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 ASAA2023011441886None · crackedLH AIR CON BAY VAPOR BARRIER AT STA 663 LWR ATTACH CORD CRACKED APPROX 3 IN OB OF KEEL BEAM. GROUNDED - YES. REMOVED DAMAGE & REPAIRED CHORD IAW B737-700 SRM 51-70-04-2R-10.SDR FDEA202301140235Crossbeam · damagedAGING AIRCRAFT ASSESSMENT: EXISTING CROSSBEAM REPAIR FOUND ON M/D AT FR 66, BTW Y953 ~ Y1456. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE : STRUCTURES-REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.70SDR YENA2023011800052Window Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER ATTACH CONTINUITY FITTING RH SIDE, CRACK LENGTH IS 0.200 INCH APPROX, IN COCKPIT; REF AEROMAN N/R 2022-662819 WO 2022 454/1, REMOVED ADN REPLACED CONTINUITY FITTING ON FRAME 2 WSDR YENA2023011800051Window Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER ATTACHMENT AR EA CONTINUITY FITTING LH SIDE, CRACK LENGTH IS 0.200 INCH APPROX, IN COCKPIT; REF N/R 2022-662818 WO 2022454/1, R&R CONTINUITY FITTING FROM FRAME 2 WINDSHIELD CENSDR FDEA202301140100Plate · corrodedFLIR CAMERA MOUNT PLATE IS CORRODED. REMOVED FLIR CAMERA MOUNTING BRACKET, REMOVED AND REPLACE HEAT PLATE WITH NEW PLATE, REINSTALL MOUNTING BRACKET BACK ON AIRCRAFT. PER FEDEX DWG B57-53-015 REV - AND B57-53-017 REV ASDR FDEA202301140093Door Frame · crackedMAIN DECK CARGO L3 DOOR JAMB AFT LOWER CORNER AREA BS 1305.25 - 1315.42 FOUND CRACKED. L3 DOOR JAMB AFT LOWER CORNER AREA STATION 1305.25 TO STATION 1315.42 SKIN CRACKED REPAIRED AS PER SRM 53-40-15-2R REPAIR 3 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GSDR CALA2023011600121Crossbeam · crackedRIGHT FR 20 CROSSBEAM, HOLE H36 HAS A REJECTABLE INDICATION IN B OTH LAYERS, FROM AND OF ROUND CONDITION. REPAIR RH FR 16 CROSSBE AM BEFORE NEXT FLIGHT PER STEP 9. (AD RELATED TASK 2018-14-09). REVISION OF ECRA 5310-08092 ON OR BEFORE THE AIRCRAFT REACHES 119SDR FDEA202301130121Dummy Rail · wornI.A.W E6-5310-7-3322E PT1 INSPECTION FOUND FR54/FR54.2 RH NO.4 TRACK GAP WAS 1.02MM. (OVER 1MM BUT LESS 2.15MM) I.A.W A300-600 SRM 53-15-16-201 PARA 5A FIG.201 P201-210 PERFORM REPAIR ACCOMPLISHED.SDR FDEA202301130120Dummy Rail · wornI.A.W E6-5310-7-3322E PT1 INSPECTION FOUND FR54/FR54.2 RH NO.3 TRACK GAP WAS 1.02MM. (OVER 1MM BUT LESS 2.15MM) I.A.W A300-600 SRM 53-15-16-201 PARA 5A FIG.201 P201-210 PERFORM REPAIR ACCOMPLISHED.SDR FDEA202301130119Dummy Rail · wornI.A.W E6-5310-7-3322E PT1 INSPECTION FOUND FR54/FR54.2 LH NO.4 TRACK GAP WAS 1.06MM. (OVER 1MM BUT LESS 2.15MM) I.A.W A300-600 SRM 53-15-16-201 PARA 5A FIG.201 P201-210 PERFORM REPAIR ACCOMPLISHED.SDR FDEA202301130118Dummy Rail · wornI.A.W E6-5310-7-3322E PT1 INSPECTION FOUND FR38.2/FR40 LH NO.4 TRACK GAP WAS 1.09MM. (OVER 1MM BUT LESS 2.15MM) I.A.W A300-600 SRM 53-15-16-201 PARA 5A FIG.201 P201-210 PERFORM REPAIR ACCOMPLISHED.SDR AALA202301171323Fitting · corrodedAIRCRAFT WAS GROUNDED (LONG TERM STORAGE): LH UPPER KICK FITTING HAS CORROSION LOCATED AT STA 663 AND STR 18A REMOVED AND REPLACED KICK FITTING PER AARD.SDR AALA202301176798Fitting · crackedAIRCRAFT WAS GROUNDED (LONG TERM STORAGE: DURING INSPECTION OF THE RH STA 663.7 FAIL SAFE STRAP, FOUND A CRACK INDICATION AT EH UPPER AFT FASTENER HOLE HIDDEN BEHIND THE STR 18A STRAP. REMOVED AND REPLACED RH STA 663 PICKLE FORK FITTING.SDR AALA202301172726Fitting · crackedAIRCRAFT WAS GROUNDED (LONG TERM STORAGE): DURING INSPECTION OF THE LH STA 663.7 FAIL SAFE STRAP FOUND A CRACK INDICATION AT UPPER FASTENER BEHIND THE STR 18A STRAP. REMOVED AND REPLACED LH STA 663 PICKLE FORK FITTING DUE TO A CRACK INDICATION.SDR CALA2023011600117Fitting · damagedUPON REMOVAL OF CORNER FITTING AT FRAME 38 L2 DOOR HAS A OUT A OUT OF ROUND HOLE LOWER O/B A3NB-53-3-6299 PER HAECO LCQ N/R 9292 471/36471 OF THE LATEST REVISION OF ECRA 5340-02083 ON OR BEFORE THE AIRCRAFT REACHES 60000 TOTAL AIRCRAFT CYCLES. ACCOMPLISH INITISDR CALA2023011600115Fitting · crackedFLIGHT DECK, AT WINDSHIELD CTR POST, LEFT AND RIGHT CONTINUITY F ITTINGS HAVE CRACK INDICATIONS ON UPPER FLANGE APPROX .55 INCH O UT FROM CENTER POST AD2020-17-03 PER NR9292350/36350 GEN BY V892 444 097. WORK C/W BY LCQ EMP V929087. FOR THE REPAIR TO THE FRONTSDR JR2R20230113776Crossbeam · corrodedCROSSBEAM AT FR84 CORRODED AT RBL9SDR JR2R20230113843Doubler · corrodedFWD RH DOUBLER AT FR14 CORRODED.SDR ASAA2023011242683Floorbeam · corrodedMAIN CABIN FLOOR BEAM IS CORRODED AT FR68 LBL24. GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN FLOOR BEAM BETWEEN FR66 AND FR68 LBL 24 IAW A320 SRM 51-42-11/001.SDR SWAA2023021491001Support · corrodedCORROSION SUPPORT ZEE LOCATED BTW BS 787 TO BS 727B LBL 21 WL 156 AFT CARGO COMPARTMENT 2023-37979<[01] TOOL USED: ULTRASONIC THICKNESS GAGE; P/N: 45MG; S/N: 221861811;CAL DUE DATE: 08-NOV-23;[02] REPLACED SUPPORT ZEE AND FASTENER LOC ON BS727 TO BS847 LBL 21 SDR IPXA2023020190510Support · crackedINSPECTION TYPE:10Y*A/C OOS* R/H DIAGONAL SUPPORT AT FR37 CRACKEDREMOVED AND REPLACED SUPPORT IAW-SRM 51-40-21SDR IPXA2023020190515Support · crackedINSPECTION TYPE:10Y*A/C OOS* R/H DIAGONAL SUPPORT AT FR38 CRACKED.REMOVED AND REPLACED SUPPORT IAW-SRM 51-40-21SDR ASAA2023011241714None · corrodedMAIN CABIN STA 986 LH UPPER FLANGE CORR FROM BL0-CUSP. GROUNDED - YES. REMOVED CORROSION ON L/H UPPER FLANGE @ STA 986 ORIGINAL THICKNESS .150" REMAINING .121" REMOVED .029". FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-70-51-2R-4. REMOVED INTERCOSTAL, FITTINSDR SWAA2023013191119Intercostal · corrodedMAIN CABIN FLOOR STRUCTURE PANEL BREAK BETWEEN STA 328 AND STA 344 LBL 11.10 HAS CORROSION ON UPPER FLANGE.<[01] INSTALLED EWIS PROTECCION AT FWD WET AREA;BET. STA 328 TO STA 344;LBL 11.PER B 737-700 AMM 20-60-07-913-901.;[02] REMOVED CORROSION AT PANEL BREAK;SDR AALA202301137915Door Frame · lack of lubeAIRCRAFT WAS NOT GROUNDED: MAIN DECK CREW REST DOOR STICKS. LUBRICATED MAIN DECK CREW REST DOOR JAMB.SDR ASAA2023011141713Intercostal · noneAFT PIT RIGHT HAND SIDE TRANSITION PANEL CORRODED STATION(S 727 TO 767. GROUNDED - YES. REMOVED CORROSION, FOUND TO HAVE 100% MAT. LOSS IN MULTIPLE AREAS. REMOVED DAMAGED TRANSITION PNL, FAB'D, LOCATED, DRILLED, ALODINED, PRIMED & INSTALLED NEW TRANSITION PNL SDR SWAA2023020290122Attach Angle · crackedCRACKED INTERCOSTAL UPPER ATTACH ANGLE STA 380-400; LBL 13; WL 208.<[01] REMOVED DAMAGED INTERCOSTAL UPPER ATTACH ANGLE STA 380-400; LBL 13; WL 208 PER SRM 51-40-02-0G-0.;[02] LOCATED AND DRILLED AND DEBURRED AND INSTALLED NEW INTERCOSTAL UPPER ATTACH ANGLE STSDR SWAA2023020290082Web · crackedCRACK WEB LOCATED BTW BS 294.5 TO BS 303.9 STR 16L AT FWD GALLEY AREA 2023-37139<REMOVED AND RE-INSTALLED WEB WEB LOCATED BTW BS 294.5 TO BS 303.9 STR 16L AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DRAWING #141A8180. REV: C. SEE INDIVIDUAL SIGN-OFF BELOWSDR FDEA202301090054Pressure Deck · corrodedMAIN CABIN PRESSURE DECK LEFT SIDE STATION 1690 TO 1704 BL0 TO BL11L HAS CORROSION AROUND FASTENER HOLES REPAIRED MAIN CABIN PRESSURE DECK PER FEDEX EA#F-5310-T0372257-P1, ORIG SUB DATE: 1/9/2023SDR SWAA2023021489745Tie Clip · crackedCRACK TIE CLIP BS 277 AT STR 10R AT PASSENGER CABIN 2023-37813<[01] REPLACED TIE CLIP BS 277 AT STR 10R AT PASSENGER CABIN IAW B737-700 SRM 51-40-02; SRM 51-10-02 AND DWG 141A1110 REV:- SHEET:17 SEE INDIVIDUAL SIGNOFFS BELOW.;[02] CERTIFIED RII WORK PERFORMED.SDR SWAA2023021489744Stub Frame · crackedCRACK FRAME STUB ON BS 294.5 AT LEVEL STR 17R AT PASSENGER CABIN 2023-37814<[01] EDDY CURRENT EQUIPMENT P/N: NORTEC500D; S/N: N500X12101V022235; DUE DATE: 03-AUG-23.;[02] PERFORMED REPAIR ON FRAME STUB BS 294.5 AT LEVEL STR 17R AT PASSENGER CABIN IAW B737-700 SDR SWAA2023020789034Web · corrodedCORROSION ON FWD CARGO BAY DOOR CUT-OUT SUB-THRESHOLD WEB FROM STA 440+7 TO STA 480+10; RBL 26 TO RBL 29; WL 156.<[01] VERIFIED APPLICABILITY IAW SRM 53-30-15-0L-1 FOR IDENTIFICATION AND SRM 53-30-15-1A-1 FOR ALLOWABLE DAMAGE.<BR>REMOVED CORROSION ON FWD CARGOSDR SWIA2023012467165Waste Box · corrodedAREA AROUND WASTE BOX IS CORRODED INTERNALLY FR 88- FR 89 STGR 21- STGR 23. REMOVED AND REPLACED WASTE BOX DOUBLER FR 88- FR 89 STGR 21R - 23R REF SRM 51-40-08SDR FDEA202301060042Longeron Splice · corrodedLOWER CENTER CARGO COMPARTMENT BILGE STATION 5-70, X 48 LONGERON SPLICE FITTING FOUND WITH CORROTION. LOWER CENTER CARGO COMPARTMENT BILGE STATION 5-70, X 48 CORRODED LONGERON SPLICE FITTING REMOVED AND REPLACED AS PER MD-11 SRM 51-33-01-0G. LONGERON SPSDR AALA202301138895Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT LEFT PASSENGER / CREW DOOR CUT OUT CORNER SHAPE FITTING AT FR 66 AND S23L. MAINTENANCE REPLACED CORNER SHAPE FITTING PER SRM 51-42-11.SDR FDEA202301060043Pressure Deck · corrodedMAIN CABIN PRESSURE DECK RIGHT SIDE STATION 1690 TO 1700 BL5R TO BL11R HAS CORROSION AROUND SEVERAL FASTENERS HOLES REPAIRED MAIN CABIN PRESSURE DECK PER FEDEX EA#F-5310-T0372257-P1, ORIG SUB DATE: 1/9/2023SDR YENA2023011000023Beam · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS FOUND ON LOWER BEAM AT CUTOUT FWD SERVICE DOOR. OUT OF LIMITS. REMOVED AND REPLACED IAW SRM 51-12-01, SRM 51-10-03 & SRM 53-10-11-AD52. MAJOR REPAIR.SDR FDEA202301060044Crease Beam · corrodedMAIN CABIN LH INNER CREASE BEAM STA 860-880 CORRODED REMOVED DAMAGE AND REPAIRED INNER CHORD PER B757 SRM 53-00-13-2R, REPAIR#1 - FIG 201- DETAIL I AND CIC PER B757 AMM 51-24-09-7-0 AND SRM 51-20-01-0GSDR DALA2023010900106Unknown · damagedDAMAGE FOUND DURING GVI IN PILOT REPORT OF BIRD STRIKE. DAMAGE LOCATED ON L/H OF A/C FWD OF CAPTAINS WINDOW AND AFT OF RADOME 20'' ABOVE STATIC PORT. COMPLIED WITH ERA 603955-14 REV.ORIG TO PRI 603955-14 REVS 0 THRU 2.SDR JR2R20230106Gusset · corrodedFLOOR GUSSET AT FR90 RBL10 CORRODEDSDR JR2R20230106512Intercostal · corrodedINTERCOSTAL AT RBL10 BETWEEN FR90 AND FR90A CORRODEDSDR CALA2023010600037Door Sill · corrodedRH AFT DOOR SILL FR66 TO FR68 CORRODED AT 4 LOCATIONS (P/N D5348 004320701) REMOVED CORROSION ON DOOR SILL IAW SRM 51-74-00. MEASURED AND FO UND OUT OF LIMITS IAW SRM 53-41-14 L=1.400" W=1.130 D=0.060" O.T =0.177" T.T=.117" REPLACED DOOR SILL IAW SRM 51-72-11-SDR CALA2023010600036Stop Fitting · crackedDURING ROTO INSP OF LH FR 20 DOOR STOP FITTING #7. CRACK INDICATION WAS NOTED IN UPPER I/B HOLE, FRAME AND INTERCOSTAL L AYERS. REPAIR BEFORE NEXT FLIGHT. REPAIRED DAMAGED HOLE IAW REPAIR DRAWING R53113118. EMP:V934583 W/C:6001971315 STENGBFMSDR ASAA2023010541945Support Beam · corrodedFOUND CORROSION ON UPPER SURFACE OF LONGITUDINAL SUPPORT BEAM AROUND LAV MOUNT HOLE AT FRAME 66+6" LBL 35 BELOW FLOOR PANEL 261DF. GROUNDED - YES. NO ALLOWABLE LIMITS FOR CORROSION REMOVAL AT LONGITUDINAL BEAM HARD POINT PER A320 SRM 53-00-14-283-002 STEP 2.C SDR SWAA2023020788644Intercostal · crackedCRACKED INTERCOSTAL AT FWD WET AREA BS344+5 RBL32 WL208.<[01] REMOVED INTERCOSTAL BS 344 TO BS 360 RBL 32 WL 208.1 PER SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED NEW INTERCOSTAL AT FWD WET AREA BS 344 TO BS 360 RBL 32 WL 208.1; IAW SRM 51-40-05-0G-0 AND DWG 14SDR SWAA2023020788658Intercostal · crackedCRACKED INTERCOSTAL AT FWD WET AREA BS294+7 RBL30 WL208.<[01] REMOVED INTERCOSTAL BS 294 TO BS 312 RBL 30 WL 208.1 PER SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED NEW INTERCOSTAL AT FWD WET AREA BS 294 TO BS 312 RBL 30 WL 208.1; IAW SRM 51-40-05-0G-0 AND DWG 14SDR SWAA2023020788660Intercostal · crackedCRACKED INTERCOSTAL AT FWD WET AREA BS312+5 RBL30 WL208.<[01] REMOVED INTERCOSTAL BS 312 TO BS 328 RBL 30 WL 208.1 PER SRM 51-40-02-0G-0;[02] RECIVED NEW INTERCOSTAL P/N 141A5110-12 LOCATED AND DRILLED NEW INTERCOSTAL AT BS 312 TO BS 328 RBL30 WL208; IAW 737-7SDR SWAA2023020788645Intercostal · crackedCRACKED INTERCOSTAL AT FWD WET AREA BS312+9 LBL46 WL208.<[01] EMOVED INTERCOSTAL BS 312 TO BS 328 LBL 46 WL 208.1 PER SRM 51-40-02-0G-0;[02] RECIVED NEW INTERCOSTAL P/N 141A5110-12 LOCATED AND DRILLED NEW INTERCOSTAL AT BS 312 TO BS 328 LBL46 WL208; IAW 737-70SDR SWAA2023020788646Intercostal · crackedCRACKED INTERCOSTAL AT FWD WET AREA BS328+7 LBL46 WL208.<[01] REMOVED INTERCOSTAL AT FWD WET AREA BS328 TO BS344 LBL46 IAW SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED NEW INTERCOSTAL AT FWD WET AREA BS328 TO BS344 LBL46 IAW SRM 51-40-05-0G-0 DWG 141A5400; OK TOSDR SWAA2023020788647Sill Drain · crackedCRACKED FWD ENTRY DOOR MOP SILL BS294+8 LBL55 WL208.<[01] EVALUATED CRACK AT FWD ENTRY DOOR MOP SILL BS294+8'' LBL55 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-15-1A-1 PART 4.C DETAIL G; L=0.5''; TOOL USED CALIPER ID: ATS2739 S/N: A22004232 DUE DATE:11/2023;
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