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 SWAA2021091505750Skin · debondedRIGHTI WING OUTBOARD AFT FLAP HAS AN AREA OF DISBOND ADJACENT TO THE INBOARD AFT CORNER OF THE TRAILING EDGE WEDGE. /SDR SWAA2021091597556Skin · debondedRIGHTI WING OUTBOARD AFT FLAP HAS AN AREA OF DISBOND ADJACENT TO THE INBOARD AFT CORNER OF THE TRAILING EDGE WEDGE. / [01] IDENTIFIED MATERIAL OF R/H O/B AFT FLAP IAW SRM 57-53-01-0I-4 FIGURE 1 AND 2; ITEM 2; 4 AND 5; TABLE 2.<BR><BR>DAMAGE IS OUT OF ALLOWABLESDR FDEA202107241888Fitting · corrodedLH OB FLAP INBD HINGE FAIRING MOUNTING BOLT HOLES TO FLAP, 4 OF 6 SHOW SIGNS OF CORROSION. LH OB HINGE WAS REPAIRED PER MD11 CMM 57-50-04 AND EA 1-5750-T363229 LH OUTBOARD TRAILING EDGE HINGE SUPPORT FITTING-REPAIR OF CORROSION AT FLAP ATTACHMENT SURFACE ASDR FDEA202107241851Skin · damagedLEFT WING O/B FLAP UPPER I/B T/E SPLIT AT CONNECTION AND DAMAGED AT CORNER. (DOT 6) REMOVED, FABRICATED AND INSTALLED L/H WING O/B FLAP UPPER I/B T/E DAMAGED SECTION REF SRM 57-20-00 VOL 1 PARAGRAPH 13 STEPS A-E.SDR FDEA202107241850Skin · delaminatedL/H WING OTBD FWD FLAP UPPER SURFACE HAS 4EA LOCATIONS OF DELAMINATION APPROX 70 OTBD OF THE INBD EDGE ALL CONTAINED WITHIN APPROX 20" OF EACH OTHER REPAIRED L/H WING O/B FWD FLAP UPPER SURFACE IAW B757-SRM 57-53-01-2R & 51-70-07-0G.SDR ASMF202110005None · noneDURING TRANSIT CHECK, IT WAS DETECTED A BIRD STRIKE ON LEFT WING. MAINTENANCE PERSONNEL PERFORMED A BIRD STRIKE INSPECTION IAW AMM TASK 05-51-18-210-801, DETECTING DAMAGES IN LEFT OUTBOARD TRAILING EDGE AFT FLAP LOWER SKIN; FIVE DENTS ON LEFT OUTBOARD TRAILINGSDR SWIA202161231None · corroded* RH INBOARD FLS65.50 FLAP VANE ACTUATOR UPPER INBOARD/OUITBOARD MOUNT BOLTS CORRODED (3EACH) (MARKED) (C-CHECK RO 9-21-21) REMOVED AND REPLACED RH INB FLS 65.50 FLAP VANE ACTUATOR UPPER INB/OB MOUNT BOLTS REF CRJ-700 AMM 27-52-23-000-801-A01 STEP (4)(A)(SDR SWIA202161230None · corroded* LH INBOARD FLS24.00 FLAP VANE ACTUATOR UPPER ROLLER NUT AND ACTUATOR OUTBOARD MOUNT BOLT CORRODED (MARKED) (C-CHECK RO 9-21-21) REMOVED AND INSTALLED NEW LH INB FLS 24.00 FLAP VANE ACTUATOR OUTBOARD MOUNT BOLT REF CRJ-700 AMM 27-52-23-400-801-A01. OPS TSDR SWAA2021072797424Skin · delaminatedR/H OUTBD AFT FLAP HAS DELAM INBD LOWER CORNER. REMOVED AND REPLACED R/H OUT/BD AFT FLAP AS PER AMM 27-51-22.SDR UIEA2021071601564Strip · damagedNO.17 V/C FLAP TOP EDGE METAL STRIP O/B AREA FOUND DAMAGE.(<P>NO.17 V/C FLAP TOP EDGE METAL STRIP REPLACED AS PER CMM 57-55-42 ASSEMBLY PAR 2C 5A (6).</P>)SDR UIEA2021071601565Strip · damagedNO.10 V/C FLAP TOP EDGE METAL STRIP O/B AREA FOUND DAMAGE(<P>NO.10 V/C FLAP TOP EDGE METAL STRIP REPLACED AS PER CMM 57-55-42 ASSEMBLY PAR 2C 5A ( 6 ).</P>)SDR FDEA202107211828Bracket · corrodedLEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE BARREL NUT LUG HOLE SURFACE FOUND WITH CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE BARREL NUT LUG HOLE SURFACE REWORKED AS PER MD-10 CMM 57-44-08 AND FOUND UPPER AND LOWER BASDR SWIA2021081960431Vane · out of limitsLEFT OUTBOARD FLAP VANE RIB AT LEFT WING WS 296.07 OUT OF LIMITS (C-CHECK RO 8/18/2021) REMOVED AND REPLACED LEFT OUTBOARD VANE RIB WITH NEW RIB. REF: CRJ700 SRM 57-53-02-201-002-A01 TYPE1 / COMPLIED WITH SKY WEST TASK CARD 51-900-1002-SKYSDR SWAA2021072696399Skin · delaminatedRT WING; O/B AFT FLAP DELAMINATED ON I/B TRAILING EDGE; TOP AND BOTTOM / [01] REMOVED OUTBOARD AFT FLAP PER M/M 27-51-22; [02] OK TO INSTALL OTBD AFT FLAP REF AMM 27-51-22; [03] REMOVED AND REPLACED RT WING O/B AFT FLAP REF MM 27-51-22SDR SWAA2021072696398Skin · delaminatedLEFT WING O/B AFT FLAP HAS DELAMINATION AREA I/B TRAILING EDGE APPROXIMATELY 5 X 3. ; / [01] REMOVED AFT FLAP PER AMM 27-51-22; [02] OK TO INSTALL AFT FLAP REF AMM 27-51-22; [03] REMOVED AND REPLACED LT WING OUTBOARD AFT FLAP REF MM 27-51-22SDR FDEA202107201827Skin · gougedR/H I/B FLAP UPPER SURFACE IS GOUGED. COMPLIED WITH EA 6-2780-T0363087 L/E SLATS AND FLAPS REPAIR UPPER SKIN R/H INBD FLAP.SDR MASA20210721286Hinge Fitting · damagedGOUGE DAMAGE TO LHS INBOARD FLAP HINGE AFT FITTING AT WS 54.55|REPAIRED PER REO 690-57-21-390 MESA RO CRJ9-57-4433
PART DEFECT LOCATION: LH INBOARD FLAP HINGE FITTING AT WS 54-55SDR DALA2021072404185Skin · wornPD: DISBONDED LOWER SKIN MIDSPAN. WORN BEARING INBD END. / CA: REPAIRED DISBONDED LOWER SKIN PER B717 SRM 57-53-01-2R RELEASE 60.00 01/15/20. REPLACED WORN BEARING REF CMM 27-50-1 DAL REV 029 DTD 03/09/2021 OEM REV 060 DTD.SDR DALA2021072004097Skin · corrodedSHIP 665 RH WING I/B FLAP UPPER I/B SKIN HAS CORROSION. CORRECTIVE ACTION: RIGHT WING I/B FLAP UPPER I/B SKIN DAMAGE FOUND TO BE COMMON TO THE TRAILING EDGE COVE PANEL INSERTS ONLY INSERTS REMOVED AND REPLACED ON ERA 592714-14 REV ORIGINAL. (1879544)SDR AALA202107202080Strut · out of rigAIRCRAFT WAS GROUNDED: DURING APPROACH INTO PHX A FLAPS LOCKED - ALIGNMENT FAULT WARNING APPEARED AT FLAPS 2. CREW DECLARED AN EMERGENCY, ABORTED THE APPROACH AND ACCOMPLISHED A GO AROUND. THE AIRCRAFT LANDED AT PHX WITHOUT FURTHER INCIDENT AND TAXIED TO THE GSDR AALA202107207409Strut · out of rigAIRCRAFT WAS GROUNDED: DURING APPROACH INTO PHX A FLAPS LOCKED - ALIGNMENT FAULT WARNING APPEARED AT FLAPS 2. CREW DECLARED AN EMERGENCY, ABORTED THE APPROACH AND ACCOMPLISHED A GO AROUND. THE AIRCRAFT LANDED AT PHX WITHOUT FURTHER INCIDENT AND TAXIED TO THE GSDR FDEA202107161798Skin · dentedRIGHT WING INBD FLAP LOWER SKIN WITH DENT L1.593" , W 1.437" ,D 0.006" RIGHT WING INBD FLAP LOWER SKIN, DENT WAS REPAIRED IAW B767 SRM 51-70-10-2R REP 4 PAG 149,150,154 FIG 201 AND B767 SRM 51-70-03-0G PAG 19,20,30,36 FIG 5 REV 79 DEC 15 2020.SDR IPXA2021072371995Angle · brokenINSPECTION TYPE:A300LT WING CENTER FLAP O/B END ANGLE BRACKET BROKEN/MISSINGREMOVED AND REPLACED 1EA ANGLE BRACKET IAW SRM 51-40--44 AND 51-40-21SDR IPXA2021072371993Angle · brokenINSPECTION TYPE:A300LT WING FLAP OB FLAP IB END ANGLE BRACKET BROKEN/MISSINGREMOVED AND REPLACED 1EA ANGLE BRACKET IAW SRM 51-40-44 AND 51-40-21SDR IPXA2021072371991Bracket · brokenINSPECTION TYPE:A3002ES L-BRACKETS ARE BROKEN BETWEEN O/B AND I/B MID FLAPREMOVED AND REPLACED L-ANGLE P/N A57960740211 AND A57960402215 IAW SRM 57-54-11,51-26-10,51-21-10 AND 51-40-21SDR IPXA2021072371990Bracket · brokenINSPECTION TYPE:A3002ES L-BRACKETS ARE BROKEN BETWEEN O/B AND I/B MID FLAPREMOVED AND REPLACED L-ANGLE P/N A57960740211 AND A57960402215 IAW SRM 57-54-11,51-26-10, 51-21-10 AND51-40-21SDR SWAA2021071593462Light · inoperativeLIGHT OUT (SIDEWALL LIGHT) ROW 8 ( CABIN INTERIOR ILLUMINATION; WITH PHOTOLUMINESCENT EMERGENCY ESCAPE PATH MARKING SYSTEM ) / R/R LIGHT ASSY.SDR CALA2021071201074Skin · delaminatedPDA 1 RIGHT OUTBOARD AFT FLAP INBOARD EDGE EXPOSED HONEYCOMB AREA 22 X 11" TRAILING EDGE ALSO DELAMINATED. REFERENCE LOGPAGE 6623875 FOR CORRECTIVE ACTION : INSTALLED RH OB AFT FLAP REF AMM 27-51-22. VERIFIED ADJUSTMENTS, ALL WITHIN LIMITS. REMOVED RIG PINS FRSDR SWIA2021090760773Skin · chafedRH INBOARD FLAP VANE IS CHAFFED ON LEADING EDGE AT IB RUB STOP LOCATION. SKIN SECTION REQUIRES REPLACEMENT (C-CHECK RO 8/29/2021) REMOVED AND REPLACED RH IB FLAP VANE LEADING EDGE IAW CRJ 200 SRM 51-42-13SDR SWIA2021090760772Skin · chafedRH INBOARD FLAP VANE IS CHAFFED ON LEADING EDGE AT OUTBOARD RUB STOP LOCATION. SKIN SECTION REQUIRES REPLACEMENT (C-CHECK RO 8/29/2021) REMOVED AND REPLACED RH IB FLAP VANE OB LEADING EDGE IAW CRJ 200 SRM 51-42-13.SDR SWIA2021090760758Skin · damagedR/H INBOARD FLAP, MID RIGHT FLAP VANE LEADING EDGE SKIN REQUIRES REPLACEMENT (C-CHECK RO 8/29/2021) REPAIRED DAMAGE TO RH INBOARD FLAP VANE MID LEADING EDGE SKIN SECTION IAW CRJ-200 SRM 57-52-00 REPAIR 1 REVISION 38B - 25 NOV 2020 , CRJ 200 SRM 51-42-13SDR FDEA202107101719Rib · cracked1EA CRACK (12MM) WAS FOUND AT R/H WING CENTER FLAP RIB 27 AFT AREA OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE WORK: RH CENTER FLAP CRACK IN UPPER FLANGE OF RIB 27 AT STRINGERS 2.8 - ALI 575306-01(FAA AD 2019-21-01) I.A.W. A300-600 EA NO: 6-5750-T0362465SDR SWIA2021091060847Vane · corroded* R/H I/B FLAP INTERNAL STRUCTURE HAS EVIDENCE OF SUSPECTED CORROSION APROX 7" FROM I/B EDGE OF FLAP AND IN BTM QUADRANT I/B SIDE OF FIRST INNER RIB (C-CHECK RO 9/8/2021) REMOVED AND REPLACED WITH NEW RH INBD FLAP. REF CRJ 700 AMM 27-52-21-400-801-A01 OSDR CALA2021070901050Skin · damagedRT OUTBD AFT FLAP, INBOARD EDGE EXPOSED HONEYCOMB AREA 22X11" TRAILING EDGE ALSO DELAMINATED.SDR SWAA2021073091817Skin · delaminatedLT I/B T/E FLAP AT O/B CORNER HAS PREVIOUS REPAIR DELAMINATING. ; / [01] REMOVED OLD REPAIR AT L/WING T/E FLAP O/B CORNER AS PER BOEING 737 SRM 51-70-10-2R-4 REPAIR 4; [02] VERIFIED STEP #1; [03] CUT- OUT DAMAGE AREA;NO WATER FOUND NO CORE DAMAGE AT L/T I/B T/SDR SWAA2021073091818Skin · delaminatedPER CUSTOMER REQUEST...RT WING O/B T/E FLAP HAS AFT EDGE DELAMINATING AT I/B CORNER ; / [01] PERFORMED CUT OUT OF 3 3/8 ' BY 1 1/4' AT DAMAGED AREA; NO WATER FOUND; NO CORE DAMAGE FOUND AT RT WING O/B T/E FLAP I/B CORNER.; [02] PERFORMED CUT OUT OF 3 3/8 ' BY SDR SWAA2021070892392Rib · crackedRIGHT WING I/B MAIN FLAP O/B L/E RIB CRACKED O/B OF AFT FLAP DRIVE ARM. REMOVED CRACKED RIB IAW SRM 51-40-02-0G-0. LOCATED AND DRILLED NEW RIB IAW SRM 51-40-05-0G-0 AND DWG 113A2213 REV- AND 113A2100 REV E. TREATED AND PRIMED NEW RIB IAW AMM 51-21-41 51-21-9SDR FDEA202107061696Skin · dentedL/H WING O/B AFT FLAP HAS 1EA DENT AT UPPER SURFACE APPROX 27" O/B OF THE 2ND TRACK OF THE AFT FLAPAND 9.25" FROM THE T/E REPAIREDL/W O/B AFT FLAP DENT AT THE UPPER SURFACE APPROX. 27" O/B OF THE 2ND TRACK OF THE AFT FLAP AND 9.25" FROM THE T/E IAW B757 SRSDR FDEA202107061695Skin · dentedL/H WING O/B AFT FLAP HAS 1EA DENT AT UPPER SURFACE APPROX. 13" I/B OF THE 2ND TRACK OF THE AFT FLAP AND 5" FROM THE T/E. REPAIREDL/W O/B AFT FLAPDENT AT THE UPPER SURFACE APPROX. 13" I/B OF THE 2ND TRACK OF THE AFT FLAPAND5" FROM THE T/E IAW B757 SRM: 57-SDR FDEA202107051681Hinge Bracket · corrodedRIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT OUTBOARD LUG HOLE BORE FOUND WITH CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT OUTBOARD LUG HOLE BORE (#3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PESDR FDEA202107051680Hinge Bracket · corrodedRIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT INBOARD LUG HOLE BORE FOUND WITH CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT INBOARD LUG HOLE BORE (#3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER SDR FDEA202107051679Hinge Bracket · corrodedRIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE PIVOT LUG HOLE BORE FOUND WITH CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE PIVOT LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-10 CMM 57-44-09. OVERSSDR FDEA202107051686Hinge Fitting · corrodedLEFT WING - FLAP SIDE OUTBOARD FLAP INBOARD HINGE INBOARD PIVOT BORE LUG HOLE FOUND WITH CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER MD-10 CMM 57-52-02. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-10 CMM 57-52- 02 AND E.A.#8-5SDR FDEA202107051685Barrel Nut · corrodedRIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT HOLE BORE FOUND WITH CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER MD-10 CMM 57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-10 CMM 57-44- 09 AND E.A.#8-5750-SDR FDEA202107051683Barrel Nut · corrodedRIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT LOWER LUG HOLE BORE FOUND WITH CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER MD-10 CMM 57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD- 10 CMM 57-44-09 AND E.ASDR FDEA202107051682Barrel Nut · corrodedRIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT UPPER LUG HOLE BORE FOUND WITH CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER MD-10 CMM 57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-10 CMM 57-44-09 AND E.ASDR FDEA202107051677Structure · damagedFOUND RH INBOARD FLAP DAMAGED DURING WALK AROUND. FABRICATED (PARTS) & REPAIRED RH INBOARD FLAP TO INCLUDE FAIRING USING EA 8-5750-T0362723 AS REFERENCE.SDR FDEA202107041672Hinge Bracket · corrodedRIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE FORWARD MOUNT OUTBOARD LUG HOLE BORE FOUND WITH CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE FORWARD MOUNT OUTBOARD LUG HOLE BORE (#6 HOLE) REWORKED AND FOUND EXCEED LIMIT AS SDR FDEA202107041671Hinge Bracket · corrodedRIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE FORWARD MOUNT INBOARD LUG HOLE BORE FOUND WITH CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE FORWARD MOUNT INBOARD LUG HOLE BORE (#6 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PESDR FDEA202107041670Hinge Bracket · corrodedRIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT INTBOARD LUG HOLE BORE FOUND WITH CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT INBOARD LUG HOLE BORE (#3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER M
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