JASC 5310

Service difficulty reports · 38,548

Reports filed under 5310 · Fuselage Main, Structure, 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 = '5310'
  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 ASOA201905167048Door Frame · corrodedSERVICE DOOR CUT-OUT CORRODED BELOW AFT LOWER STOP. REMOVED DAMAGED AREA, INSTALLED FILLER AND DOUBLER. AIRCRAFT WAS IN C CHECK BUT IS NOW RELEASED AND RETURNED TO SERVICE.Apr 22, 2019 · N14916 · Emb EMB145LRSDR UIEA2019042603973Structure · corrodedM/D STA 1240 STR 12-13 FOUND CORROSION.(<P>CABIN STA 1240 STR 12R-13R CORROSION AREAS REPAIRED IAW RI-53-00-13522 REV. A. </P>)Apr 22, 2019 · N493MC · Boeing 74747UFSDR UIEA2019042604005Panel · dentedAFT CARGO COMP STA 1680 FLOOR TORQUE BOX PANEL AT RBL 28 RBL 41 AND RBL 49 FOUND DENT(<P><SPAN>AFT CARGO COMP STA 1680 FLOOR TORQUE BOX PANEL AT RBL 28 RBL 41 AND RBL 49 DAMAGED AREAS REPAIRED IAW RI-53-65-13482 REV A</SPAN><BR /></P>)Apr 22, 2019 · N493MC · Boeing 74747UFSDR UIEA2019042604019Structure · crackedBS 990 S38R-39R CRACK FOUND AT 1EA FASTENER HOLE OF CHORD WHICH COMMON TO BATH TUB LWR FITTING(<P>CAT C REPAIR COMPLETED I.AW RL-53-00-13524 REV B WITH FOLLOW UP ACTION OF CAT A OR B REPAIR OR MODIFICATION TO BE COMPLETED WITHIN 24 MONTHS OR 1,700 FLIGHT CYCLEApr 22, 2019 · N493MC · Boeing 74747UFSDR UIEA2019042604041Torque Box · corrodedFX - KEEL BEAM TORQUR BOX AT STA 1174 LBL 8 FOUND CORROSION.(<P>CORROSION REMOVED IAW SRM 51-10-02 AND DAMAGE WITHIN ALLOWABLE LIMIT IN SRM 53-40-12 FIG 102.</P>)Apr 22, 2019 · N493MC · Boeing 74747UFSDR DALA2019042432595Door Frame · crackedWHILE PERFORMING SVC CHECK FOUND 2" CRACK ON RT WHEEL WELL FWD FRAME BELOW DOOR PROX SWITCH. REPLACED RIGHT FWD WHEEL WELL DOOR JAMB PER BOEING DWG # 5930584. (LP5655004)Apr 22, 2019 · N998DL · Doug MD88SDR SWAA2022030749405Stiffener · crackedLT FLOOR SUPPORT STIFFNER AT APPROXIMATELY F.S.540 (CENTER AISLE) CRACKED / REMOVED AND REPALCED LT FLOOR SUPPORT STIFFNER AT APPROXIMATELY FS 540 CENTER AISLE PER SRM 51-40-02Apr 21, 2019 · N8634A · Boeing 7378H4SDR SWAA2022030745902Angle · corrodedAFT CARGO COMPARTMENT BETWEEN STA 727D AND 767 R/H Z ANGLE IS CORRODED IN SEVERAL AREAS TOP AND BOTTOM SIDES AS MARKED / REMOVED AND REPLACED Z ANGLE; AFT CARGO STA 727 TO 767 R/H IAW BOEING DWG 146A7502 SHT 2 REV: A. REMOVED CORROSION IAW SRM 51-10-02-0G-0 ONApr 20, 2019 · N435WN · Boeing 7377H4SDR SWAA2022030745896Intercostal · corrodedAFT CARGO COMPARTMENT BETWEEN STA 787 AND 767 RBL 6 INTERCOASTAL WEB IS CORRODED ON INBD SIDE AS MARKED / AFT CARGO INTERCOSTAL AT 767 TO 787; RBL6 BLENDED CORROSION IAW 737-700 SRM 51-10-02-0G-0. VERIFIED MATERIAL LOSS AT ORG 'T'= .040'; REMAIN .032' LOSS OF Apr 20, 2019 · N435WN · Boeing 7377H4SDR SWAA2022030745886Support · corrodedAFT CARGO COMPARTMENT STA 907 LBL 3 FLOOR TRACK TOP SURFACE HAS SEVERAL AREAS OF CORROSION AND BOTTOM SURFACE NUTPLATES AS MARKED / BLENDED CORROSION AT AFT CARGO STA 907 LBL 3 FLOOR SUPPORT IAW 737 SRM 51-10-02-0G-0. VERIFIED LOSS AS ORG 'T' = .070'. REMAININApr 20, 2019 · N435WN · Boeing 7377H4SDR SIMA201904290006Crossbeam · crackedNLG UPLOCK BOX, AFT CROSSBEAM IS CRACKED. CRACK IS ON THE LH SIDE, OTBD OF THE UPLOCK BOX. -C/A-INSTALLED NEW NLG UPLOCK BOX AFT CROSSBEAM IAW SRM-51-40-02.Apr 20, 2019 · N661JA · Emb EMB145LRSDR SWAA2022030745867None · crackedFWD PIT; FWD SIDE OF STA 500A BELOW STR 25L; INTERCOSTAL CLIP CRACKED IN RADIUS; MRK'D. / REMOVED AND REPLACED INTERCOSTAL CLIP P/N 143A7502-13 ATAG# A82987 AT STA 500A STR 25L IAW SRM 51-40-02-0G-0 STEP 4 AND BOEING DWG# 143A7505 REV: -Apr 19, 2019 · N435WN · Boeing 7377H4SDR SWAA2022030745861Channel · corrodedFWD PIT STA 400-500D; LBL25; Z CHANNEL UPPER SURFACE HAS CORROSION ADJACENT TO 34 EA FASTENER HOLES; MRK'D. / REMOVED DAMAGE AT FWD CARGO L/H ZEE ANGLE STA 400 TO 500D LBL 25. ORIG 'T' .040'; LOSS .012'; REMAINING .028' IS OUT OF LIMITS IAW B737-700 SRM 53-00-Apr 19, 2019 · N435WN · Boeing 7377H4SDR SWAA2022030702272Support · corroded***CORROSION*** AT AFT CENTER LWR BULKHEAD SUPPORT BS 947 RBL 19 TO LBL 10 / REMOVED EXISTING BULKHEAD SUPPORT AT STA 947 RBL 19- LBL 10; REPLACED WITH NEW BULKHEAD SUPPORT PN 149A8118-30 IAW SRM 51-40-02; DWG 149A8117 59230C 07MAY19Apr 19, 2019 · N7813P · Boeing 7377K9SDR CA190423005Pressure Panel · cracked(CAN) CENTER FUSELAGE FR36 R/H SIDE, PRESSURE PANEL ATTACHMENT HOLE, 22TH FROM INBD HAS CRACK INDICATION, FWD SIDE OF THE HOLE. THIS FASTENER IS OUTSIDE OF CUTOUT AREA. (S/O 294028//N/R 40951) (TC# 20190423005)Apr 19, 2019 · Airbus A320214SDR CA190423004Pressure Panel · cracked(CAN) CENTER FUSELAGE FR36 R/H SIDE, PRESSURE PANEL ATTACHMENT HOLE, 9TH FROM INBD HAS CRACK INDICATION, FWD SIDE OF THE HOLE. THIS FASTENER IS OUTSIDE OF CUTOUT AREA (S/O 294028//N/R 40950) (TC# 20190423004)Apr 19, 2019 · Airbus A320214SDR CA190423003Pressure Panel · cracked(CAN) CENTER FUSELAGE FR36 R/H SIDE, PRESSURE PANEL ATTACHMENT HOLE, 4TH FROM INBD HAS CRACK INDICATION, FWD SIDE OF THE HOLE. THIS FASTENER IS OUTSIDE OF CUTOUT AREA (S/O 294028//N/R 40949) (TC# 20190423003)Apr 19, 2019 · Airbus A320214SDR R61A201905010458Beam · corroded***WHILE AIRCRAFT WAS IN FOR BRIDGING*** MAINTENANCE FOUND ADDITIONAL CORROSION AND CHAFE DAMAGE DURING REMOVAL OF SHEAR CLIPS, AT FR17 BETWEEN STR 24R AND 24L. REMOVED AND REPLACED BEAM AT FR 17, BETWEEN STR 24R AND 24L IAW SRM 51-40-08.Apr 19, 2019 · N806MD · Emb ERJ170100LRSDR DALA201904232580Door Frame · corrodedDURING REMOTION OF RETAINERS WAS FOUND CORROSION ON INTERNAL PRODUCTION DOUBLER AT LOWER DOOR JAMB OF AFT CARGO COMPARTMENT SUMMARY: OF NRC 00180 ON INTERNAL PRODUCTION DOUBLER AT LOWER DOOR JAMB OF AFT CARGO COMPARTMENT (CCT) WAS REPAIRED (PERMANENT REPAIR) PApr 19, 2019 · N923DN · Doug MD9030SDR DALA201904232579Door Frame · corrodedINITIAL INSPECTION: CORROSION ON DOOR JAMB LOWER AREA. AT AFT CARGO COMPARTMENT. CORROSION ON DOOR JAMB LOWER AREA WAS REPAIRED (AS PERMANENT REPAIR) PER MD90 VOL I SRM 53-60-02 FIG 9 A, ER/A 577398-14 REV ORIGINAL AND ETI90-19-020 REV 2 ASSOCIATED ER/A 00-577Apr 19, 2019 · N923DN · Doug MD9030SDR FDEA2019042290862Bracket · corrodedBS 1410, AFT CARGO DOOR, LOWER FRAME SUPPORT BRACKET HAS EXFOILIATING CORROSION, 1 INCH BY 1 INCH SIZE. BOTH SIDES OF BRACKET ARE CORRODED.Apr 19, 2019 · N928FD · Boeing 75728ASDR RAIA201904209001Door Frame · corrodedCORROSION ON LH SIDE OF CARGO DOOR FRAME AT FR 65 AROUND NUT PLATE HOLE- REMOVED CORREDED DOOR FRAME STRUCTURE AT FR 65 LH SIDE AND INSTALLED NEW FRAME STRUCTURE.Apr 19, 2019 · N13123 · Emb EMB145XRSDR SWAA2022030729741Support · crackedFLOOR SUPPORT IS CRACKED BS 540 BL0-LBL25 WL 208 / REMOVED CRACK DAMAGED FLOOR SUPPORT AT BS 540 BL 0 - LBL 25 WL 208 IAW SRM 51-40-02-0G-0 LOCATED AND DRILLED NEW FLOOR SUPPORT IAW SRM 51-40-05-0G-0 OK TO INSTALL 1365R 28APR19 INSP 28 28APR19 INSTALLED NEW FLApr 18, 2019 · N289CT · Boeing 7377H4SDR SWAA2022030729742Support · crackedFLOOR SUPPORT IS CRACKED BS 540 BL0-RBL25 WL 208 / REMOVED CRACK DAMAGED FLOOR SUPPORT AT BS 540 BL0- RBL 25 WL208 IAW ARM 51-40-02-0G-0 LOCATED AND DRILLED NEW FLOOR SUPPORT IAW SRM 51-40-05-0G-0 OK TO INSTALL 13656R 28APR19 INSP 28 28APR19 INSTALLED NEW FLOOApr 18, 2019 · N289CT · Boeing 7377H4SDR SWAA2022030746363Baffle · crackedFWD CARGO COMPARTMENT RH BAFFLE AT BS 500C-500D IS CRACKED / REMOVED AND REPLACED BAFFLE FWD CARGO R/H SIDE STA 500C TO 500D IAW BOEING DWG. 143A7505 I.D. 108 REV-.; AND SRM 51-40-02-0G-0.Apr 18, 2019 · N8614M · Boeing 7378H4SDR SWAA2022030746351Support · corrodedFWD CARGO COMPARTMENT STA 500I LBL 24-RBL 24; FLOOR SUPPORT AT AFT BULKHEAD IS CORRODED. / BLENDED OUT CORROSION ON FWD CARGO COMPARTMENT FLOOR SUPPORT AT AFT BULKHEAD STA 500I LBL24-RBL24 IAW B737 SRM 51-10-02-0G-0; ORIG THICKNESS 0.071 MAT LOSS 0.015 REMAINIApr 18, 2019 · N8614M · Boeing 7378H4SDR RJEY2019052200005Stop Fitting · crackedCRACK INDICATION ON FRAME 16 LT SIDE DOOR STOP FITTING 7.Apr 18, 2019 · N307NV · Airbus A319112SDR CALA2019041900615Door Frame · crackedROTO PROBE INSPECTION OF DOUBLE JOGGLE SHOW S CRACK INDICATION AT DOOR STOP #7 LOCATION (UPPER LOCATIONS) RH SIDE, 3RD FASTENER OF AFT COLUMN INTERIM REPAIR PERFORMED PER PART 1 OF ECRA 5311-02125.Apr 18, 2019 · N461UA · Airbus A320232SDR CALA2019041900612Door Frame · crackedROTO PROBE INSPECTION OF DOUBLE JOGGLE SHOW S CRACK INDICATION AT DOOR STOP #7 LOCATION (UPPER LOCATION) LH SIDE, 4TH FASTENER OF AFT COLUMN INTERIM REPAIR PERFORMED PER PART 1 OF ECRA 5311-02127. *DIP CREATED* THEREAFTER INTERIM REPAIR PERFORMED PER PART 1 OFApr 18, 2019 · N461UA · Airbus A320232SDR AALA201905249008Fitting · crackedAIRCRAFT IN BASE VISIT: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER ATTACHMENT CONTINUITY FITTING LH SIDE (L=0.150) IN COCKPIT (1 EA). PERFORMED PERMANENT REPAIR ON FRAME 2 WINDSHIELD CENTER POST LOWER ATTACHMENT CONTINUTY FITTING LH SIDE IAW EA 2Apr 17, 2019 · N177US · Airbus A321211SDR TLLA20190417001Rivet · looseDURING SCHEDULED INSPECTION WORKING RIVETS WERE FOUND IN CABIN ROOF STRUCTURE STATION 142. THIS IS A COMMON LOCATION FOR WORKING FASTENERS IN THE 206 SERIES AIRCRAFT, ESPECIALLY ON HIGH TIME FUSELAGES. DISCREPANT FASTENERS REPLACE IAW DER STRUCTURAL ENGINEERApr 17, 2019 · N5000G · Bell 206L1SDR SWAA2022030727359Angle · corrodedAFT PIT LH Z ANGLE BETWEEN STA 767-787 CORROSION AROUND NUTPLATE HOLES / REMOVED AND EVALUATED CORROSION; ORIGINAL THICKNESS .040' LOSS OF .006' WITH .034' REMAINING. BLEEND FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. REMOVED AND REPLACED Z-ANGLE SECTION Apr 16, 2019 · N282WN · Boeing 7377H4SDR SWAA2022030727348Angle · corrodedAFT PIT STA 747+19' RH Z ANGLE CORRODED AROUND NUTPLATE HOLE / REMOVED DAMAGE FROM AFT P2 Z ANGLE STA 747_9 IAW SRM 51-10-02-0G-0. VERIFIED LIMITS MAT. 0RIG .040' MAT. LOSS .040' MAT. REMAINING .000'. OUT OF LIMITS IAW B737-700 SRM 53-00-53-1A-2. REMOVED AND RApr 16, 2019 · N282WN · Boeing 7377H4SDR FDEA201904160808Structure · crackedRH SIDE CENTER WING JOINT AT FR40 SKIN UPPER HOLE FOUND CRACK SIGNAL REPAIRED THE RH SIDE CENTER WING JOINT AT FR40 UPPER CRACKED HOLE PER FEDEX EA: 6-5710-T0346356 P1, TITLE: WINGS - BASIC WING STRUCTURE - CRACK IN THE UPPER HOLE AT FR40 RHS CENTER WING JApr 16, 2019 · N751FD · Airbus A300B4622RSDR SWAA2019050332241Crease Beam · corrodedLT CREASE BEAM INNER CHORD UPPER SURFACE CORRODED AT BS. 344+9, LBL 61. R&R L1 CREASE BEAM IAW SRM AND DWG.Apr 16, 2019 · N282WN · Boeing 7377H4SDR SWAA2019043032075Pressure Deck · crackedR/H INTERNAL HORIZONTAL PRESSURE DECK CRACKED AT BS. 671.5, RBL 41.5. / REPAIRED DECK PER SRM.Apr 16, 2019 · N217JC · Boeing 7377H4SDR FDEA201904160811Crease Beam · corrodedMAIN CABIN CREASE BEAM STA. 860-880 RBL64.20 HAS CORROSION REMOVED CORR. ON CREASE BEAM STA 860-880 RBL 64.20 IAW B757 SRM 51-10-02. ORIG MAT .071 REM .051 LOSS .020 FOUND OUT OF LLIMITS IAW B757 SRM 53-30-13-1A FIG 101 DET VIII. REMOVED, FABRICATED ANDApr 16, 2019 · N928FD · Boeing 75728ASDR CALA2019041900598Beam · corrodedB757-53-3-0479 MAIN CABIN FLOOR BEAM FWD OF PRESSURE DECK HAS CO RROSION ON UNDERSIDE AT NUTPLATE AT APPROX. STA 1680, LBL 2, REF ST SAA N/R 0055173 CABIN FLOOR BEAM AT STA 1680 LBL 2 FOUND OUT OF LIMITS IAW B757- 200 SRM 53-00-51-A1 L=4.2, W=1.0, D=.098 CUT OApr 16, 2019 · N12114 · Boeing 757224SDR WVER201904160001Beam · damaged2 EA. OVERSIZE HOLES AT F.S.693 RBL 18 BEAM DEVIAION TO SERVICE BULLETIN 670SH-53-042 REV B.Apr 16, 2019 · N513MJ · Cndair CL6002C10SDR SWAA2022030874795Stiffener · crackedRIGHT WHEEL WELL; RBL 26 VERTICAL STIFFENER CRACKED AT LOWER END. / REMOVED AND REPLACED STIFFENER PER SRM 51-40-02.Apr 15, 2019 · N729SW · Boeing 7377H4SDR R61A2019041850384Beam · corrodedWHILE IN HEAVY CHECK, ON REMOVAL OF THE RT UPPER SHEET, 2 INCHES FRAMES 85 - 86, FOUND CORROSION ON THE BEAM. REPLACED THE BEAM IAW SRM 51-40-08.Apr 15, 2019 · N404YX · Emb ERJ170200LRSDR R61A201904150382Splice · corrodedWHILE IN HEAVY CHECK, THE RT SPLICE AT FRAME 89 HAS CORROSION. REMOVED AND REPLACED THE SPLICE IAW SRM 51-75-16.Apr 15, 2019 · N404YX · Emb ERJ170200LRSDR JJBA201904175011Receptacle · corrodedWASTE SERVICE PANEL RECEPTACLE HAS AREAS OF CORROSION AROUND DISCHARGE NOZZLE. REMOVED AND REPLACED WASTE SERVICE PANEL RECEPTACLE.Apr 15, 2019 · N11193 · Emb EMB145XRSDR WVER201904150018Structure · chafedPREVIOUS REPAIR HAS CHAFING DAMAGE AT 2 EACH ;LOCATIONS AT APPROXFS 913, STR 27. REPAIRED IAW REO 670-53-00-290 REV E.Apr 15, 2019 · N908FJ · Cndair CL6002D24SDR SWAA2019050332254Beam · crackedAFT CARGO BAY LOWER THRESHOLD VERTICAL BEAM CRACKED BETWEEN BS. 794 TO BS. 847, RBL 20. R&R BEAM IAW SRM AND DWG.Apr 14, 2019 · N551WN · Boeing 73776QSDR DALA2019041542428Door Frame · corrodedCORROSION ON LOWER DOOR JAMB FROM STA=954 TO 985 AT AFT CARGO COMPARTMENT (C2). NRC 00238: CORROSION LEVEL2, LOWER DOOR JAMB FROM STA=954 TO 985 AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-20-15-2R-7.Apr 14, 2019 · N940AT · Boeing 717200SDR DALA2019041502450Structure · crackedCRACK INDICATION FOUND HOLE A RT SIDE. REPAIR IAW WC 5311-01171- 04B REPAIRED IAW A320 AMDS CARD 5311-01171-04B.Apr 13, 2019 · N336NW · Airbus A320212SDR DALA2019041542427Door Frame · corrodedCORROSION ON LOWER/RH FWD FACE AT DOOR JAMB VENTRAL DOOR. CORROSION LEVEL2, LOWER/RH FWD FACE AT VENTRAL DOOR JAMB WAS REPAIRED PER ETI-17-19-052 REV. 3 AND ER/A 577238-14 REV. ORIGINAL.Apr 13, 2019 · N940AT · Boeing 717200SDR FDEA201904120783Beam · crackedNDT FOUND CRACK ON MDCC LHS OF GANTRY RH #5 AT FR52A REPAIRED THE CRACKED RH #5 GANTRY ON MDCC AT FR52A PER A300-600 SRM51-40-21 & AIRBUS DWG:R53810583 ISSUE:D, MAJOR REPAIR IAW FEDEX GMM 6-2-100Apr 12, 2019 · N751FD · Airbus A300B4622RSDR FDEA201904120782Beam · crackedNDT FOUND CRACK ON MDCC LHS OF GANTRY LH #4 AT FR52A. REPAIRED THE CRACKED LH #4 GANTRY ON MDCC AT FR52A PER A300-600 SRM 51-40-21 & DWG:R53810581 ISSUE:C, MAJOR REPAIR IAW GMM 6-2-100.Apr 12, 2019 · N751FD · Airbus A300B4622R
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