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 VNAA202204199991Frame · corrodedFS 333.0 IS CORRODED FROM STR 26R TO STR 27.SDR V0XD20220419001Hinge · out of tolerancePASSENGER DOOR FUSELAGE HINGE DID NOT PASS THE "GO-NO-GO" GAUGE TEST (IAW BOMBARDIER REO 670-53-21-582 REV. E DATED 2017-06-05). CORRECTIVE ACTION: REMOVED AND REPLACED THE PASSENGER DOOR FUSELAGE HINGE (PN: SH670-31876-13S) IAW CRJ 900 SRM 51-42-06. WORK DOSDR EE4Y2022041815417Stringer · corrodedDURING THE STRUCTURE INSPECTION PER ALLEGIANT TASK CARD 534107-01-1-001, IT WAS FOUND AFT COMPARTMENT AT FR65, STRG 43LH WITH CORROSION.
WORK PERFORMED:
PERFORMED PERMANENT REPAIR IN AFT CARGO COMPARTMENT BETWEEN FR64 AND 310MMM AFT OF FR65, STRG43 LH IAW SSDR SCNA20220523054Floor Skin · crackedDEFECT: FOUND DAMAGE TO FRAME, AFT CARGO @STA 727E, STR 24L TO 25L. RESOLUTION: REPAIRED FRAME @STA 727E STR 24L - 25L IAW SCA ENG-53SCA-10964 REV 00 AND ATS ER 22-01693 REV IR.SDR SCNA20220523053Frame Angle · crackedDEFECT: FOUND DAMAGE TO FRAME, AFT CARGO @STA 727B, STR 24L. RESOLUTION: REPAIRED DAMAGED FRAME @STA 727B STR 24L IN ACCORDANCE WITH B737 SRM 53-60-70-2R-3 REV 75. THIS IS A CATEGORY "B" REPAIR. INSPECTION THRESHOLD IS 50,000 FLIGHT CYCLES AFTER AIRPLANE DESDR SCNA20220520049Floorbeam · crackedDEFECT: FOUND DAMGE TO FRAME, AFT CARGO @STA. 727B, STR. 3R RESOLUTION: REPAIRED FRAME AFT CARGO @STA 727B, STR 23R PER SRM 53-60-07-2R-3 REV 75 REPAIR IS CAT B. INSPECTION THRESHOLD 50,000 FLIGHT CYCLES AFTER AIRPLANE DELIVERY OR 35,000 FLIGHT CYCLES AFTER SDR SCNA202205170SUPPFrame Angle · crackedDEFECT: FOUND DAMAGE TO FRAME, AFT CARGO @STA 727C, STR 23LSDR SCNA22020516047Floor Support · crackedDEFECT: FOUND DAMAGE TO FRAME, AFT CARGO @STA. 727F, STR. 24L. RESOLUTION: AFT CARGO FRAME @ STA 727F, STR 24L REPAIRED PER SRM 53-60-07-2R-3 REV 75. REPAIR IS CAT B. INSPECTION THRESHOLD 50,000 FLIGHT CYCLES AFTER AIRPLANE DELIVERY OR 35,000 FLIGHT CYCLES SDR SWAA2022051195449Web · out of positionFORWARD CARGO COMPARTMENT DOOR CUT-OUT THRESHOLD HAS SPOTS OF CORROSION BETWEEN STA.440 AND STA.500 RBL27 TO RBL29. / [01] REMOVED CORROSION AT FWD CARGO COMP. DOOR CUTOUT THRESHOLD BETW. STA 440 THRU STA 500 RBL 27 THRU RBL29 (WORKED BY HERNANDEZ MEDINA #2634SDR SWAA2022051195665Web · corrodedCORROSION ON AFT CARGO BAY THRESHOLD AT RBL 26 BS 787+15; BS 807+3; BS 807+8; BS 807+10; BS 807+12; BS 807+13; BS 807+15; BS 807+17. / [01] COMPLETED STEPS 1-9;[02] UPDATED STEPS 1-9 TO PARTIAL;[03] VERIFIED;[04] COMPLETED STEPS 1-9;[05] LOCATED AND DRILLED NESDR SWAA2022051095273Door Frame · crackedCRACK FOUND ON FRAME AT STA 328 ABOVE L1 DOOR CUTOUT. / [01] CONFIRMED CRACK AT STA 328 FRAME ABOVE L1 DOOR CUTOUT IAW NDTM PART 6;51-00-00 PROCEDURE 23.<BR>CRACK LENGTH : 0.157';[02] TRIMMED OUT FRAME INNER CHORD TO REMOVE DAMAGE AT STA 328 BETWEEN S-5L AND SSDR SWAA2022051095655Frame · crackedCRACK IN RADIUS OF FRAME AT B.S. 312 JUST ABOVE FORWARD ENTRY DOOR CUT OUT. / [01] REMOVED DAMAGE AT FRAME RADIUS BS 312 JUST ABOVE FED CUT OUT I.A.W SRM 51-10-02-0G-0;[02] REMOVED DAMAGE AT FRAME RADIUS AREA OF .25 X .15 BS 312 JUST ABOVE FED CUT OUT I.A.W SRSDR AALA202205058304Shield · corrodedAIRCRAFT IN BASE MAINTENANCE: FOUND CORROSION ON SHIELD TRANSITION PANEL LOCATED BETWEEN STA 767 AND STA 787, AND RIGHT BUTT LINE 25. INSTALLED NEW SHIELD PER AARD 51-00-05-1.SDR ASAA2022041838163Unknown · corrodedAFT CARGO COMPARTMENT R/H TRANSITION PANEL UPPER AND LOWER SURFACES CORRODED FS 727-767. GROUNDED - YES. REMOVED CORROSION AND CHECKED LIMITS FOUND TRANSITION PANEL OUT OF LIMITS IAW B737-900ER SRM 53-00-53-1A-2 REPAIRED TRANSITION PANEL IAW B737-900ER SRM 53-SDR ASAA2022041838162Unknown · corrodedAFT CARGO COMPARTMENT L/H TRANSITION PANEL CORRODED UPPER AND LOWER SURFACES FROM FS 727-847. GROUNDED - YES. REMOVED CORROSION AND CHECKED LIMITS FOUND TRANSITION PANEL OUT OF LIMITS IAW B737-900ER SRM 53-00-53-1A-2, REPAIRED TRANSITION PANEL IAW B737-900ER SSDR ASAA2022041838141Shield · corrodedAFT CARGO COMPARTMENT SHIELD FWD OF DOOR CORRODED. GROUNDED - YES. REMOVED CORROSION AND CHECKED LIMITS FOUND TO BE OUT OF LIMITS IAW B737-900ER SRM 53-60-15-1A-1. REMOVED AND REPLACED SHIELD IAW B737-900ER SRM 51-40-02-0G-0W .5 O .050 R .037 L .8 D .013.SDR FDEA202204181076Seat Track · damagedMAIN DECK COMPT - SEAT TRACK CROWN LIP AREA FOUND ENLARGED AT FR20 6" AND -Y450 CUT OUT AND INSTALLED NEW SEAT TRACK PORTION & REPAIR ANGLES I.A.W EA NO:6-5310- T0367804 P1, SEQ NO:001135, TITLE:FUSELAGE-MAINFRAME- MAIN DECK SEAT TRACKS AT -Y450 & -Y1456 WOSDR FDEA202204181075Seat Track · damagedMAIN DECK COMPT - SEAT TRACK CROWN LIP AREA FOUND ENLARGED AT FR20 6" AND -Y1456 CUT OUT AND INSTALLED NEW SEAT TRACK PORTION & REPAIR ANGLES I.A.W EA NO:6-5310- T0367804 P1, SEQ NO:001135, TITLE:FUSELAGE-MAINFRAME- MAIN DECK SEAT TRACKS AT -Y450 & -Y1456SDR EE4Y2022041815415Pressure Plate · crackedDURING THE STRUCTURE INSPECTION PER ALLEGIANT EO E5331-0006/0007, IT WAS FOUND FASTENER WITH CRACK ON THE PRESS PNL FLEX BRKT AT FR 36
WORK PERFORMED:
EO E5331-0006/0006 REV 03 AD 2018-06-04 INSPECTION AND REPAIR OF FR 35-FR36 PRESSURE PLATE ATTACHMENTSSDR EE4Y2022041815412Stringer · corrodedDURING THE STRUCTURE INSPECTION PER ALLEGIANT TASK CARD 534107-01-1-001, IT WAS FOUND AFT COMPARTMENT BETWEEN FR64 AND FR65, STRG 42RH WITH CORROSION.
WORK PERFORMED:
PERFORMED PERMANENT REPAIR IN AFT CARGO COMPARTMENT BETWEEN FR64 AND FR6 STRG42 RH IAW SDR VNAA202204211111Pressure Valve · departedTHE LOW PRESSURE DOOR WAS LEFT OPEN DEPARTING CLT AND THE LOW PRESSURE VALVE DOOR CAME OFF SOMEWHERE BETWEEN CLT AIRPORT AND JAN AIRPORT. CLT OPS HAS BEEN NOTIFIED OF THE MISSING VALVE COVER AND AIRCRAFT DAMAGE AS WELL. A DENT NEXT TO THE LOW PRESSURE VALVE DOSDR QXEA2022041800161Fairing · corrodedFWD WING TO BODY FAIRING STRAP CORRODED BETWEEN 5 AND 6 0 CLOCK POSITION. BLENDED CORROSION ON FWD WING TO BODY FAIRING STRAP BETWEEN 5 AND 6 0 CLOCK POSITION PER SRM 51-10-03. NOMINAL MATERIAL THICKNESS OF STRAP IS 0.050". MATERIAL REMOVED 0.003" . MATERIAL RSDR EE4Y2022041715406Stringer · corrodedDURING THE STRUCTURAL INSPECTION PER TASK Nº: 534107-01-1-001_P1-OP-UP/0 CPCP, IT WAS FOUND AT AFT CARGO COMPARTMENT FROM FR57 TO FR59 AT S-42RH AND BETWEEN 260MM AFT FR57 AND 200MM FWD FR57 AT S-43L WITH CORROSION. DUE TO THIS FACT, DETAILS WERE SENT TO AIRBUSDR EE4Y2022041715405Crossbeam · crackedDURING THE WORK CARD Nº: 53-120-003 INSPECTION ACCOMPLISHMENT WHICH IS RELATED TO AD 2018-14-09 / SB A320-53-1286 (R1), IT WAS FOUND ON CROSSBEAM SPLICING UPPER ROW AREA AT AFT LH SIDE HOLE IDENTIFY AS H3 WITH CRACK AT 12 O´CLOCK POSITION. DUE TO THIS FACT, DESDR F3LA2022091400108Shear Plate · corrodedCORROSION ON MULTIPLE AREAS ON RH LATERAL SHEAR PLATE FROM FRAME C69C70. REMOVED AND REPLACED RH LATERAL SHEAR PLATE FROM FRAME C69 TO C70 IAW SRM 51-42-11.SDR F3LA2022091400107Shear Plate · corrodedCORROSION ON MULTIPLE AREAS ON LH LATERAL SHEAR PLATE FROM FRAME C69C70. REMOVED AND REPLACED LH LATERAL SHEAR PLATE FROM FRAME C69 TO C70 IAW A320 SRM 51-42-11. PERFORMED PERATIONAL TEST OF VOR 1 AND 2 SYSTEMS IAW AMM 34-55-00-740-002-A. BITE TEST GOODSDR F3LA2022091400106Beam · corrodedAFT R2 DOOR SILL BEAM PREVIOUS REPAIR CORRODED. REMOVED AND REPLACED CORRODED R2 DOOR SILL IAW SRM 51-42-11SDR F3LA2022091400103Beam · corrodedL1 DOOR SILL BEAM, FWD AND AFT FASTENER HOLES CORRODED. REMOVED AND REPLACED L2 DOOR SILL IAW A320 SRM 51-42-11SDR ASAA2022041538532Plate · corrodedMAIN CABIN FLOOR STRUCTURE HAS CORROSION AT R/H STGR 23 BETWEEN FR69 AND FR70 (AREAS MARKED IN RED)(STREAMER ATTACHED) GROUNDED - YES. DISPLACED AND RE-SECURED WIRING TO VACUUM GENERATOR IAW ESPM 20-33-11 AND AWM 38-31-06. REMOVED, LOCATED, DRILLED THE PLATE SDR VGCA20220415001Skin Panel · corrodedCORROSION ON FUSLAGE SKIN AT THE WINDOW CUTOUT BETWEEN STRETCH STA 389.5 AND 409.5 LHS. REPAIRED IN ACCRODANCE WITH ENGINEERING REPAIR R278-053-012-002SDR FDEA202204150970Intercostal · elongatedMAIN CABIN STA 1640STR14L INTERCOSTAL HAS ELONGATED/ DAMAGED FASTENER HOLES REMOVED, FABRICATED AND INSTALLED NEW WEB 143N8735-3 , IAW B757-2 DWG 146N8735 REV: CSDR SWAA2022042594318Angle · crackedL/H MWW ATTACH CLIP 149A7692-15 CRACKED BS 727 LBL 19 WL 145 L/H MWW SUPPORT RING CLIP IS CRACKED BS 727 LBL 20.5 W/L 148. P/N 149A7678-7 / [01] UPDATED MEASUREMENTS;[02] ATTACH CLIP HAS NO LIMITS FOR A CRACK. PART FOUND TO BE OUT OF LIMITS IAW SRM 53-40-71-1ASDR IPXA2022041681212Panel · crackedINSPECTION TYPE:3CRCB WALL P/N WSP0798-505 HAS A CRACK INSIDE AT POSITION 4.REPLACED THE RCB WALL P/N WSP0798-505 IAW MD11 AMM 25-59-13-400-801 (MINOR)SDR CALA2022041801003Shear Web · noneSUPPORT TASK-- MAIN CABIN SHEAR WEB STA 700-720 RBL25 REQUIRES F ABRICATION. TRANSCRIBED FROM HAECO GSO NRC 9285902 REMOVED AND REPLACED -4 SHEAR WEB IAW B757-200 SRM 51-40-02 AND BOEING DWG 143N5140 REV B. HAECO GSO MECH V917499 INSP QC302SDR CALA2022041801002Deck Plate · corroded(SUPPORT TASK) MAIN CABIN DECK PLATE STA 1716 RBL50 HAS CORROSIO N ON WEB, TRANSCRIBED FROM HAECO GSO NRC 9285434 REMOVED CORROSION ON THE AFT DECK PLATE AT STA 1716 RBL50. REMAI INSP QC302 NING THICKNESS FOUND TO BE .027, REMOVED .044, ORIG .071 PER B75 7-200SDR QXEA2022041400153Floor Support · corrodedCORROSION FOUND IN THE FWD WET AREA RH SILL BETWEEN FR12-FR13, Y+49. REMOVED AND REPLACED RH FWD FLOOR SILL BETWEEN FR12-FR13 IAW SRM 51-40-08 AND 51-45-00.SDR KCQA20220506Door · damagedFUSELAGE SKIN UPPER LH CORNER OF THE CARGO DOOR WAS DAMAGED FROM A FORKLIFT. REPAIRED DAMAGE AT REAR FUSELAGE CARGO DOOR FWD UPPER CORNER DOOR SKIN CUTOUT AS PER EMBRAER ETD2022-120-014837 REV B AND CALSPAN CORPORATION ENGINEERING DRAWING # CAL-F-M0329 REV B SDR FDEA202204120926Longeron · crackedCENTER CARGO COMPARTMENT BILGE AT STATION 5-113LONGERON 48 LEFT HAND AFTER REMOVAL OF UPPER DAMAGED SPLICE FOUND LONGERON 48 LEFT HAND CRACKED AT STATION 1538. CENTER CARGO COMPARTMENT BILGE CRACKED LEFT HAND LONGERON 48 AT STATION 1538 REPAIRED AS PERSDR CALA2022041400978Stringer · corrodedAFT CARGO COMP. STR38R IS CORRODED BETWEEN FR59 AND FR60. GENERA TED BY V061690 ON HAECO LCQ NR 9294386/36386 REMOVED CORROSION AFT CARGO COMP. STR38R BETWEEN FR59 AND FR60 F OUND TO BE OUT OF LIMITS IAW A319 SRM 53-41-13-283-002 REMOVED A ND REPLACED STRINGERSDR CALA2022041400977Stringer · corrodedAFT CARGO COMP. STR37R IS CORRODED BETWEEN FR59 AND FR61. GENERA TED BY V061690 ON HAECO LCQ NR 9294385/36385 REMOVED CORROSION AFT CARGO COMP. STR37R BETWEEN FR59 AND FR61 F OUND TO BE OUT OF LIMITS IAW A319 SRM 53-41-13 REMOVED AND REPLA CED STRINGER IAW A31SDR FDEA202204120925Splice · corrodedCENTRE CARGO BILGE AT STATION 5-113 LONGERON 48 LEFT HAND SPLICE FITTING FOUND CORROSION . CENTRE CARGO BILGE AT STATION 5-113 LONGERON 48 LEFT HAND SPLICE FITTING CORROSION EVALUATED FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-00-00-2R FIGURE 5 RSDR SWAA2022042593165Support Ring · crackedL/H MWW SUPPORT RING CLIP IS CRACKED BS 727; LBL 20.5; W/L 148. P/N 149A7678-7 / [01] REMOVED CLIP AT L/H MWW SUPPORT BS 727; LBL 20.5; W/L 148. IAW SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED NEW CLIP P/N 149A7678U9 PO# 864333 IAW SRM 51-40-05-0G-0 AND DWG 149SDR IPXA2022042581448Frame · dentedINSPECTION TYPE:CAFT LOWER CARGO PIT FRAME AT FS 1520 BETWEEN STR 25R TO 26R HAS A DENT ON UPPER FLANGE OF FRAMEREPAIRED FRAME 1520 PER SRM 53-00-07-2R-5SDR FDEA202204111007Rib · crackedWING FUSELAGE FAIRING RIB RH, STA.5-113 BETWEEN STRG 28-29 - CRACK AT RIB/FUSELAGE ANGLE UPPER FASTENER. CRACK CONFIRMED USING NDT HFEC. (PANELS AFFECTED 152LT & 152KT) CUTOUT DAMAGED RIB, FABRICATED AND PROCESSED NEW REPAIR ANGLE AND SPLICE, INSTALLED NSDR IPXA2022050581792Frame · damagedINSPECTION TYPE:CNEEDED ALTERNATIVE METHOD TO INSPECT FRAME 1600 RH PER EO# B757-5310-73926-AMODIFIED REPAIR AT FR 1600 RH STR 26R PER EA# 757-5360-27-A2897SDR IPXA2022050581791Frame · damagedINSPECTION TYPE:CNEEDED ALTERNATIVE METHOD TO INSPECT FRAME 1560 LH PER EO# B757-5310-73926-AMODIFIED REPAIR AT FR 1560 STR 26L PER EA# 757-5360-27-A2892SDR IPXA2022050581790Frame · damagedINSPECTION TYPE:CNEEDED ALTERNATIVE METHOD TO INSPECT FRAME 1300 LH PER EO# B757-5310-73926-AMODIFIED REPAIR AT FR 1300 STR 26L PER EA# 757-5360-27-A2901-ASDR IPXA2022042981579Frame · incorrectINSPECTION TYPE:18/2AFT LOWER CARGO PIT AT FS 1560 STR 26R DURING AN AD FRAME INSPECTION FOUND THE PREVIOUS REPAIR WAS FABRICATED AND INSTALLED INCORRECTLYREMOVED PREVIOUS REPAIR AND INSTALLED REPLACEMENT REPAIR PER EA #757-5360-27-A2895 STEPS 1-8SDR QXEA2022042900179Panel · dentedAIRCRAFT RECEIVED A HARD LANDING. REMOVED FROM SERVICE AND FERRIED FOR A PHASE III INSPECTION. AIRCRAFT CURRENTLY OUT OF SERVICE.SDR SWAA2022042692567Web · corrodedAFT CARGO FLOOR STRUCTURE THRESHOLD WEB WITH CORROSION RBL 23-26 AND WL 157-163 AND BETWEEN BSTA 794-847 / [01] REMOVED CORROSION ON THRESHOLD WEB AT AFT CARGO BETWEEN STA 794 AND 847 RBL 23-26 AS PER B737-700 SRM 51-10-02-0G-0;[02] VERIFIED STEP #1;[03] PERFO
Back to JASC 5310