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 SWAA2022032186183Stringer · out of toleranceWHILE ACCOMPLISHING SI#12107-53 FOUND HOLE 9L AT STR-3L OUT OF THE 0.3745-0.3755 TOLERANCE REQURED FOR STEP 29.D. EXISTING WHOLE DIAMETER 0.380. / REPAIRED FASTNER HOLE AT BS 1016; STRINGER 3L; HOLE 9L AS PER SOUTHWEST SPECIAL ITEM (SI # 12107 # 53) STEP 31 RESDR FDEA2019110792887Structure · corrodedUPPER CARGO COMPT UNDER FLOOR NEAR STA 1225 LBL 42-45. STRUCTURE EXFOLIATED. ALL WORK COMPLIED WITH ACCORDING TO E.A.# 1-5730-T0350197. TILLE: WING-PLATES AND SKINS- CENTER WING UPPER SKIN PANELS- STRINGER 15.SDR FDEA2019110792886Structure · corrodedUPPER CARGO COMPT UNDER FLOOR NEAR STA 1225 LBL 36-37. STRUCTURE EXFOLIATED. ALL WORK COMPLIED WITH ACCORDING TO E.A.# 1-5730-T0350197. TILLE: WING-PLATES AND SKINS- CENTER WING UPPER SKIN PANELS- STRINGER 15.SDR FDEA2019110792884Structure · corrodedUPPER CARGO COMPT UNDER FLOOR NEAR STA 1225 LBL 18-20. STRUCTURE EXFOLIATED. ALL WORK COMPLIED WITH ACCORDING TO E.A.# 1-5730-T0350197. TILLE: WING-PLATES AND SKINS- CENTER WING UPPER SKIN PANELS- STRINGER 15.SDR ABXA20190919153Beam · damagedDAMAGE ON THE CENTER WING BOX LOWER BEAM, LOWER CHORD BETWEEN FUSELAGE STATIONS 900 AND 925. THE CHORD WAS REPAIRED. THE AIRPLANE WAS GROUNDED.SDR SWAA2022032146777Support · corroded***CORROSION*** FWD CARGO BAY AFT BULKHEAD TO L/H SIDEWALL SUPPORT AT STA 500I HAS CORROSION FROM LBL 24 TO LBL 43 WL 156 / AFTER EVALUATION OF DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 TABLE 101 PARA 4.A(2) DETAIL E. REMOVED AND REPLACED AFT L/H SDR SWAA2022032146778Support · corroded***CORROSION*** FWD CARGO BAY AFT BULKHEAD TO R/H SIDEWALL SUPPORT AT STA 500I HAS CORROSION FROM RBL 24 TO RBL 43 WL 156 / AFTER EVALUATION OF DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 TABLE 101 PARA 4.A(2) DETAIL E. REMOVED AND REPLACED FWD CARGSDR C77A2020011100019Beam · corrodedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIRS OF CORROSION DAMAGE BY REPLACEMENT OF THE FOLLOWING AFT CABIN FLOOR STRUCTURE: P/N 170-92856-001 FLOOR DOUBLER, P/N 170-66796-001 LH PANEL SUPPORT, P/N 170-91919-001 RH SHEAR PSDR FDEA201909182752Structure · corrodedUPPER CARGO COMPT UNDER FLOOR NEAR STA 1260 AT RBL 105 STRUCTURE EXFOLIATED. REPAIRED CORROSION FOUND AT UPPER CARGO COMP UNDER FLOOR AREA NEAR STATION 1260 RBL105 REF E.A 1-5730-T0350234 P1. TITLED "WING-PLATES AND SKINS-CENTER WING- UPPER SKIN-REWORK" ASDR FDEA2019121382687Structure · corrodedUPPER CARGO COMPT UNDER FLOOR NEAR STA 1235 AT LBL 106 STRUCTURE EXFOLIATED.SDR R61A2019100498153Beam · corrodedDURING HEAVY CHECK, MAINTENANCE FOUND AFT SERVICE DOOR LOWER BEAM IS CORRODED AT FORWARD AND AFT GIRT BAR FLOOR FITTINGS, AND AT CENTER OF BEAM, FRAMES 85-87. REMOVED AND REPLACED AFT SERVICE DOOR LOWER BEAM PER SRM 51-40-08, 51-23-05, 51-23-06.SDR DALA2019091905426Door Frame · crackedCRACK INDICATION ON FRAME 68 UPPER CORNER AFT FACE AT LEVEL STR 8L PASSENGER CREW DOOR CUTOUT APPROX L= 0.625IN AT AFT GALLEY AREA. REPAIR FRAME 68 UPPER CORNER AFT FACE AT LEVEL STR 8L PASSENGER CREW DOOR ASPER ER/A NR 580967-14AD SECTION 1 REV ORIGINAL AND ASDR SWAA2022032112732Angle · corrodedFWD PIT RIGHT Z ANGLE CORRODED UPPER SURFACE STA 500C-500D RBL 24 W/L 157. / REMOVED AND REPLACED FWD PIT R/H Z ANGLE STA 500C-500D RBL24 W/L 157 IAW SRM 51-40-02-0G-0; DWG 143A7500 ID: 0058. OUT OF LIMITS IAW SRM 53-00-53-1A-2 ORIGINAL 'T' .040 LOSS OF .012 RSDR SWAA2022032146742Support · corroded***CORROSION*** FWD CARGO BAY AFT BULKHEAD TO FLOOR SUPPORT AT STA 500I HAS CORROSION FROM LBL 24 TO RBL 24 WL 156 / REMOVED DAMAGED FLOOR SUPPORT FROM FWD CARGO BAY AFT BULKHEAD STA 500I LBL 24 TO RBL 24 WL 156; DAMAGED CORROSION FOUND OUT OF LIMITS PER S.R.MSDR SWAA2022032146764Gusset · crackedFWD CARGO GUSSET CRACKED STR 19R STA 500I / REMOVED DAMAGED GUSSET FROM FWD CARGO STA 500I STR 19R AND INSTALLED NEW PART PER S.R.M 51-42-02-0G-0 AND SEALED PER AMM 51-31-00-390-803SDR SWAA2022032146749Support · corroded***CORROSION*** ON AFT CARGO COMPARTMENT R/H FLOOR TO SIDEWALL SUPPORT FROM STA 727 - 767 RBL 21 WL 155 / AFT CARGO COMPARTMENT R/H FLOOR TO SIDEWALL SUPPORT HAS CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. REMOVED FLOOR TO SIDEWALL SUPPORT PSDR SWAA2022032146748Support · corroded***CORROSION*** ON AFT CARGO COMPARTMENT L/H FLOOR TO SIDEWALL SUPPORT FROM STA 727 - 847 LBL 21 WL 155 / AFT CARGO COMPARTMENT L/H FLOOR TO SIDEWALL SUPPORT HAS CORROSION AND FOUND TO BE OUT OF LIMITS SRM 53-00-53-1A-2. REMOVED FLOOR TO SIDEWALL SUPPORT PER SSDR C77A2020011100008Crossbeam · damagedDURING BASIC CHECK AT EAMS, CORROSION DAMAGE WAS FOUND TO THE FORWARD FUSELAGE FR11 COCKPIT CROSSBEAM. REFERENCE ETD2019-170-122405-A, FIGURE 1 FOR DETAILS. EAMS REQUESTED AND RECEIVED PERMANENT REPAIRS FOR THE DAMAGE IN THE FORM OF ETD2019-170-122405-A WHICH SDR R61A201909271004Beam · corrodedCORROSION STRUCTURAL CENTER FUSELAGE III WET AREA 53-23 RH BEAM Y=+10.748" FRAME 86-89. REMOVED AND REPLACED CENTER FUSELAGE III WET AREA 53-23 RH BEAM Y=+10.748" FRAME 86-89 PER SRM 51-40-08. SEE EAMS W/O H6968 SN 136 FOR WORK DETAILS. AIRCRAFT REMAINS IN HESDR CALA2019092301606Crease Beam · corroded(B757-53-3-0556) CORROSION ON MAIN CABIN LT CREASE BEAM INNER CHORD UPPER SURFACE STA 732-735 AS MARKED 50-032. REF N/R 0071663 BLENDED AND CHECK LIMITS TO LT CREASE BEAM INNER SHORD IN MAIN CABIN STA 732-735; L=3.5" W=1.0" A=.014". OUT OF LIMITS IAW SRM 53-30SDR SWAA2022032174941Web · corrodedAFT CARGO DOOR SILL WEB HAS CORROSION ON UPPER SURFACE BS 794 - BS 847 RBL20-28 WL158; MARKED. / REMOVED AND REPLACED AFT CARGO DOOR SILL WEB B5794-BS847 RBL 20-28 WL158 IAW BOEING DWG 146A8340 REV: A AND B737 SRM 51-40-05-0G-0. 51-40-02-0G-0SDR SWAA2022031739683Intercostal · crackedPASSENGER CABIN FWD WET AREA THERE IS AN INTERCOSTAL AT STA 312 TO STA 328 RBL 32' WITH CRACKED HOLE / REMOVED AND REPLACED INTERCOSTAL BETWEEN STA 312 AND STA 328 RBL 32' REF B737-7 SRM 51-40-02-0G-0 AND BOEING DRW #141A5400 SHEET 39SDR SWAA2022031886176Stringer · out of toleranceWHILE ACCOMPLISHING SI#12107-53 FOUND HOLE 7L AT S-3L OUT OF THE 0.312-0.3130' TOLERANCE REQUIRED PER THE SI ON STEP 19D. (EXISITING HOLE DIAMETER 0.317) / REPAIRED FASTENER HOLE AT BS 1016 STRINGER 3L HOLE 7L AS PER SOUTH WEST SPECIAL ITEM (SI # 12107-53) STESDR SWAA2022031886177Stringer · out of toleranceWHILE ACCOMPLISHING SI#12107-53 FOUND HOLE 8L AT S-3L OUT OF THE .0312- 0.3130 TOLERANCE REQUIRED PER THE SI ON STEP 19F. (EXISTING HOLE DIAMETER 0.319) / REPAIRED FASTENER HOLE AT BS 1016 STRINGER 3L; HOLE 8L AS PER SOUTHWEST SPECIAL ITEM (SI # 12107 # 53) STSDR SWAA2022031886178Stringer · out of toleranceWHILE ACCOMPLISHING SI#12107-53 FOUND HOLE 7R AT S-3R OUT OF THE 0.312- 0.3130' TOLERANCE REQUIRED PER STEP 24D. (EXISTING HOLE DIAMETER .315) / REPAIRED FASTENER HOLE AT BS 1016 STRINGER 3R HOLE 7R AS PER SOUTH WEST SPECIAL ITEM (SI # 12107-53) STEP 25 REF. FSDR SWAA2022031886179Stringer · out of toleranceWHILE ACCOMPLISHING SI#12107-53 FOUND HOLE 8R AT S-3R OUT OF THE 0.312- 0.3130' TOLERANCE REQUIRED PER THE SI ON STEP 24F. (EXISTING HOLE DIAMETER .315) / REPAIRED FASTENER HOLE AT BS 1016 STRINGER 3R; HOLE 8R AS PER SOUTHWEST SPECIAL ITEM (SI # 12107 # 53) STSDR AALA201911069019Door Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FORWARD RIGHT HAND DOOR CUT OUT FRAME AT FR 20 BETWEEN S10R AND S11R AT THE #7 DOOR STOP. REPAIRED FRAME PER EA 298911.SDR SWIA2019101846515Vertical Support · damagedFS409+128 BL0 VERT POST HAS INDICATIONS NOTED ON BOTH SIDES IN THE AFT FLANGE RADIUS AT WL69 GREATER THAN 50%FSH. L/H SIDE IS 0.350" LONG AND R/H SIDE IS 0.300" LONG. MARKED ON A/C. (C-CHECK) RO: 10/16/2019 REMOVED AND REPLACED F/S 409+128 BL 0 VERT POST IAW RSDR FDEA2019091762683Doubler · crackedR/H CENTER LANDING GEAR WHEEL WELL FWD KEEL BEAM MACHINE DOUBLER (AEA0526)HAS A CRACK ON THE AFT ANGLE BETWEEN THE FASTENER HOLES. REMOVED AND REPLACED MACHINE DOUBLER IN REF TO DWG AEA0526 AND SRM 51-31-01.SDR FDEA2019101462640Doubler · crackedLEFT CENTER LANDING GEAR WHEEL WELL FWD KEEL BEAM DOUBLER WAS CRACKED ON THE AFT ANGLE BETWEEN THE FASTENER HOLES. REMOVED AND REPLACED PER DWG AEA0526SDR CALA2019092301602Pressure Plate · crackedROTARY INSP FROM TASK CARD 14333 AT 35-36 FOUND 19 HOLES WITH CRACK INDICATIONS IN PRESSURE PLATE. HOLE 1,2,3,4,5,6,7,9,11,16,17 ,18,20,23,24,26,27,28 RT SIDE PER HGR NR 9294449. REPAIRED RT FR35-36 HOLES IAW SRM 51-42-11 REO L22287 REV IR ECRA 5331-02458 REV SDR AALA201909179036Door Frame · crackedAIRCRAFT IN BASE MAINTENANCE:L1 DOOR CUT OUT FRAME CRACKED AT FR 16 AND DOOR STOP #1. REPAIRED FRAME PER EA 298359.SDR DALA2019091605333Door Frame · crackedCRACK INDICATION ON PASSENGER CREW DOOR FRAME FASTENER HOLE NR 6. LOCATED AT FR16 UPPER DOUBLE JOGGLE AREA, LT SIDE. IN PASSENGER CABIN (1 EA). PERFORMED PERMANENT REPAIR ON PASSENGER CREW DOOR FRAME FASTENER HOLE N.6 LOCATED AT FR 16 UPPER DOUBLE JOGGLE AREA SDR DALA2019091605332Door Frame · crackedCRACK INDICATION ON PASSENGER CREW DOOR FRAME 16 STOP FITTING 7 AT UPPER INBOARD FASTENER HOLE. RT SIDE. IN PASSENGER CABIN (1 EA). PERFORMED PERMANENT REPAIR ON PASSENGER CREW DOOR FRAME 16 STOP FITTING 7 AT UPPER INBOARD FASTENER HOLE AS PER ER/A NR 580938 -SDR DALA2019091605331Door Frame · crackedCRACK INDICATION ON PASSENGER CREW DOOR FRAME 16 STOP FITTING 7 AT LOWER INBOARD FASTENER HOLE. RT SIDE. IN PASSENGER CABIN (1 EA). PERFORMED PERMANENT REPAIR ON PASSENGER CREW DOOR FRAME 16 STOP FITTING 7 AT LOWER INBOARD FASTENER HOLE AS PER ER/A NR 580738-1SDR DALA2019091605329Door Frame · crackedCRACK INDICATION ON FRAME 16 LH SIDE ON OPEN FASTENER HOLES LOWER IB AND UPPER IB AT DOOR STOP FITTING 7 (CRACK DIRECTIONS ARE: LOWER IB: 1, 3 AND 5 OCLOCK, UPPER IB: 1, 3 AND 5 OCLOCK) AT FWD GALLEY AREA (6 EA). REPLACED AFFECTED INTERCOSTAL FITTING LOC BTW FSDR SWAA2022032974880Angle · crackedFWD GALLEY DOOR CUTOUT AREA; SUPPORT ANGLE OUTBOARD OF INBOARD CREASE BEAM CRACKED AT AFT END; BS 291.5 - BS 295.5 RBL54 WL208; MARKED. / REMOVED AND INSTALLED NEW SUPPORT CLIP P/N: 141A8312-3 AT CABIN STA 291.5-295.5; RBL 54; WL 208 IAW B737-700 SRM 51-40-02-SDR FDEA2019102812755Structure · corrodedUPPER CARGO COMPT. UNDER FLOOR AREA NEAR STA 1250 RBL 105 STRUCTURE/AROUND FASTNERS SHOWING EXFOLIATTION AREA MARKED DOT 35 REPAIRED CORROSION FOUND AT UPPER CARGO COMP UNDER FLOOR AREA NEAR STATION 1250 RBL105 REF E.A 1-5730-T0350234 P1. TITLED "WING-PSDR FDEA2019109282753Structure · corrodedUPPER CARGO COMPT. UNDER FLOOR AREA, STRUCTURE/AROUND FASTNERS NEAR STA 1240 AT RBL 105 SHOWING EXFOLIATTION AREA MARKED DOT 39 REPAIRED CORROSION FOUND AT UPPER CARGO COMP UNDER FLOOR AREA NEAR STATION 1240 RBL105 REF E.A 1-5730-T0350234 P1. TITLED "WISDR FDEA2019110752891Skin · corrodedUPPER CARGO COMPT. UNDER FLOOR AREA, STRUCTURE/AROUND FASTNERS NEAR STA 1225 AT LBL 45 SHOWING EXFOLIATTION AREA MARKED DOT 38 ALL WORK COMPLIED WITH ACCORDING TO E.A.# 1-5730-T0350197. TILLE: WING-PLATES AND SKINS- CENTER WING UPPER SKIN PANELS- STRINGSDR FDEA2019110752883Structure · corrodedUPPER CARGO COMPT. UNDER FLOOR AREA, STRUCTURE/AROUND FASTNERS NEAR STA 1225 AT LBL 18 SHOWING EXFOLIATTION AREA MARKED DOT 37 ALL WORK COMPLIED WITH ACCORDING TO E.A.# 1-5730-T0350197. TILLE: WING-PLATES AND SKINS- CENTER WING UPPER SKIN PANELS- STRINGESDR FDEA2019110752882Structure · corrodedUPPER CARGO COMPT. UNDER FLOOR AREA, STRUCTURE/AROUND FASTNERS NEAR STA 1225 AT CENTER- LINE SHOWING EXFOLIATTION AREA MARKED DOT 36 ALL WORK COMPLIED WITH ACCORDING TO E.A.# 1-5730-T0350197. TILLE: WING-PLATES AND SKINS- CENTER WING UPPER SKIN PANELS- SSDR SWAA2019101637927Failsafe · corrodedUPPER SURFACE UPPER FAIL SAFE CHORD CORRODED AT BS. 260, BETWEEN LBL 33 TO RBL 33. / R&R "FAIL SAFE" CHORD IAW SRM AND DWG.SDR SWAA2019101637865Web · corrodedUPPER SURFACE VERTICAL WEB CORRODED AT BS. 260, BETWEEN BL 0 TO RBL 10. / REPAIRED WEB PER EA & ER.SDR SWAA2019101637864Web · corrodedUPPER SURFACE OF VERTICAL WEB CORRODED AT BS. 260, BETWEEN LBL 10 TO BL 0. / REPAIRED WEB PER EA AND ER.SDR AALA201909169059Window Post · crackedAIRCRAFT IN BASE MAINTENANCE: LEFT HAND CENTER FLIGHT DECK WINDSHIELD POST CRACKED. REPLACED WINDOW POST PER EA 296967.SDR AALA201909169058Window Post · crackedAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND CENTER FLIGHT DECK WINDSHIELD POST CRACKED. REPLACED WINDSHIELD POST PER EA 296968.SDR AALA201909169055Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: LEFT HAND CENTER FLIGHT DECK WINDSHIELD FRAME CRACKED AT FR 2 AND Y0. REPAIRED FRAME PER EA 296965.SDR FDEA2019110742890Structure · corrodedUPPER CARGO COMPT. UNDER FLOOR NEAR STA 1225 FROM RBL 75 TO NEAR RBL95 STRUCTURE/AROUND FASTNERS SHOWING EXFOLIATTION AREA MARKED DOT 23 ALL WORK COMPLIED WITH ACCORDING TO E.A.# 1-5730-T0350197. TILLE: WING-PLATES AND SKINS- CENTER WING UPPER SKIN PANSDR FDEA2019110742885Structure · corrodedUPPER CARGO COMPT UNDER FLOOR NEAR STA. 1225 RBL 62 STRUCTURE EXFOLIATED DOT 15 ALL WORK COMPLIED WITH ACCORDING TO E.A.# 1-5730-T0350197. TILLE: WING-PLATES AND SKINS- CENTER WING UPPER SKIN PANELS- STRINGER 15.
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