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.
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 SWAA2022060911102Support Angle · crackedCRACKED FLOOR SUPPORT ANGLE AT BS380+6 LBL12 WL 208 / [01] FLOOR SUPPORT ANGLE AT BS 380+6 LBL12 WL208 FOUND TO BE OUT OF LIMITS; NO SRM ALLOWABLE DAMAGE FOR THE AREA; REMOVED FLOOR SUPPORT ANGLE BS 380-400 LBL12 WL 208 PER SRM 51-10-02-0G-0 STEP 9 AND SRM 51-SDR IPXA2022052482448Adapter · delaminatedINSPECTION TYPE:C AFT CABIN SEAT TRACK ADAPTER AT FR 72 BETWEEN Y1456 AND Y1959 EXFOLIATED.REMOVED AND REPLACED CLS ADAPTER IAW-SRM 51-40-21.SDR IPXA2022052582483Crossbeam · bentINSPECTION TYPE:C CROSSBEAM AT FR48 -Y450 AND -Y953 IS BENT REMOVED AND REPLACED CROSSBEAM IAW SRM 51-40-21SDR IXXA20220524011Roller Tray · corrodedCORROSION ON SUPPORT BRACKET STA1175-1179 LBL2 WING LOCK TRAYSDR IXXA2022052407Shear Tie · corrodedCORROSION STA368 BETWEEN 39L-38LSDR SWAA2022070110581Web · crackedCRACK FLOOR STRUCTURE WEB LOCATED BTW BS 312 TO BS 328 AT LBL 46 AT PASSENGER CABIN 2022-265925 / [01] REPLACED WEB AND FASTENERS LOC. BS 312 TO BS 328 AT LBL 46 AT PASSENGER CABIN. IAW B737-700 SRM 51-10-02 ITEM 9. DRAWING 141A5400. REV. -;[02] CORRECTED STEPSDR SWAA2022070110580Web · crackedCRACK FLOOR STRUCTURE WEB LOCATED BTW BS 328 TO BS 344 AT LBL 47 AT PASSENGER CABIN 2022-265926 / [01] REPLACED WEB AND FASTENERS LOCATED BTW BS 328 TO BS 344 AT LBL 47 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 AND DRAWING 141A5400. SHEET 44; REV -.;[02] COSDR SWAA2022070110583Web · crackedCRACK FLOOR STRUCTURE WEB LOCATED BTW BS 312 TO BS 328 AT RBL 31 AT PASSENGER CABIN 2022-265929 / [01] REPLACED WEB LOCATED BTW BS 312 TO BS 328 AT RBL 31 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 AND DWG 141A5400; SHEET 20; REV.-;[02] CORRECTED STEP 1.<BR>SDR SWAA2022070110584Web · crackedCRACK FLOOR STRUCTURE WEB BTW BS 270 TO BS 294 AT BL 0 AT PASSENGER CABIN 2022-265930 / [01] REPALCED WEB AND FASTENERS LOC. BS 270 TO BS 294 AT BL 0 AT PASSENGER CABIN. IAW B737-700 SRM 51-10-02 ITEM 9 DRAWING 141A5400. REV.-;[02] CORRECTED STEP 1.<BR>REPALCESDR IPXA2022061483123Skin · wornINSPECTION TYPE:1CLH OUTER WING LOWER SKIN REAR SPAR LOWER CAP HAS AN OVERSIZE HOLE AT XORS=420.375.REPAIRED LH WING SKIN OVERSIZED HOLE IAW VT-SAA EA 011-5720-01-A9594 REV I/R AND UPS EO MD11-5730-83869-A (MINOR).SDR IPXA2022060682871Strap · corrodedINSPECTION TYPE:17/1FLIGHT DECK FLOOR SHEAR WEB SPLICE AT FS 297 RBL 2 HAS SURFACE CORROSION. REMOVED CORROSION ORIGINAL THICKNESS .100" REMAINING THICKNESS .095" SRM DOES NOT HAVE ALLOWABLE LIMITSREMOVED CORROSION PER EA 757-5310-27-A2937SDR IXXA2022061308Floor Support · damagedTOOLING DANAGE ON WEB AT STA 522SDR IPXA2022060682870Web · corrodedINSPECTION TYPE:17/1FLIGHT DECK FLOOR SHEAR WEB SPLICE AT FS 297 LBL 20 HAS SURFACE CORROSION. REMOVED CORROSION ORIGINAL THICKNESSS .100" REMAINING THICKNESS. .086" SRM DOES NOT HAVE ALLOWABLE LIMITS.REMOVED CORROSION PER EA 757-5310-27-A2937SDR VNAA202205251111Skin · distortedEA22-C7-53-101 (PERM REPAIR - AERODYNAMIC FILLER LOOSE FUSELAGE SKIN FS 220) / FINISHED THE PERM REPAIR OF THE AERODYNAMIC SMOOTHNESS OF THE FUSELAGE SKIN AT FS220 IAW EA 21-C7-53-128 REV B INSTRUCTIONS AND SRM 51-12-00. THIS CLEARS THE PERM REPAIR NO FURTHER SDR IPXA2022052382426None · crackedINSPECTION TYPE:CCLS ADAPTER AT FRAME 20 FRAME 20 APPROX -Y1959 BROKEN.INSTALLED NEW CLS ADAPTER IAW-SRM 51-40-21.SDR EE4Y2022052315569Skin Panel · nickedLOWER CENTER FUSELAGE I, EXTERNAL SKIN WITH NICKS LOCATED FROM FR29 AND FR30 BETWEEN STRINGER 26LH AND STRINGER 27LH. NOTA: THE FUSELAGE SKIN WAS REPAIRED AS PER EMBRAER INSTRUCTIONS. ( FOR ADDITONAL DETAILS SEE COOPESA JOB: A1M007 SPECIAL ITEM: 21-48 ).SDR EE4Y2022052315565Skin Panel · dentedUPPER FORWARD FUSELAGE EXTERNAL SKIN WITH DENT LOCATED AT FR20+10MM BETWEEN STRINGER 12LH AND STRINGER 13LH. NOTE: THE FUSELAGE SKIN WAS REPAIRED AS PER EMBRAER ETD2022-190-012471 GUIDELINES AS STATED IN COOPESA ENGINEERING ORDER NO: COO-EO-2022-15334 INSTRUCTSDR EE4Y2022052315567Skin Panel · dentedLOWER REAR FUSELAGE , EXTERNAL SKIN WITH DENT AND OIL CAN LOCATED AT FR95+310MM BETWEEN STRINGER 23LH AND STRINGER 25LH. NOTE: THE FUSELAGE SKIN WAS REPAIRED AS PER EMBRAER ETD2022-190-014171 REV:B GUIDELINES AS STATED IN COOPESA ENGINEERING ORDER NO: COO-EO-2SDR IXXA2022052301Skin Panel · corrodedFLC PDU TRAY 2L CORRODED UPPER AND LOWER SURFACESSDR FDEA202205221269None · noneFR54/54.2 LH NO.4 DUMMY SEAT TRACK SLOT GAP OVER GAP VALUE(A) 0.0393 INCHES(1.0MM) BUT LESS THAN 0.0846 INCHES(2.15MM).SLOT GAP ACTUAL VALUE 1.20MM. I.A.W A300-600 SRM 53-15-16-201 PARA 5A PAGE 201-210 FIG.201 PERFORM RAIL HOLE REPAIR ACCOMPLISHED.SDR SWAA2022061309991Web · corrodedCORROSION ON AFT CARGO DOOR CUTOUT LOWER MAIN SILL THRESHOLD WEB AROUND FASTENER NUTPLATE HOLES. STA 794 TO STA 847; RBL26. / [01] REMOVED CORROSION PER SRM 51-10-02. REMOVED .009 INCH OF MATERIAL AT THE FASTENER HOLE AT STA. 787+18 AND .017 INCH OF MATERIAL ASDR IPXA2022060782928Frame Angle · dentedINSPECTION TYPE:17/1LOWER AFT CARGO PIT AT FRAME 1540 LH SIDE BETWEEN STR 26L AND 27L HAS A .50" LONG BY .50" WIDE BY .050" DEEP DENT ON THE UPPER FLANGE OF FRAMEREPAIRED PER SRM 53-00-07-2R-5SDR IPXA2022052182331None · crackedINSPECTION TYPE:1C/3CENTER FUSELAGE BASE FRAME FITTING AT FR46 RH SIDE HAS A CRACK.ACCOMPLISHED MAJOR REPAIRED PER UPS EO A300-5310-46789-G APPENDIX K.SDR IPXA2022052182330None · crackedINSPECTION TYPE:1C/3CENTER FUSELAGE BASE FRAME FITTING AT FR46 LH SIDE HAS A CRACK.ACCOMPLISHED MAJOR PER UPS EO A300-5310-46789-G APPENDIX J.SDR AALA202205267496Web · gougedAIRCRAFT IN BASE MAINTENANCE: ELECTRICAL EQUIPMENT DOOR CUT OUT RIGHT WEB GOUGED LOCATED AT STA 330.62, STR 27R. REMOVED AND REPLACED WEB PER SRM 51-40-02.SDR IPXA2022062083269Skin · corrodedINSPECTION TYPE:1CCENTER WING BOX UPPER SKIN HAS CORROSION BETWEEN STA. XCW= 102 AND XCW= 110 AT STR. 13.REPAIRED CORRODED CENTER WING TANK UPPER SKIN BETWEEN STA. XCW= 102 AND XCW= 110 AT STR. 13 IAW VT-SAA EA 011-5730-1-A9589 REV. I/R AND UPS EO D11-5730-838SDR KCSA202205191064Stiffener · corrodedCORROSION ON AFT L-ANGLE UPPER SURFACE INSIDE WING CENTER SECTION FORWARD ACCESS HOLESDR IXXA2022051902Bracket · brokenR/H MAIN LANDING GEAR SUPPORT BEAM ACCESS PANEL SUPPORT BRACKET JUST ABOVE STRUT DOOR AFT SIDE IS BROKEN.SDR IPXA2022072184422Floor Panel · corrodedINSPECTION TYPE:3CRCB FLOOR PANEL P/N WSP0789-502 WITH CORROSION AT STA X=-47.5 TO X=-75.250.REMOVED, REPLACED FLOOR PANEL IAW SRM 51-31-01 (MINOR)SDR IPXA2022060382775Frame · crackedINSPECTION TYPE:SEG4AT STA 1240 IN RAT COMPARTMENT INTERIOR FRAME IS CORRODEDWORK PER UPSS E.O. B757-5310-24700-C, UPS RCD 262046, AND VT MAE E.A. 757-5360-A2931 REV- FAA FORM 8100-9 APPROVAL ATTACHEDSDR IPXA2022060282751Frame · damagedINSPECTION TYPE:16/4DURING ACCOMPLISHMENT OF E.O#B757-531073926-A. FOUND EXISTING REPAIR AT STA 1280, S2323R TO S27R REQUIRE ENGINEERING ASSISTANCE FOR ALTERNATIVE INSPECTIONWORK PER USPS E.O. B757-5310-39407-C, UPS RCD 262047, AND VTMAE E.A. 757-5360-27-A29SDR IPXA2022052782562Wing Root · crackedINSPECTION TYPE:C16CRACK ON R/H OVERWING EMERGENCY EXIT DOOR LOWER MAIN SILL INNER CHORD AT STA 883.5REPAIR I.A.W BOEING SR:4-5501411401 AND UPS EO B767-5310-83826-ASDR IPXA2022052782561Wing Root · crackedINSPECTION TYPE:C16CRACK ON L/H OVERWING EMERGENCY EXIT DOOR ;OWER MAIN SILL INNER CHORD AT STA 883.5REPAIR I.A.W BOEING SR:4-5500527955 AND UPS EO B767-5310-83822-ASDR SIMA20220518006Skin Panel · gougedDENT/GOUGE ON R/H SIDE AFT FUSELAGE BETWEEN FRAMES 80-82 STRINGERS 21L-22L. (MAJOR REPAIR)-C/A-C/W PERMANENT REPAIR IAW ERS EJ-53MR-4524SDR KCSA202205181057Stiffener · crackedSTIFFENER FOUND TO BE CRACKED AT WL 130 BETWEEN STA 300 TO STA 320 NOSE WHEEL WELL INTERNALSDR EBVR20220518None · noneCLAFING WAS FOUND AT F.S. 337.625 ON EXISTING INTERIOR REPAIR DOUBLER AT RH SURROUND DOUBLER, EMERGENCY EXIT LOCATION.
SDR CALA2022051801281Skin · chafedFUS SKIN BS2108-BS2150 STRG 1L-3L EXTERBAL SURFACE FOUND CHAFING REF HAECO NR L/P: 9482049, ORIGINATED BY EMP V905539, SPEC NO.: B777-06-3-7179. PERFORMED BY EMP V916782, FUS SKIN BS2108-BS2150 STRG 1L-3L EXTE EC/RA: 5370-01067 REV -, THIS REPAIR APPROVED AS PSDR CALA2022051801280Skin · chafedFUS SKIN BS2108-BS2150 STRG 1R-3R EXTERNAL SURFACE FOUND CHAFING REF HAECO NR L/P: 9482051, ORIGINATED BY EMP V905539, SPEC NO.: B777-06-3-7179. PERFORMED BY EMP V916782, FUS SKIN BS2108-BS2150 STRG 1R-3R EXTE EC/RA: 5370-01067 REV -, THIS REPAIR APPROVED AS PSDR CALA2022051801279Skin · chafedFUS SKIN BS2108-BS2150 STRG 1R-3R EXTERNAL SURFACE FOUND CHAFING REF HAECO NR L/P: 9482051, ORIGINATED BY EMP V905539, SPEC NO.: B777-06-3-7179. PERFORMED BY EMP V916782, FUS SKIN BS2108-BS2150 STRG 1R-3R EXTE EC/RA: 5370-01067 REV -, THIS REPAIR APPROVED AS PSDR CALA2022051801278Skin · chafedFUS SKIN BS2108-BS2150 STRG 1L-3L EXTERBAL SURFACE FOUND CHAFING REF HAECO NR L/P: 9482049, ORIGINATED BY EMP V905539, SPEC NO.: B777-06-3-7179. PERFORMED BY EMP V916782, FUS SKIN BS2108-BS2150 STRG 1L-3L EXTE EC/RA: 5370-01067 REV -, THIS REPAIR APPROVED AS PSDR SWAA2022061708780Bear Strap · crackedCRACK FOUND AT FWD GALLEY DOOR (R1) BEAR STRAP, BS 290-296, BETWEEN S-8R & S-9R, AFT OF FASTENER OPPOSITE FITTING LATCH. INSTALLED EWIS AND FOD PROTECTION AROUND R1 DOOR FOR BEARSTRAP REPAIR IAW AMM 20-60-07-913-801. REMOVED RAIN GUTTER FROM R1 DOOR IAW SRM SDR F3LA2022052000041Plate · corrodedDISCREPANCY: REFERENCE PEMCO N/R# 12317.0423 AFT CABIN WET ARE R/H AFT SHEAR WEB FROM FR69 TO FR70 CRACKED AND HAS SURFACE CORROSION.
CORRECTIVE ACTION: REMOVED AND REPLACED AFT CABIN WET AREA R/H SHEAR WEB FROM FR 69 TO FR 70 IAW A321 SRM 51-42-11SDR IPXA2022051782178Repair · discoveredINSPECTION TYPE:SEG4 AFT CARGO COMPARTMENT HAS AN EXISTING REPAIR AT STA 1480 R/H. INBD SIDE OF S-26R. REF: B757-5310-25026-CREPAIRED PER EA# 757-5360-27-A2915SDR IPXA2022051782186Repair · discoveredINSPECTION TYPE:SEG4 AFT CARGO COMPARTMENT HAS AN EXISTING FRAME REPAIR AT STA 1280 R/H INBD SIDE OF THE S-26RREPAIRED PER EA # 757-5360-27-A2916 REV - AND EO B757-5310-83609-ASDR IPXA2022051882203Support · bentINSPECTION TYPE:CW/W REAR ZONE FLOOR PANEL SUPPORT MIDDLE WEB IS BENTREFORMED SUPPORT WEB 2EA IAW SREO M-5100-41097-41097-E APPENDIX A STEP 11SDR IPXA2022051782187Repair · discoveredINSPECTION TYPE:SEG4 AFT CARGO COMPARTMENT HAS AN EXISTING FRAME REPAIR AT STA 1360 R/H INBD SIDE OF THE S-26R.REPAIRED PER EA # 757-5360-27-A2917 AND EO B757-5310-83614-ASDR IXXA2022072603Pressure Deck · corrodedRT WHEEL WELL PRESSURE DECK CORRODEDSDR IXXA2022072206Floorbeam · corrodedLOWER FLANGE OF ANGLE IN THE KEEL AREA AT STA 1168 CORRODEDSDR IXXA2022072205Skin · corrodedRT WHEEL WELL PRESSUER DECK CORRODED STA 100 RBL 49SDR IXXA2022072202Door · corrodedRT WEHEEL WELL PRESSURE DECK CORRODED STA 1100 RBL 64-58
Back to JASC 5310