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.

SDR FDEA202107041669Hinge Bracket · corrodedRIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT OUTBOARD LUG HOLE BORE FOUND WITH CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT OUTBOARD LUG HOLE BORE (#3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER Jul 4, 2021 · N311FE · Doug MD1030FSDR FDEA202107041668Hinge Bracket · corrodedRIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE UPPER MOUNT OUTBOARD LUG HOLE BORE FOUND WITH CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE UPPER MOUNT OUTBOARD LUG HOLE BORE (#2 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER Jul 4, 2021 · N311FE · Doug MD1030FSDR FDEA202107041667Hinge Bracket · corrodedRIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE BARREL NUT LOWER LUG HOLE BORE FOUND WITH CORROSION CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE BARREL NUT LOWER LUG HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER MD-10 CMM 57-44-08.Jul 4, 2021 · N311FE · Doug MD1030FSDR SWIA2021091060859Slat Track · corroded* L/H SLAT TRACK 3-2 HAS FRETTING TOP AND BTM (C-CHECK RO 9/8/21) SLAT TRACK BLENDED W/IN LIMITS IAW REO 670-57-42-1150 REV-- DATED 2021-08-23. €ŒALL STEPS C/W€?. REINSTL'D LH 3-2 SLAT TRACK IAW CRJ700 AMM 27-81-41-400-802-A01. ALL CHK GOOD. SKYCARD 5Jul 3, 2021 · N705SK · Cndair CL6002C10SDR SWIA2021091060857Hinge Fitting · corroded* R/H #4 FLAP HINGE LUGS HAVE EVIDENCE OF CORRODED HARDWARE (C-CHECK RO 9/8/2021) INSTALLED NEW HARDWARES ON RH #4 HINGE LUGS REF CRJ700 AMM 57-53-27-400-802-A01 FROM STEP 1. TO 4. AND STEP 4. A. (4) TO (16) AND STEP5.Jul 3, 2021 · N705SK · Cndair CL6002C10SDR SWIA2021091060855Hinge Fitting · corroded* R/H #5 FLAP HINGE LUGS HAVE EVIDENCE OF CORRODED HARDWARE (C-CHECK RO 9/8/2021) REMOVED AND INSTALLED NEW HARDWARE ON RH #5 FLAP HINGE LUGS REF CRJ700 AMM 57-53-27-400-803-A01 STEP 4. A. (7) (B).Jul 3, 2021 · N705SK · Cndair CL6002C10SDR SWIA2021091060854Hinge Box · corroded* R/H I/B FLAP HINGE BOX #1 HAS EVIDENCE OF CORRODED HARDWARE (C-CHECK RO 9/8/2021) REMOVED AND INSTALLED NEW HARDWARES ON I/B FLAP HINGE BOX #1 REF CRJ700 AMM 57-54-02-400-801-A01 STEP 4. A. (1)(D) (5) (7) ONLY.Jul 3, 2021 · N705SK · Cndair CL6002C10SDR SWIA2021091060852Hinge Fitting · corroded* R/H #4 FLAP HINGE LUGS HAVE EVIDENCE OF CORRODED HARDWARE (C-CHECK RO 9/8/2021) REMOVED AND INSTALLED NEW R/H # 4 FLAP HINGE LUGS REF CRJ 700 SRM 51-41-02-001-001-A01Jul 3, 2021 · N705SK · Cndair CL6002C10SDR SWIA2021091060844Skin · gougedLH INBOARD FLAP SKIN HAS DENT WITH GOUGE WS 126 AND LOWER SPAR INTERCOSTAL AS MARKED (C-CHECK RO 9/8/2021) L/H INBD FLAP LOWER SKIN DAMAGE OUT OF LIMITS, APPROX LOCATION, INTERSECTION RIB WS120.00 AND INTERCOSTAL SPART, REPAIRED ON JOB 710145125 OP 107Jul 3, 2021 · N705SK · Cndair CL6002C10SDR FDEA202107021656Hinge Bracket · corrodedRIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE PIVOT LUG HOLE BORE FOUND WITH CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE PIVOT LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-10 CMM 57-44-08. OVERSIZEJul 2, 2021 · N311FE · Doug MD1030FSDR FDEA202107021657Hinge Bracket · corrodedRIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE BARREL NUT UPPER LUG HOLE BORE FOUND WITH CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE BARREL NUT UPPER LUG HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER MD-10 CMM 57-44-08Jul 2, 2021 · N311FE · Doug MD1030FSDR FDEA202107021655Hinge Bracket · corrodedLEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE FORWARD MOUNT OUTBOARD LUG HOLE BORE SURFACE FOUND WITH CORROSION CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE FORWARD MOUNT OUTBOARD LUG HOLE BORE SURFACE REWORKED AND FOUND EXCEED LIMIJul 2, 2021 · N311FE · Doug MD1030FSDR FDEA202107021654Hinge Bracket · corrodedLEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT HOLE BORE FOUND WITH CORROSION CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT HOLE BORE (#10 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-10 CMM 57-44-09. OVERSJul 2, 2021 · N311FE · Doug MD1030FSDR FDEA202107021653Hinge Bracket · corrodedLEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE PIVOT LUG HOLE BORE FOUND WITH CORROSION. CORROSION AT LEFT 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. OVERSIZEJul 2, 2021 · N311FE · Doug MD1030FSDR FDEA202107021659Rub Strip · crackedR/W I/B FLAP O/B SUPPORT CARRIAGE I/B AND O/B PHENOLIC RUB STRIPS ARE CRACKED REMOVED AND REPLACED RUB STRIPS PER DWG #113N2150 REV CJul 2, 2021 · N997FD · Boeing 757230SDR SWIA2021091060840Vane · chafed*RIGHT WING INBOARD FLAP VANE LEADING EDGE IS CHAFED ON PANEL 684ET. (FLAGGED) (C-CHECK RO 9/8/2021) REMOVED AND REPLACED WITH NEW PANEL P/N CC670-14027-3. REF CRJ 700 SRM 51-40-06-001-001-A01.Jul 1, 2021 · N705SK · Cndair CL6002C10SDR IPXA2021071371624Tee Fitting · crackedINSPECTION TYPE:2CRT WING O/B FLAP I/B AFT HINGE FAIRING STRUCTURE TEE BEAM IS CRACKED.REMOVED AND REPLACED CRACKED RT WING O/B FLAP I/B AFT HINGE FAIRING STRUCTURE TEE BEAM IAW SRM 51-33-01 & 51-35-01. (MINOR)Jul 1, 2021 · N296UP · Doug MD11FSDR YEWA2021F00072Flap Track · brokenDURING FINAL APPROACH, THE LH OTBD FLAP I/B FLAP TRACK BROKE INTO TWO PIECES ALLOWING THE FLAP TO CANT CAUSING IT TO JAM AND NOT ALLOW TRAVEL TO THE APPROACH POSITION. BECAUSE THE FLAP WAS CANTED IT ALSO ALLOWED IT TO CONTACT THE LH AILERON INDUCING A RESISTAJun 30, 2021 · N911ZC · Beech C90ASDR IPXA2021070171165Hinge · corrodedINSPECTION TYPE:CR/H I/B FLAP O/B AFT HINGE #7 LUG BORE AND O/B FACE HAS PITTINGCORROSION REMOVED PER CMM 57-52-03. PERFORMED DETAILED, FPI, HFEC TO ENSURE NO CRACKING OR FURTHER DAMAGE PRESENT.INSTALLED BUSHINGS IAW CMM 57-52-03 REF. EO MD11-5740-80847-A AND Jun 30, 2021 · N283UP · Doug MD11FSDR IPXA2021070171164Hinge · corrodedINSPECTION TYPE:CL/H I/B FLAP O/B AFT HINGE #6 LUG BORE HOLE AND I/B FACE HAS PITTINGREMOVED PITTING AND CORROSION FROM FLAP LUG BORE IAW CMM 57-52-03. PERFORMED DETAIL INSPECTION ,FPI, AND HFEC TO INSURE NO CRACKING OR FURTHER DAMAGE.FABBED AND INSTALLED BUSHJun 30, 2021 · N283UP · Doug MD11FSDR KCSA202106301079Skin · corrodedL WING I/B T/E FLAP I/B SIDE HAS AREA OF POSSIBLE FILIFORM CORROSION UNDER SKINJun 30, 2021 · N276DH · Boeing 7673Q8SDR FDEA202106301622Vane · wornR/H INB'D T/E FLAP VANE INB'D L/E AREA SHOWING RUBBING DAMAGE. REPAIRED R/H INB FLAP VANE I/B L/E PER SRM 51-71-00 VOL II PAR 16 PG 64. I.A.W. SRM 57-00-01 FIG 4 SHEET 1. RSC TRACKING E.A. 8-5750-T-0362626 FLT. SURFACES - R/H I/B FLAP VANE STRUCTURE RJun 30, 2021 · N321FE · Doug MD1030FSDR SWAA2021071389151Skin · delaminatedRIGHT INBOARD FLAP OUTBOARD TRAILING EDGE WEDGE IS DELAMINATED. REMOVED R/H I/B MAIN FLAP PER AMM 27-51-11. REMOVED AND REPLACED R/H I/B FLAP ASSY.PER AMM 27-51-11. ADJUSTMENT CK GOOD IAW AMM 27-51-11 OPS CK GOOD PER AMM 27-51-11.Jun 29, 2021 · N283WN · Boeing 7377H4SDR SWAA2021071389152Skin · delaminatedRH INBD MAIN FLAP IS DELAMINATED ON THE OTBD AFT END.Jun 29, 2021 · N283WN · Boeing 7377H4SDR UIEA2021072201607Flap · damagedMULTIPLE AREAS OF DAMAGE ON LH IB FLAP ASSY, FOUND OUT OF LIMITS IAW B767 SRM 51-10-02. CUSTOMER REQUEST FLAP REPLACEMENT. REMOVED AND REPLACED LH IB FLAP ASSY AND OPS CHECK GOOD IAW B767 AMM 27-51-06-422-059.Jun 28, 2021 · N1093A · Boeing 73736NSDR IPXA2021072872197Skin · gougedINSPECTION TYPE:A300RT WING O/B FLAP I/B L/E SKIN GOUGED.REMOVED AND REPLACED REPAIR IAW A300 SRM 51-40-21 AND 57-50-00.Jun 28, 2021 · N144UP · Airbus A300F4622RSDR SWAA2021070288658Skin · delaminatedRIGHT WING O/B TE AFT FLAP HAS A DELAM AREA ON LOWER INBOARD SURFACE. ; / [01] R&R RH WING O/B AFT FLAP REF AMM 27-51-22. OPS CHECK GOOD; NO DEFECTS NOTED.Jun 28, 2021 · N7877H · Boeing 7377Q8SDR CALA2021062800985Fairing · missingPDA 3 REF LOGPAGE #6550149 4 FLAP TRACK FAIRING PIVOT COVERS WERE FOUND MISSING ON ARRIVAL MEX. LOGPAGE #6550149 DEFERED PER CDL 27AD. IAH AND IAD HAVE BEEN INFORMED AND ARE CHECKING LOCALLY FOR POSSIBLE REMOVAL ISSUES THAT OCCURED AND NOT REINSTALLED.Jun 28, 2021 · N818UA · Airbus A319131SDR SWIA2021081960458Hinge Arm · corroded* RIGHT WING # 4 FLAP HINGE ARM HAS CORRODED H/W COMMON TO AFT FLAP MOUNT (C-CHECK RO 8/18/2021) REMOVED HARDWARE (PIN) FROM RH WING #4 FLAP HINGE ARM. REF CRJ 700 AMM 57-53-27-000-802-A01 STEP 4A (12) AND (13). / INSTALLED NEW HARDWARE (PIN) TO RH WINJun 25, 2021 · N752EV · Cndair CL6002C10SDR SWIA2021081960450Hinge · chafed* RIGHT WING O/B #4 FLAP HINGE ARM HAS CHAFFED AFT FAIRING MOUNT (C-CHECK RO 8/18/2021) REPLACED RH WING OB #4 FLAP HINGE ARM FAIRING MOUNT (GUIDE BRACKET) INBD SIDE WITH NEW GUIDE BRACKET REF. CRJ700 SRM 51-42-06-001-001-A01Jun 25, 2021 · N752EV · Cndair CL6002C10SDR SWAA2021070687237Skin · crackedR/H I/B FLAP I/B END ELEPHANT EAR WORN AND CRACKED LOWER SIDE (MARKED) / REMOVED AND REPLACED THE ELEPHANT EAR ON THE R/H I/B FLAP; I/B END IAW AMM 27-51-11Jun 24, 2021 · N8669B · Boeing 7378H4SDR DU4R2021062300079Angle · crackedDURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND L/H WING #3 FLAP FAIRING HAS TWO CRACKED INTERNAL "L" ANGLES. S/O 660006 N/R 38745Jun 23, 2021 · N362NC · Boeing 737300SDR A6WA202107027809Skin · scratchedSCRATCH ON LH INBOARD FLAP UPPER SKIN AT INBOARD TRAILING EDGE. ***AIRCRAFT REMOVED FROM SERVICE*** PERFORMED SRM 57-52-00 INBOARD FLAP REPAIR NO. 2 ON LH INBOARD FLAP UPPER SKIN AT INBOARD TRAILING EDGE. CUTOUT DAMAGED SECTION OF UPPER SKIN INBOARD TRAILINJun 22, 2021 · N429AW · Cndair CL6002B19SDR SWIA2021081960453Hinge · corroded* LEFT WING OUTBOARD FLAP, INBOARD AND MID HINGE ARM AFT ATTACHING HARDWARE IS CORRODED. (C-CHECK RO 8/18/2021) LEFT WING OUTBOARD FLAP, INBOARD AND MID HINGE ARM AFT ATTACHING HARDWARE REPLACED WITH NEW HARDWARE. PERFORMED OPERATIONAL TEST OF THE FLAPSJun 21, 2021 · N752EV · Cndair CL6002C10SDR SWIA2021081960452Bolt · corroded* RIGHT WING FLAP BPSU MOUNTING HARDWARE IS CORROED. (C-CHECK RO 8/18/2021) REMOVED CORRODED HARDWARE ON R/H WING FLAP BPSU AND INSTALLED NEW HARDWARE IAW CRJ700 AMM CHAPTER 27-52-03-000-801-A01 AND CRJ700 AMM CHAPTER 27-52-03-400-801-A01 STEP 4. D. (4)Jun 21, 2021 · N752EV · Cndair CL6002C10SDR SWIA2021081960451Hinge · corroded* RIGHT WING OUTBOARD FLAP HINGE ARMS HAVE CORRODED HARDWARE AT THE AFT MOUNTS ( 3 EACH ). (C-CHECK RO 8/18/2021) REMOVED CORRODED HARDWARE (BOLTS 2EA, PIN 1EA) AND INSTALLED NEW HARDWARE ON R/H WING OUTBOARD FLAP HINGE ARMS AT AFT MOUNTS (BOLTS 2EA, PIJun 21, 2021 · N752EV · Cndair CL6002C10SDR SWIA2021090760810Nut · corrodedON TOP OF L/H OUTBD. FLAP (CENTER HINGE BOX)- COIL SPRING IS CORRODED ALONG WITH ITS ATTACH BOLT NUTS. ALSO, THE NUTS ARE CORRODED AT THE AFT ATTACH FITTING TO WING LOCATION (C-CHECK RO 8/29/2021) ON LH OUTBD CENTER FLAP HINGE BOX BUTE DOOR ACTUATOR SPRJun 19, 2021 · N430SW · Cndair CL6002B19SDR SWIA2021090760808Spring · corrodedON TOP OF LH OUTBD. FLAP HINGE BOX, SPRING IS CORRODED ,ALONG WITH THE ATTACH HARDWARE NUTS (C-CHECK RO 8/29/2021) REMOVED RUSTED BUTE DOOR ACTUATOR SPRING AND RUSTED HARDWARE, INSTALLED NEW SERVICEABLE SPRING AND HARDWARE IAW BOMBARDIER BUTE DOOR ACTUJun 19, 2021 · N430SW · Cndair CL6002B19SDR SWIA2021080560103Bolt · corroded*L/H OTBD FLAP INBD SEAL HARDWARE IS CORRODED (MARKED) (C-CHECK RO 8/1/2021) REMOVED AND REPLACED L/H OTBD FLAP INBD SEAL HARDWARE WITH NEW REF CRJ 200 AMM 57-53-10-400- 801. SEE CONTINUE CARD FOR DETAILSJun 19, 2021 · N945SW · Cndair CL6002B19SDR SWIA2021080560102Bolt · corroded*L/H OTBD FLAP OTBD SEAL HARDWARE IS CORRODED (MARKED) (C-CHECK RO 8/1/2021) REMOVED AND REPLACED WITH NEW 7EA BOLTS ON L/H OTBD FLAP OTBD SEAL REF CRJ 200 SRM 51-41-02Jun 19, 2021 · N945SW · Cndair CL6002B19SDR REXA2021062400453Skin · dentedDENT ON L/H I/B FLAP UPPER SKIN @ W.S. 139. REPAIRED L/H I/B FLAP UPPER SKIN IAW REO#601R-57-52-058Jun 18, 2021 · N8932C · Cndair CL6002B19SDR SCNA20210618075Skin · damagedDAMAGE TO L/H O/B FLAP UNDER I/B FAIRING. REPAIRED 2.2"X1.5" GOUGE TO L/H O/B FLAP UNDER I/B FAIRING IAW B737-800 SRM 51-70-10-2R4 REPAIR 4& B737-800 SRM 5170-102R-0 REPAIR GENERAL. RESTORED FINISH IAW B737-800 AMM 51-21-73-370-803.Jun 17, 2021 · N804SY · Boeing 7378Q8SDR SWAA2021062185312Wedge · debondedRIGHT WING INBOARD MAIN FLAP LOWER SKIN DISBONDED ON TRAILING EDGE AT OUTBOARD END. REMOVED TE WEDGE IAW SRM 51-40-02-0G-0 VERIFIED RT INBD FLAP WEDGE PART EFFECTIVITY . INSTALLED NEW RIGHT WING I/B FLAP AFT WEDGE ASSEMBLY IAW DWG 113A2100 REV A AND PL 113AJun 16, 2021 · N7846A · Boeing 73776NSDR FDEA202106161558Skin · crackedLEFT WING ,I/B FLAP, I/B LOWER SURFACE HAS CORROSION REMOVED AND REPLACED LOWER PANEL PER DWG # 113N2402 REV GJun 16, 2021 · N949FD · Boeing 757236SDR SWAA2021061885039Skin · delaminatedLEFT WING PTBD AFT FLAP LOWER SURFACE HAS A LARGE DELAMINATION AT INBD AREA. DELAM MEASURES 14' X 11' / R&R L/H O/B T/E AFT FLAP PER AMM 27-51-22 PN OFF/ON 113A700-25 SN OFF 004056 SN ON 00525AMT 11543 INSP 10886Jun 16, 2021 · N8308K · Boeing 7378H4SDR CALA2021061800887Skin · puncturedDURING WALKAROUND FOUND METAL SHAPED CLIP EMBEDDED INTO LOWER SURFACE OF INBOARD FWD FLAP ON RT WING. DAMAGE DIMENSION IS A HOLE 1.2" X.4" WIDED. LOCATION IS AT BS 321 WITHIN ZONE 7 IAW SRM 57-53-01 FIGURE 105. REPAIR PUNCTURE IAW SRM 57-53-01 ALLOWABLE DAMAJun 16, 2021 · N77014 · Boeing 777224SDR SWAA2021061883219Skin · crackedRH I/B FOREFLAP LOWER SURFACE HAS APROX 1' CRACK WITH ASSOCIATED DELAMINATION 5' FROM TRAILING EDGE AND 72' FROM O/B END. MARKED ; / REPAIRED RIGHT INBD MAIN FLAP LOWER SURFACE IAW SRM 57-51-01-2R-1 REPAIR 1.; REPAIRED RIGHT INBD MAIN FLAP LOWER SURFACE IAW SRJun 15, 2021 · N478WN · Boeing 7377H4SDR AALA202106165199Strut · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION INTERCONNECTING STRUT IB FLAP ON RIGHT WING (1 EA). REPLACED INTERCONNECTING STRUT IB FLAP ON RIGHT WING. THE INSTALLATION IS DOCUMENTED ON JOB CARD 26C67057001.Jun 15, 2021 · N701UW · Airbus A319112SDR IPXA2021070171175Hinge Bracket · corrodedINSPECTION TYPE:3CLT I/B FLAP FWD HINGE BRACKET CORRODED AT #3 LUG.REPAIRED CORRODED HINGE BRACKET IAW VT-SAA EA 011-5740-01-A91998 REV I/R AND UPS EO MD11-5740-80864-A (MINOR).Jun 14, 2021 · N283UP · Doug MD11FSDR IPXA2021062170849Rub Strip · crackedINSPECTION TYPE:A300 LT WING CENTER FLAP L/E TOP SURFACE ROLLER RUB PLATE CRACKEDREMOVED,FABRICATED,AND INSTALLED IAW A300 SRM 51-40-21 AND 57-53-12Jun 14, 2021 · N126UP · Airbus A300F4622R
Back to JASC 5753