JULY-2021, TUC5658 DUE 31-JSDR SWIA202157442Vane · corroded* LH INBD FLAP VANE ACTUATOR MOUNT FITTINGS AT APPROXIMATELY FLS24.00 HAS CORRODED HARDWARE (C-CHECK RO 4/4/2021) REPLACED SUSPECT HARDWARE WITH NEW REF CRJ 700 AMM 20-21-00-910-801-A01, AND 20-51-00-400-807-A01. TUC6229 DUE 31-JULY-2021, TUC5658 DUE 31-SDR SWIA202157234Fitting · corroded* LH INBD FLAP VANE ACTUATOR MOUNT FITTINGS AT APPROXIMATELY FLS24.00 HAS 2EA CORRODED BOLTS (C-CHECK RO 4/1/2021) REMOVED 2EA CORRODED BOLTS AND INSTALLED NEW NAS6203-4 BOLTS. REF: CRJ700 SRM 51-41-02-001-001-A01. TUC5600, CAL DUE 28 FEB 22,SDR SWAA2021030852503Fairing · crackedCRACK FLAP TRACK FAIRING 1 PRELOAD PAD AT LT WING REPLACED PRELOAD PAD ON FLAP TRACK FAIRING #1 LT WING IAW SRM B73770 5140020G0 AND B737700 AMM 275128820801.SDR FDEA202102150358Skin · damagedDURING INSTALL OF R/H WING CENTER FLAP FOUND SKIN PUNCTURED, LOWER SURFACE CENTER OF FLAP. REPAIRED DAMAGE/PUNCTURED ON LOWER SURFACE OF CENTER FLAP IAW A300 SRM 57-50- 00, FIG. 205, MAJOR REPAIR.SDR DALA2021021600855Strut · corrodedSHIP 3252 CORROSION IB FLAP INTERCONNECTING STRUT ON LH WING. CORRECTIVE ACTION: REPLACED INTERCONNECTING STRUT PER DELTA WORKCARDS AMDS 2750-6010-LT AND 2750-6020-LT. (1730439)SDR SWIA202156919Plate · chafed* LH INBOARD FLAP OUTBOARD HINGE ARM INBOARD GUIDE PLATE CHAFED. (C-CHECK) RO 3/10/2021 REMOVED DAMAGE ON LH INBOARD FLAP OUTBOARD HINGE ARM INBOARD GUIDE PLATE REF CRJ200 SRM 51-12-00 SEE CONTINUATION FOR WORK PERFORMEDSDR SWIA202156918Plate · chafed* LH INBOARD FLAP INBOARD HINGE ARM INBOARD GUIDE PLATE CHAFED. (C-CHECK) RO 3/10/2021 REMOVED DAMAGE ON LH INBOARD FLAP INBOARD HINGE ARM INBOARD GUIDE PLATE REF CRJ200 SRM 51-12-00 SEE CONTINUATION FOR WORK PERFORMED
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