JASC 5310

Service difficulty reports · 38,528

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 SWAA2021072831587Stop Fitting · crackedFWD E/E ACCESS DOOR L/H SIDE LOWER STOP FITTING CRACKED / REMOVED AND REPLACED FWD E/E ACCESS DOOR L/H SIDE LOWER STOP FITTING PER CMM 52-48-01.AMT 104702INSP 49017Nov 20, 2020 · N8683D · Boeing 7378H4SDR R61A2020122100933Crossbeam · corrodedCORROSION ON CROSSBEAM AT FR 14 Y+26. R & R REPAIR STRAP, IAW SRM 53-00-10.Nov 20, 2020 · N241JQ · Emb ERJ170200LRSDR SCNA20201201392Stub Frame · crackedSTUB BEAM BS 296.4 RT CRACKED/BROKEN INBOARD FLANGE AT WL 208 RBL 62. REMOVED DAMAGE AREA AT STUB FRAME BS 296.4 INBOARD FLANGE AT WL 208 RBL 62, PER SRM 53-10-15-2R-7 PARA 4B, C MADE REPAIR PART ITEM (I) PER SRM 53-10-05-2R-7 ALODINE AND PRIMED, PER SOPM 20-Nov 20, 2020 · N817SY · Boeing 7378K2SDR SCNA20201201361Door Frame · corrodedFWD SERVICE DOOR LOWER SILL INNER CHORD HAS CORROSION FROM STA 297-332, RBL 64, WL 208. INSTALLED FWD SERVICE DOOR LOWER SILL INNER CHORD FROM BS 360 TO BS 259.5 RBL 64 WL 208, PER SRM 51-40-02-0G-0 PARA 4B 7D DWG NR 141A8310, 143A5900, AND ATTACHED ANGLE.Nov 20, 2020 · N817SY · Boeing 7378K2SDR K11A2020112400031Window Frame · corrodedEXTERNAL WINDOW FRAME CORROSION STA 950D-950E LEFT.Nov 20, 2020 · N726CK · Boeing 7272M7SDR K11A2020112400029Window Frame · corrodedEXTERNAL WINDOW FRAME CORROSION STA 970-990 RIGHT.Nov 20, 2020 · N726CK · Boeing 7272M7SDR DALA2020112303823Door Frame · crackedCRACK INDICATION ON PASSENGER CREW DOOR FRAME 16 RT STOP FITTING. CORRECTIVE ACTION: REPLACED INTERCOSTAL WEB LOCATED BETWEEN FR 15 TO FR 16 AT LEVEL OF DOOR RT SIDE IN PASSENGER CABIN COMPLYING WITH ER/A 588369-14AD. OK FOR SERVICE.Nov 20, 2020 · N377NW · Airbus A320211SDR R61A2020120700847Doubler · corrodedCFIII, CORROSION FOUND ON WASTE AND WATER BOX DOUBLER BETWEEN FR 88-FR 89 AND BETWEEN STR 25-28 RT. REPAIRED IAW SRM 53-23-60 REV 44.Nov 19, 2020 · N212JQ · Emb ERJ170200LRSDR SCNA20201201360Door Frame · corrodedFWD ENTRY DOOR LOWER SILL INNER CHORD HAS CORROSION FROM STA 303.9-348.2, LBL 64, WL 208. CORROSION ON LOWER INNER CHORD BS 348-304 LBL 64 WL 208 FOUND TO BE OUT OF LIMITS, IAW SRM 53-10-15-1A-1 FIG 103 DETAIL D. REMOVED INNER CHORD, IAW SRM 51-40-02-0G-0. Nov 19, 2020 · N817SY · Boeing 7378K2SDR DALA2020112003802Panel · damagedWEAR AND ELONGATED HOLES ON AFT EDGE AT 193D CENTER WHEEL WELL PANEL. REPAIRED, PER B737-800 SRM 51-70-04-2R-10 PAR 4, IN REFERENCE TO ERA 588671-14AD REV ORIGINAL SECTION 1.Nov 19, 2020 · N383DN · Boeing 737832SDR SWIA202055352Door Frame · corrodedAVIONICS BAY DOOR SURROUND STRUCTURE, INTERCOSTAL CORRODED AT STGR 27L. C-CHECK RO 1/6/2021. REFERENCE CAMP NR 21867157, 910220124/40 FOR REPLACEMENT OF AVI DOOR SURROUND INTERCOSTAL AT STGR 27L BETWEEN FS 349-FS 364. SEE CONTINUE CARD FOR MAINTENANCE PERFONov 18, 2020 · N755SK · Cndair CL6002C10SDR SWIA202054991Door Frame · corrodedPAX DOOR FRAME IS CORRODED INSIDE OF THE VENT FLAP STRUCTURE ON THE AFT SIDE OF CUT OUT. C-CHECK RO 12/30/2020. REMOVED AND REPLACED PAX DOOR FRAME AT FS 349, IAW CRJ 200 SRM. COMPLETED TASK CARD AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE NOTED.Nov 18, 2020 · N924SW · Cndair CL6002B19SDR FDEA202011182897Structure · crackedCENTER WING BOX, INSPECTION OF REAR SPAR AND BOTTOM PANEL AT JUNCTION OF FUSELAGE, LT SIDE, HOLE "C" FOUND CRACK SIGNAL. COMPLIED WITH EA: 6-5710-T0357880 P1. TITLE: WINGS-BASIC WING STRUCTURE-CRACK HOLE C AT FR 47 LT SIDE DURING SB57-6086 EMBODIMENT. REPNov 18, 2020 · N728FD · Airbus A300B4622RSDR SWAA2020120931015Crease Beam · corrodedCORROSION ON CREASEBEAM INNER CHORD STA 675-727 RBL 65 WL 208 UPPER SURFACE. REMOVED DAMAGED CREASE BEAM INNER CHORD AND INSTALLED NEW CREASE BEAM INNER CHORD AT BS 675-727 RBL 65 WL 208, IAW SRM 51-40-02-0G-0 AND DWG 144A5900.Nov 17, 2020 · N730SW · Boeing 7377H4SDR SWAA2020121536060Pressure Deck · dentedCOCK PIT FLOOR HAS DENTS AT STATION 254 LBL 2 AND UNDER OBSERVER SEAT. REPAIRED COCKPIT FLOOR WEB, PER EA 1-A53-33179.Nov 16, 2020 · N7744A · Boeing 7377BDSDR DALA2020111803774Seal Depressor · corrodedDURING MX CHECK FOUND CORROSION AT AFT CARGO DOOR LOWER SILL DEPRESSOR, FRAME 55. CORRECTIVE ACTION: REMOVED CORROSION ON DEPRESSOR AT FRAME 55. REMOVED SEAL DEPPRESSOR SECTION; DVI COMPLETED, NO FURTHER DAMAGE NOTED. MATCH DRILLED NEW SEAL DEPRESSOR, PER ANov 16, 2020 · N303DN · Airbus A321211SDR DALA2020111803773Seal Depressor · corrodedDURING MX CHECK FOUND CORROSION AT AFT CARGO DOOR LOWER SILL SEAL DEPRESSOR, FRAME 54 MINUS 9.5". CORRECTIVE ACTON: CORROSION REMOVED ON SEAL DEPRESSOR 9.5" FWD OF FRAME 54 NDT. REMOVED SEAL DEPRESSOR SECTION, PERFORMED DVI, NO FURTHER DAMAGE NOTED. MATCH DNov 16, 2020 · N303DN · Airbus A321211SDR SWAA2020120930469Crease Beam · corrodedCORROSION CREASE BEAM WEB RT BS 663-685 AT CENTER LIGHTNING HOLE INBOARD SIDE RBL 65 WL 208. REMOVED CORROSION ON CREASE BEAM WEB RT RBL 65, WL 208 STA 663-685 AT CENTER LIGHTNING HOLE INBOARD SIDE. MAX MATERIAL REMOVED ON WEB WAS .008' 1' X 2' FROM .040' OUNov 15, 2020 · N730SW · Boeing 7377H4SDR SWAA2020120834518Pressure Deck · dentedFLIGHT DECK FLOOR IS DENTED AT BS 255 RBL 4 LBL 14 WL 207.54. DAMAGE REPAIRED, PER EA 1-A53-33179 REV 1 AND ER 20-03616 REV IR AND EA 20-153-02333 REV IR.Nov 13, 2020 · N730SW · Boeing 7377H4SDR JGVR20201113002Door Frame · chafedREPAIRED CHAFED E-EXIT SURROUND WEB AND FRAME AT APPROXIMATELY FS 400 PER AEROSPACE QRD ERO-967189 REV IR, TITLED "E-EXIT SURROUND WEB AND FRAME REPAIR" DATED OCT 30 2020 AND SUPPORTED BY FAA FORM 8110-3 DATED 10/30/2020.Nov 13, 2020 · N375QS · Cessna 680ASDR JGVR20201113001Structure · corrodedREPAIRED SEVERAL AREAS OF CORROSION ON FUSELAGE DROP AISLE STRUCTURE BETWEEN FS 165 AND FS 426 PER AEROSPACE QRD ERO-967178 REV IR DATED NOVEMBER 09, 2020 AND SUPPORTED BY FAA FORM 8110-3 DATED NOVEMBER 09, 2020.Nov 13, 2020 · N375QS · Cessna 680ASDR DALA2021070203670Pressure Panel · crackedSHIP 3270 CRACK INDICATION ON INTERNAL STRUCTURE PRESSURE PANEL 3 E/A RH SIDE IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPAIRED PER DELTA WORKCARD AMDS 5311-01171-04B. (1654226)Nov 12, 2020 · N370NW · Airbus A320212SDR DALA2021070203669Pressure Panel · crackedSHIP 3270 CRACK INDICATION ON INTERNAL STRUCTURE 3 E/A ON PRESSURE PANEL LH SIDE IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPAIRED PER DELTA WORKCARD 5311-01171-04A. (1654224)Nov 12, 2020 · N370NW · Airbus A320212SDR SWIA202054901Door Frame · damagedLT EMERGENCY ESCAPE DOOR SURROUND FRAME P/N SH670-36070-6 AT APPROXIMATELY FS 785.15 HAS ELONGATED MOUNTING HOLE FOR SIDE SEAT RAIL. C-CHECK RO 12/28/2020. COMPLIED WITH REPAIR TO LT EMERGENCY ESCAPE DOOR SURROUND FRAME P/N SH670-36070-6 AT APPROXIMATELY FS Nov 12, 2020 · N787SK · Cndair CL6002C10SDR SWAA2020121433039Structure · crackedCRACK INNER CHORD LOCATED AT BS 303.9 AT LEVEL STR 17L AT FWD GALLEY AREA. REPLACED INNER CHORD LOCATED BS 270 TO BS 360 AT LEVEL STR 17 LBL 61.5 AT FWD GALLEY AREA. DUO CRACK L=0.600' NOT ALLOWABLE DAMAGE. PART NUMBER USED 654A000-4-1073, IAW B737-700 SRM Nov 12, 2020 · N932WN · Boeing 7377H4SDR SWAA2020121433038Structure · corrodedCORROSION INNER CHORD LOCATED BETWEEN BS 967 TO BS 986.5 AT LEVEL STR 17R RBBL 64 AT PASSENGER CABIN WL 208.1. REPLACED INNER CHORD LOC BETWEEN BS 967 TO BS 986.5 AT LEVEL STR 17R RBBL 64 AT PASSENGER CABIN WL 208.1, IAW B737-700 SRM 51-10-02 SRM 51-40-02 ANDNov 12, 2020 · N932WN · Boeing 7377H4SDR AALA202012119008Window Frame · crackedAIRCRAFT IN BASE MAINATENANCE. CRACK INDICATION ON FRAME 4 LATERAL WINDOW FRAME UPPER STIFFENER RIGHT HAND SIDE BETWEEN FR 3 AND FR 8 AT -Y765. REPLACED WINDOW FRAME, PER EA 309364.Nov 12, 2020 · N763US · Airbus A319112SDR FDEA202011122830Floorbeam · corrodedAFT CARGO COMPARTMENT FLOOR SUPPORT STRUCTURE CROSSBEAM CORRODED AT FR 60 BETWEEN Y805 AND -Y805. REPAIRED THE AFT CARGO COMPARTMENT FLOOR SUPPORT CROSSBEAM AT FR 60 BETWEEN Y805 AND -Y805, PER A300-600 SRM 53-10-15-201 PARAGRAPH 9. THIS IS CATEGORY A REPAIRNov 12, 2020 · N728FD · Airbus A300B4622RSDR FDEA202011122829Crossbeam · corrodedAFT CARGO COMPARTMENT FLOOR SUPPORT STRUCTURE-CROSSBEAM CORRODED, AT FR 59, BETWEEN Y805 AND -Y805. REPAIRED THE AFT CARGO COMPARTMENT FLOOR SUPPORT CROSSBEAM AT FR 59, BETWEEN Y805 AND -Y805, PER A300-600 SRM53-10-15-201 PARAGRAPH 9. THIS IS CATEGORY A REPANov 12, 2020 · N728FD · Airbus A300B4622RSDR FDEA202011122828Pressure Deck · damagedHORIZONTAL PRESSURE DECK UPPER SURFACE BETWEEN FR 39 AND FR 40, -Y1959 AND -Y2462 FOUND 1 EA PUNCTURE. COMPLIED WITH EA: 6-5310-T0357997 P1. TITLE: FUSELAGE-MAINFRAME-PUNCTURE ON PRESSURE FLOOR PANEL BETWEEN FR 39 AND FR 40 AT Y-2354-REPAIR. REPAIRED THE HONov 12, 2020 · N728FD · Airbus A300B4622RSDR A6WA202011137416Structure · corrodedT-CAP EXTRUSION AT FS 574 T0 FS 605+10 CORRODED. AIRCRAFT REMOVED FROM SERVICE. REPLACE CORRODED T-CAP EXTRUSION AT FS 574 T0 FS 605+10 LBL 27, IAW BOMBARDIER DRWG 601R35031 REV P.Nov 12, 2020 · N454AW · Cndair CL6002B19SDR SWAA2021071529401Web · corrodedFWD CARGO CENTER THRESHOLD WEB CORRODED IN SEVERAL AREAS. / DAMAGE WAS FOUND TO BE OUT OF LIMITS PER SRM 53-30-15-1A-1. REPLACED WEB PER SRM 51-40-02. (SA-M 326 A1200878)Nov 11, 2020 · N8329B · Boeing 7378H4SDR SWIA202054337Angle · crackedRT 280 CROSSBEAM CLIPS ARE CRACKED AROUND RBL 9 FLOORBEAM. C-CHECK RO 11/23/2020. REMOVED AND INSTALLED NEW RT 280 CROSSBEAM CLIPS AT RBL 9 FLOORBEAM, REF CRJ200 SRM AND DWG. COMPLIED WITH TASK CARD.Nov 11, 2020 · N907SW · Cndair CL6002B19SDR SWIA202054336Angle · crackedLT 280 CROSSBEAM CLIPS ARE CRACKED AROUND LBL 9 FLOORBEAM. C-CHECK RO 11/23/2020. REMOVED AND INSTALLED NEW LT 280 CROSSBEAM CLIPS AT LBL 9 FLOORBEAM, REF CRJ200 SRM AND DWG. COMPLIED WITH TASK CARD.Nov 11, 2020 · N907SW · Cndair CL6002B19SDR DALA2020111203691Structure · crackedDURING INSPECTION MAINTENANCE FOUND A CRACK ON 624 AND STRINGER 16L. CRACK REPAIRED, PER ERA 588549-14.Nov 11, 2020 · N588NW · Boeing 757351SDR CALA2020111101259Pressure Panel · crackedCRACK INDICATION FOUND AT OUTBOARD FASTENER HOLE OUTSIDE OF REPAIR AREA FR 35 LT PRESSURE PANEL, REF EA-5330-05216 REV "B", REF AAR N/R: 9469368 GENERATED BY: V903469. ACCOMPLISHED INTERIM REPAIR PART 1, AS PER ECRA 5330-06774 AND EA 5330-05216 REV B ON OR BENov 11, 2020 · N457UA · Airbus A320232SDR SWIA202054806Tie Clip · corrodedSTRINGER TIE AT FS STA 661+90 TO 667 STGR 19R CORRODED. C-CHECK RO 12/26/2020. STRINGER TIE AT FS 661+90-667 AND 19R REMAINING MATERIAL IS BEYOND ALLOWABLE DAMAGE LIMITS. REMOVED AND INSTALLED NEW 19R STRINGER TIE AT FS 661+90 AND 667, REF CRJ 900 SRM AND DNov 10, 2020 · N802SK · Cndair CL6002D24SDR SWAA2020121429498Crease Beam · corrodedCORROSION, MAIN CABIN FLOOR CREASE BEAM INNER CHORD AT FASTENERS HEAD RBL 55 STA 616 &STA 639, MARKED DOTS 60-023. REMOVED AND INSTALLED NEW CREASE BEAM INNER CHORD AT MAIN CABIN FLOOR BETWEEN STA 626 TO STA 673 RBL 55', REF B737-7 SRM 51-40-0G-0 AND DWG NR 1Nov 10, 2020 · N432WN · Boeing 7377H4SDR SWIA202054551Intercostal · corrodedINTERCOSTAL DD1 IS CORRODED IN SEVERAL LOCATIONS (NOTED AFTER INTERNAL SKIN WAS REMOVED). C-CHECK RO 12/05/2020. PAX DOOR MID DD1 INTERCOSTAL ORIGINAL MATERIAL THICKNESS IS 0.050", IAW CRJ 200 SRM. EXFOLIATED CORROSION AT MULTIPLE LOCATION AND MORE TWO ELEMNov 10, 2020 · N939SW · Cndair CL6002B19SDR SWIA202054550Intercostal · corrodedINTERCOSTAL DD2 IS CORRODED IN SEVERAL LOCATIONS (NOTED AFTER INNER SKIN WAS REMOVED). C-CHECK RO 12/05/2020. PAX DOOR MID DD2 INTERCOSTAL ORIGINAL MATERIAL THICKNESS IS 0.050", IAW CRJ 200 SRM. EXFOLIATED CORROSION AT MULTIPLE LOCATION AND MORE TWO ELEMENTNov 10, 2020 · N939SW · Cndair CL6002B19SDR AALA202011109014Expansion Joint · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN EXPANSION JOINT AT STA 540 AND BL 0, MEASURING L=0.75 IN, W=0.002 IN, D=0.04 IN. REPLACED EXPANSION JOINT WITH NEW IAW SRM 51-10-02.Nov 9, 2020 · N962NN · Boeing 737823SDR R61A2020112800814Access Door · corrodedCF III WASTE ACCESS DOOR HAS CORROSION. REPLACED IAW AMM 53-03-60-440-801-A.Nov 9, 2020 · N731YX · Emb ERJ170200LRSDR DALA2020111103670Window Post · crackedCRACK INDICATION ON FRAME 4 WINDSHIELD SIDE POST RT SIDE LOWER ATTACHMENT. CORRECTIVE ACTION: PERFORMED REPAIR IN CONJUCTION WITH CARD 5311-01230-01B.Nov 9, 2020 · N369NB · Airbus A319114SDR 2020F00441Support Frame · crackedNOSE LANDING GEAR WHEEL WELL FRAME CRACKS.Nov 9, 2020 · N542Q · Cessna 680ASDR 2A6D20201109001Deck Plate · dentedA/C 4613 HAS SEVERAL DENTS LOCATED ON THE ENGINE DECK LOCATED AT APPROXIMATELY STA 4387, WL 1759, AND BL 650L. THE DAMAGE IS IN AN AREA 2.4 BY 1.8 WITH THE DEEPEST DENT MEASURING .045. THE DENTS ARE LOCATED ABOVE A FRAME WHICH IS UNDAMAGED.Nov 9, 2020 · N574AM · Snias AS350B3SDR SWAA2021040728828Pressure Deck · damagedFLIGHT DECK FLOOR DAMAGED / INSTALLED REPAIR AT FLIGHT DECK FLOOR FABRICATED TWO (2) DOUBLERS MAT USED 2024 T3 .050 PO# 1484683 AND ONE WEB MAT USED 2024 T3 .040 PO# 1691232; TREATED AND PRIMED REPAIR AS PER B737-7 SRM 51-40-02-0G-0; 51-20-13-0G-0; 51-30-01; 5Nov 8, 2020 · N432WN · Boeing 7377H4SDR SWIA202054547Door Frame · corrodedPAX DOOR FRAME FS 313.56 AND CLEAT HAS CORROSION. C-CHECK RO 12/05/2020. REMOVED FS 313.56 PAX DOOR FRAME & CLEAT. BLENDED CORROSION TO A SMOOTH CONTOUR. REMAINING MATERIAL ON FS 313.56 FRAME WITHIN LIMITS & CLEAT WAS NOT. REINSTALLED FS 313.56 PAX DOOR FNov 7, 2020 · N939SW · Cndair CL6002B19SDR DALA2020111103685Door Frame · corrodedDURING INSPECTION FOUND CORROSION ON LOWER DOOR JAMB LT AFT EMERGENCY EXIT. CORROSION ON LOWER DOOR JAMB LT AFT EMERGENCY EXIT WAS REMOVED, PER B737-800 SRM 51-10-02-0G PAR 15 AND SRM 53-40-15-1A-1.Nov 7, 2020 · N383DN · Boeing 737832SDR DALA2021070203672Window Frame · crackedSHIP 3277 CRACK INDICATION ON FRAME 4 WINDOW LH SIDE POST LOWER ATTACHMENT INTERNAL SIDE IN COCKPIT. CORRECTIVE ACTION: REPAIRED PER DELTA WORKCARD AMDS 5311-01230-01A. (1649492)Nov 6, 2020 · N377NW · Airbus A320211SDR SWIA202054968Pressure Deck · crackedPRESSURE FLOOR SKIN HAS 2.5 INCH CRACK AT FS 461 BETWEEN BL 0 AND RBL 9. C-CHECK RO 12/30/2020. REMOVED DAMAGE IN PRESSURE FLOOR SKIN AT FS 461 BETWEEN BL 0 AND RBL 9, IAW REO. COMPLETED TASK CARD AND ATTACHED COMPLETED FORM 337. WEIGHT CHANGE NEGLIGIBLE.Nov 6, 2020 · N924SW · Cndair CL6002B19
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