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.
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
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 SWAA2022030445765Web · dentedFLIGHT DECK FLOOR AFT WEB HAS MULTIPLE DENTS/CREASES. EA 1-753-34306 PROVIDED INITIAL 30 DAY TIME-LIMITED REPAIR. EA 1-753-34411 PROVIDES AN EXTENSION AFTER A DVI OF THE UNDERLYING STRUCTURE IS ACCOMPLISHED / REMOVED DAMAGED SECTION OF FLIGHT DECK FLOOR. INSTASDR SWAA2022030465648Channel · crackedCABIN FLOOR BS 540 RBL 1' CABIN FLOOR BOARD SUPPORT CHANNEL CRACKED. / REMOVED; LOCATED; DRILLED AND INSTALLED B5540 RBL 1' CABIN FLOOR BOARD SUPPORT CHANNEL IAW SRM 51-40-02; 51-40-05 AND IPC 53-42-11-66. REMOVED AND REINSTALLED FLOOR BOARD 231UF IAW AMM 53-2SDR SWAA2022030465649Channel · crackedCABIN FLOOR BS 540 LBL 1' CABIN FLOOR BOARD SUPPORT CHANNEL CRACKED. / REMOVED COATED AND DRILLED AND INSTALLED BS540 LBL 1' CABIN FLOOR BOARD SUPPORT CHANNEL IAW SRM 51-40-02; 51-40-05 AND BOEING DWG 143A5240. REMOVED AND REINSTALLED FLOOR BOARD 231UF IAW AMMSDR SWAA2019050232142Crease Beam · corrodedCREASE BEAM WEB CORRODED BETWEEN BS. 500C TO BS. 500D, RBL 67. R&R CREASE BEAM WEB PER ER & EA.SDR AALA201904129028Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON CORNER FITTING AT FR 68 AND S23R. REPLACED CORNER FITTING PER SRM 51-42-11 AND 51-72-11.SDR CALA2019040100498Pressure Panel · crackedAD RELATED AD 2018-06-04, RESULTS OF ROTO-TEST ON TC 14332, FOUND 3RD & 4TH HOLES FROM LH OB END ALONG FR36 CRACK IND IN PRESSUR E PLATE LAYER "CONTACT ENG FOR REPAIR INSTRUCTIONS & REPAIR BEFO RE NEXT FLIGHT" PER HAECO LCQ NR 9292516, GEN. BY MECH V892444 HAESDR CALA2019040100495Door Frame · crackedEMERGENCY EXIT LT AFT 834. IB FWD VERTICAL FRAME CRACKED AT FAST ENER HOLES. AAR NONROUTINE 9817724 REMOVED AND REPLACED FWD VERTICAL FRAME (BEAM AND SEGMENT) ON L/ H AFT EMERGENCY EXIT DOOR IAW A320 SRM 51-72-11-911-001. AAR NON ROUTINE 9817724 INSPECTION COMSDR CALA2019040100493Beam · crackedEMERGENCY EXIT LT AFT 834. IB AFT VERTICAL FRAME CRACKED AT FAST ENER HOLES. AAR NONROUTINE 9817723 REMOVED AND REPLACED EMERGENCY EXIT LT AFT 834 IB AFT VERTICAL F RAME IAW A320 SRM 51-72-11-911-001. AAR NONROUTINE 9817723 INSPECTION COMPLIED WITHSDR DALA2019032902052Door Frame · crackedCRACK INDICATION ON PASSENGER CREW DOOR CUTOUT AT FRAME 68 AFT FACE BE LOW THE STR 8L IN THE RADIUS AREA OF THE FRAME IN PASSENGER CABIN (1 EA). (CRACK LENGTH = 0.275 IN. APPROX). PERFORMED REPAIR LOCATED ON PASSENGER CREW DOOR CUT OUT AT FR 68 AFT FACE BELOW SDR EE4Y2019032908566Door Frame · crackedFR16 FRAME LT DOOR STOP FITTING NR 1 HOLE WITH CRACK INDICATION. FOR CORRECTIVE ACTION SEE NRI 2-142. ACTION TAKEN, PERFORMED PERMANENT REPAIR AT FR16 LT DOOR STOP FITTING DUE TO CRACK. SEE EO Nº COO-EO-2019-7849 R00 AND DOSSIER NUMBER: 80567937.SDR SWAA2022030405442Skin · bentAFT CARGO DOOR FUSELAGE CUT OUT; FWD EDGE; FUSELAGE SKIN BENT AND DEFORMED IN TWO PLACES APPROXIMATELY 19' FROM LOWER EDGE OF CUT OUT JUST ABOVE LAP SEAM / REPAIRED IAW EA 1-753-34531.SDR SWAA2022030405443Skin · gougedAFT CARGO DOOR FUSELAGE CUT OUT; FWD EDGE; FUSELAGE SKIN BENT AND GOUGED WITH MATERIAL MISSING IN TWO PLACES ON INNER SURFACE APPROXIMATELY 19' FROM LOWER EDGE OF CUT OUT JUST ABOVE LAP SEAM / REPAIRED IAW EA 1-753-34531.SDR SWAA2019050832477Door Frame · crackedABOVE ENTRY DOOR FRAME CRACKED AT BS. 312, STR. 5L. REPAIRED FRAME IAW ER AND EA.SDR AALA201904269037Stop Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED INTERCOSTAL FITTING AT FR 16 RIGHT HAND AT THE #7 DOOR STOP FITTING. REPLACED INTERCOSTAL FITTING PER SRM 51-72-11.SDR ASAA2019042382913Beam · corrodedMAIN CABIN LWR DOOR SILL SUPPORT AT R-2 DOOR, FWD OF FR68 HAS ACORRODED EXISTING REPAIR GROUNDED - YES. REMOVED DAMAGED REPAIR IAW A320 SRM 51-42-11. FABRICATED NEW REPAIR AND 2 EACH FILLERS IAW A320 SRM 53-41-14-300-001. INSTALLED REPAIR AND 2 EACH FILLERSDR UIEA2019032903700Web · corrodedREPAIR - CORROSION DAMAGES ON THE REAR SPAR WEB AT STA 1241 LBL 91(<P>1. REPAIR DAMAGE AREA IAW EI NO. T2019A57M-1307 REV.1</P><P>2. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)SDR SWAA2022030438577Support · corroded***CORROSION*** ON FRAME TO SKIN ANGLE SUPPORT STA 1088+13 WL 224 STR 20R; 26 INCHES BELOW LOWER HORIZONTAL DECK (MARKED) / REMOVED DAMAGE ON FRAME TO SKIN ANGLE SUPPORT BS 1088+13' W/L 224 STR 20R AND REPAIRED IAW ATS ER # 19-02755 REV IR AND SWA EA # 1-753-3SDR SWAA2022030465107Support · crackedPASSENGER COMPARTMENT; LATERAL FLOOR SUPPORT IS CRACKED AT STA 540; LBL1 / REMOVED FLOOR BOARD 231VF IAW B737 AMM 53-21-00-000-801. REMOVED AND REPLACED FLOOR SUPPORT AT STA 540 LBL 1 IAW B737 SRM 51-40-02-0G-0 AND SRM 51-40-05-0G-0 REINSTALLED FLOOR BOARD 231SDR AALA2019042309901Beam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON FASTERNER HOLE OF LONGITUDINAL BEAM AT PRESSURE PANEL LEFT HAND SIDE OF FR 36. REPAIRED LONGITUDINAL BEAM PER TASK CARD 5316Y209002.SDR ASAA2019042372991Door Frame · corrodedL1 DOOR LOWER FRAME AT GIRT BAR LOCATION FWD HAS CORROSION (MARKED IN RED) GROUNDED - YES. REMOVED CORROSION ON L1 LOWER DOOR FRAME AT FWD GIRT BAR PER A320 SRM 53-11-14-283-005, A320 SRM 51-74-00, A320 SRM 51-74-00. ORIG. THICK .197 REMAINING .181 REMOVED .01SDR ASAA2019042372990Door Frame · corrodedR1 DOOR LOWER FRAME AT GIRT BAR304 LOCATION FWD AND AFT HAS CORROSION (MARKED IN RED) GROUNDED - YES. REMOVED CORROSION ON R1 DOOR LOWER FRAME AT FWD AND AFT GRIT BAR LOCATIONS PER A320 SRM 53-11-14-283-005, A320 SRM 51-74-00, A320 SRM 51-74-00. ORIG THICK .18SDR C77A2019032700001Beam · corrodedDURING THE B5 BASIC CHECK AT EAMS, CORROSION DAMAGE WAS DISCOVERED ON THE AFT PASSENGER (L2) DOOR THRESHOLD LOWER BEAM (P/N 170-65703-005) AT SEVERAL FASTENER HOLES AROUND THE FORWARD AND AFT GIRT BAR FITTINGS. A TEMPORARY REPAIR OF THE BEAM WAS ACCOMPLISHED PSDR SWAA2022030425952Strap · corroded***CORROSION*** ON TENSION STRAP AT STA 1016+13 RBL 18 WL 208 / REMOVED AND REPLACED TENSION STRAP FROM BS 1016 TO BS 1028.5 WL 208 RBL 18 IAW SRM 51-40-02 AND DWG 147A5730.SDR SWAA2022030476333Angle · corrodedAFT CARGO COMPARTMENT FLOOR R/H SIDE Z-ANGLE HAS CORROSION STA 887 TO 947 / REMOVED CORROSION ON AFT CARGO R/H 'Z' ANGLE STA 887-947 ORIG T.040 REMOVED .08; REMAINING .032' OUT OF LIMITS I/A/W SRM 53-00-53-1A-2. REPLACED 'Z' ANGLE R/H SIDE FROM STA 881-947 I/ASDR SWAA2022030476331Angle · corrodedAFT CARGO COMPARTMENT R/H SIDE Z-ANGLE HAS CORROSION STA 867 TO 887 / REMOVED AND EVALUATED CORROSION ON AFT CARGO R/H 'Z' ANGLE STA 867-887 FOUND TO BE OUT OF LIMITS I/A/W SRM 53-00-53-1A-2 USING AAR TOOL# 38294 CAL DUE 5/1/19. ORIG 'T' .032'; REMAINING .012'SDR SWAA2022030476316Angle · corrodedAFT CARGO COMPARTMENT FLOOR R/H SIDE Z-ANGLE IS CORRODED STA 727 TO 767 / EVALUATED CORROSION ORIGINAL THICKNESS .040' LOSS OF .012' WITH 028' REMAINING. BLEND FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. REMOVED AND REPLACED RH 2-ANGLE STA 727-767 PER SRMSDR SWAA2019050732367Crease Beam · corrodedL1 DOOR WAY LOWER SILL CREASE BEAM INNER CHORD VERTICAL FLANGE CORRODED BETWEEN BS. 323 TO BS. 344, LBL 60. R&R L1 DOOR CREASE BEAM IAW DWG.SDR SWAA2019042931955Pressure Deck · crackedHORIZONTAL PRESSURE DECK CRACKED AT BS. 665, RBL 40. / REPAIRED WEB IAW SRM.SDR ASAA2019042352912Beam · corrodedAFT MAIN CABIN, R-2 DOOR THRESHOLD. DOOR SILL SUPPORT BEAM CORROSION AFT END. GROUNDED - YES. BLENDED CORROSION IAW A320 SRM 53-41-14-283-002. ORIG MAT .071 REMAINING MAT .0. 100% MAT. LOSS. REPAIRED AREA IAW A320 SRM 53-41-14-300-001. THIS IS A CATEGORYSDR ASAA2019042352988Beam · corrodedAFT MAIN CABIN, FLOOR BEAM, BUTT LINE 8 L. JUST FORWARD OF FRAME 70, CORROSION ON TOP GROUNDED - YES. CORROSION LOCATED AT A HARD POINT AREA WHICH IS A EXCLUDED AREA REQUIRING BEAM REPLACEMENT, REF. A320 SRM 53-00-14-283-002, FIG 001 (SHT 1) REMOVED DAMAGED BESDR SWAA2019042331991Door Frame · corroded*APU COMPARTMENT L/H DOOR CUTOUT STRUCTURE CORRODED AT STA 1088+8 TO 1088+68, LBL 24 / REMOVED AND REPLACED APU DOOR CUTOUT CHORD IAW SRM 51-40-02-0G-0, BOEING DWG 148A8600 AND BOEING DWG 148A8540SDR ASAA2019042252957Support Beam · corrodedAFT MAIN CABIN, L-2 DOOR THRESHOLD. DOOR SILL SUPPORT BEAM CORROSION AFT END. GROUNDED - YES. BLENDED CORRODED AREA. ORIGINAL MAT. THICKNESS .071, REMOVED .016, REMAINING .055. FOUND TO BE OUT OF LIMITS AS PER SRM 53-41-14-283-002. FABRICATED REPAIR ANGLE IAWSDR CA190326012Doubler · cracked(CAN) DEFECT- DURING HMV INSPECTION, CRACK FOUND ON LH TEAR STRAP DOUBLER PN S53172101204 AT FRAME 7 OF NLG. W/O 33424191 NR 00027. INSPECTION TASK CARD 425-ZL-115-GVI-10000-1 CORRECTIVE ACTION: PARTS REPLACEMENT (TC# 20190326012)SDR AALA201904109027Stop Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED #1 DOOR STOP FITTING UPPER INBOARD FASTENER HOLE AT FR 66 AND S10R. REPAIRED DOOR STOP FITTING PER SRM 53-41-12-300-010.SDR SWAA2019032631084Crease Beam · corrodedRT CREASE BEAM CORRODED AT BS 767+2, STR 17R. R&R CREASE BEAM IAW SRM.SDR VNAA2019032499908Beam · crackedUPON REMOVAL OF AFT CARGO FLOOR LANDING PLATE FOUND TRAVERSE BEAM AT FS 589, OUTBOARD OF LBL 27, CRACKED IN RADIUS. CORRECTIVE ACTION: COMPLIED WITH REO 601R-53-61-6908 REV.-- DATED 2019-03-15.SDR SWAA2022030437040Web · corroded**CORROSION** AFT CARGO COMPT CARGO DOOR CUTOUT SURROUND STRUCTURE FROM STA 787 TO STA 878 FROM RBL 19 TO RBL28 WL162 WEB HAS MULTIPLE CORRODED AREAS. / REMOVED + REPLACED AFT CARGO COMPT CARGO DOOR CUTTOUT SURROUND STRUCTURE FROM BS 787 TO BS 878 RBL 19 - RBLSDR REXA2019040823413Crossbeam · crackedAWR: HIDDEN DAMAGE: DURING REMOVAL OF LH DRIP TRAY THE FS.280 CROSS BE AM WAS FOUND CRACKED AT LBL 15.IN REF TASK CARD R53581 STEP 21. CROSS BEAM WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 PAR. 6. AND CRJ900 SRM 51-42-20-001-001-A01SDR SWAA2022030471301Angle · corroded***CORROSION*** AFT CARGO FLOOR TO SIDEWALL TRANSITION STA 785-797 LBL21 WL156 / CORROSION AT BS790 FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY TO A FASTENER HOLE IAW SRM 53-00-53-1A-2 FIGURE 103 DETAIL D. REMOVED AND REPLACED AFT CARGO FLOOR TO SIDEWALL TRANSISDR SWAA2022030445874Gusset · crackedFWD CARGO AT BS 500I GUSSET CRACKED AT S19RH. / REMOVED AND REPLACED GUSSET AT FWD CARGO AT B.S. 500I STR 19RH; P/N 143A7902 ATAG A30211 IAW B737-700 DWG 143A7902 REV B AND SRM 51-40-02-0G-0SDR SWAA2022030445889Angle · corrodedAFT PIT RH Z-ANGLE STA 767 TO 787 IS CORRODED AND HAS 2 EA DRILLED OFF SCREWS / AFT CARGO PIT SHIELD AT STA 767 T 287 WAS CORROED OUT OF LIMITS IAW SRM 53-60-15-1A-1. REMOVED AND REPLACED WITH NEW ONE IAW BOEING 737 SRM 51-40-02 AND BOEING DWG 146A0081 REV A. SDR SWAA2022030445883Angle · corrodedAFT PIT RH Z-ANGLE STA 727D TO 767 HAS SPOTS OF CORROSION AND TOOLING DAMAGE / REMOVED DAMAGE ON AFT CARGO R/H Z-ANGLE FROM STA. 727D TO 767 AND VERIFIED LIMITS (DEEPEST SPOT LOSS:.010) (ORIGINAL T:.040) (REMAINING:.030) FROM STA 727J TO 767 OUT OF LIMITS IAW SDR AALA201906039030Door Frame · crackedAIRCRAFT IN BASE VISIT: APPROX. 0.080" CRACK I/B LOWER (#3) HOLE IN #1 DOOR STOP FITTING AT FR 16L. REMOVED STOP FITTING AND INTERCOSTAL FOR ACCESS. REMOVED CRACK BY REAMING HOLE. INSTALLED BUSH REPAIR. REINSTALLED STOP FITTING AND INTERCOSTAL IAW COOPESA EO #SDR SWIA201904250785Support Beam · chafedCARGO DOOR SUPPORT BEAM HAS CHAFE MARK ON FWD AND AFT LOWER CHANNEL. (C-CHECK) RO: 04/21/2019 REMOVED AND INSTALLED NEW CARGO BEAM SUPPORT ANGLE IAW SRM AND REO. PRESSURE CHECK GOOD.SDR SWAA2022030497668Panel · corrodedFWD CARGO BIN RT TRANS ANGLE CORRODED STA 492 TO 500A. / R/R TRANSITION ANGLE PN # 143A8126-20 PER SRM.51-40-02SDR SWAA2022030497666Angle · corrodedFWD CARGO BIN LT TRANS ANGLE CORRODED STA 500 TO 500D. / REPAIRED SECTION OF L/H TRANSITION ANGLE FROM STA. 480+8 TO STA.500D MATERIAL REPAIR #BAC1496-444 ; PER SRM 53-0053-2R-6SDR SWAA2022030497664Angle · corrodedFWD CARGO BIN RT TRANS ANGLE CORRODED STA 436 TO 440. / REMOVED TRANSITION ANGLE (MPN 143A8126-22) AND INSTALLED NEW 143A8126-22 ANGLE PER SRM 51-40-02. SEE TASKS AND WIPS FOR INDIVIDUAL SIGNOFFS.SDR SWAA2022030497659Angle · corrodedAFT CARGO RIGHT TRANSITION ANGLE HAS MULTIPLE AREAS OF CORROSION FROM STA 767-787 / REMOVED CORROSION AFT CARGO RIGHT TRANSITION ANGLE FROM STA 767-787 PER SRM. 51-10-02 ; MATERIAL FOUND TO BE OUT OF LIMITS PER SRM. 53-00-53-1A-2 ; REMOVED AND REPLACED PART # SDR CALA2019032200446Beam · wornCOMPLETE REPAIR PER SRM 53-11-14-283-005 FIG 1 AT R1 SILL BEAM WHERE FWD GIRT FITTING MOUNTS INCLUDING MATERIAL REMAINING BY BOLT HOLES, SPOT FACE AT BOLT HOLES, BUSHINGS IF NEEDED, NDT ROTO CHECK OF HOLES. REF N/R 99830719 REF. N/R:99830831 CLEANED AREA FOR NSDR CALA2019032200445Beam · wornCOMPLETE REPAIR PER SRM 53-11-14-283-005 FIG 1 AT L1 SILL BEAM WHERE AFT GIRT FITTING MOUNTS INCLUDING MATERIAL REMAINING BY BOLT HOLES, SPOT FACE AT BOLT HOLES BUSHINGS IF NEEDED, NDT ROTO CHECK OF HOLES, REF N/R 99830717 REF N/R:99830829 CLEANED AREA FOR NDT
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