JASC 5311
Service difficulty reports · 61,540
Reports filed under 5311 · Fuselage Main, Frame, 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 = '5311' 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 = '5311' 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 DALA2023050803564Unknown · unknownCRACK ON FRAMES STA Y=674 & Y=696 AT RH KEEL BEAM AREA (SM). SUMMARY OF NRC 00296: FRAMES STA Y=674 & Y=696 AT RH KEEL BEAM AREA WERE REPAIRED PER B717-200 SRM 51-70-11-2R, REPAIR 1. (LP #2753031)SDR AALA202307249590Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME AFT FACE WEB LEFT SIDE IN HORIZONTAL FLANGE RADIUS AT FR 68 AND S22L. REPAIRED FRAME PER EA 344814.SDR SWIA202302601504Unknown · crackedCO-PILOTS SIDE POST CRACKED ON BOTTOM LOWER OTBD BRACKET (C-CHECK RO 6/20/2023) REMOVED CRACKED BRACKET AND INSTALLED NEW BRACKET ON CO-PILOT SIDE POST OUTB`D SIDE REF CRJ200 SRM 51-42-21 AND DWG 601R33007 REV -U. COMPLIED WITH 51-900-1003-SKYSDR SWAA2023060145782Frame · crackedCRACK FRAME ON BS 947.5 LOCATED LBL10 AND WL178 AFT CARGO COMPARTMENT 2023-295529<[01] REPLACED FRAME LOCATED ON BS947.5 BTW STR23L TO STR23R LBL10 AND WL178 AT AFT CARGO COMPARTMENT. IAW B737-700 SRM 51-40-02; DWG 147A1047; SHEET: 107; REV: ?. DWG 147A002; SHSDR DALA2023050803562Unknown · unknownCRACK ON CUSP WEB AT STA Y=674 LH/RH ALSO STA Y=715 (X=56) RH SIDE AT PASSENGER CABIN. SUMMARY OF NRC 00415: CUSP WEB AT STA Y=674 LH/RH ALSO STA Y=715 (X=56) RH WERE REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4. (LP #2751970)SDR DALA2023050503528Unknown · unknownSHIP 3237 CRACK INDICATION ON OPEN HOLE AREA KEEL BEAM ON AFT FITTING ACTUATOR LH SIDE. CORRECTIVE ACTION: COMPLIED WITH ERA 607917-14AD REV 0,1,2,3,4,5. (8941444)SDR DALA2023050403460Unknown · unknownCORROSION ON RH CUSP WEB STA Y=474, Y=488, FROM Y=446 TO Y=465, Y=545 AND Y=575 AT PAX CABIN. SUMMARY OF NRC 00623: CORROSION LEVEL 2. RH CUSP WEB STA Y=474, Y=488, FROM Y=446 TO Y=465, Y=545 AND Y=575 WERE REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPSDR DALA2023050403459Unknown · unknownCORROSION ON LOWER SKIN OF CUSP ANGLE FROM STA 200 TO 218 AND -X=56 AT PASSENGER CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00489: LOWER SKIN OF CUSP ANGLE FROM STA 200 TO 218 AND -X=56 AT PASSENGER CABIN FLOOR STRUCTURE WAS REPAIRED PER ER/A 607622-14 REV. ORIGINASDR DALA2023050503537Unknown · unknownSHIP 6707 AA - AWR: CRACK AT 9 CLOCK POSITION IN RH INBOARD UPPER FASTENER HOLE ON FUSELAG FRAME AND LOWER HINGE FITTING AT BS 1640 FUSELAGE FRAME IN REFERENCE TO JOB 083-0001 / CARD 5311-01218- 01B. CORRECTIVE ACTION: SUMMARY OF NRC 00234: LOWER HINGE FITTINGSDR CALA2023050501359Frame · dentedAFT CARGO COMPARTMENT FRAME AT STA 1280 S-26R HAS A DENT ON THE UPPER FLANGE. REPORT (DTA). REMOVE AIRCRAFT FROM SERVICE ON OR BEFORE NOV 01, FOR DAMAGE TOLERANCE REQUIREMENTS. 2024, UNLESS ANOTHER 8110-3 FORM IS RECEIVED FINDING APPROVAL THE REPAIR INCORPORATSDR CALA2023050501356Frame · crackedCABIN FRAME IS CRACKED AT I/B FASTENER FOR PSU BRACKET STA.1120 BETWEEN S-8LT & S-9LT. [MARKED AND VERIFIED WITH HFEC] INSPECTION REQUIREMENTS AS GIVEN IN TABLE 203/REPAIR 8 ZONE 1. INSTALLATION, OR 50,000 AIRFRAME FLIGHT CYCLES, WHICHEVER COMES FLIGHT CYCLES.SDR DALA2023050403463Unknown · unknownSHIP 3237 CRACK INDICATION ON OPEN HOLE AREA KEEL BEAM ON AFT FITTING ACTUATOR LH SIDE. CORRECTIVE ACTION: COMPLIED WITH PRI 607917-14AD REV 0,1,2,3,4. (2750309)SDR DALA2023050403458Unknown · unknownCRACK EVIDENCE ON FWD LWR CORNER OF LH WINDOW BELT STA S 851 AND 908 AT PAX CAB. SUMMARY OF NRC 00408: REPAIR WAS PERFORMED PER B717-200 SRM 56-20-02-2R PROCEDURE 1. (LP #2750268)SDR SWIA2023052302Unknown · crackedCRACKED LINTEL STGR3L FS280 (C-CHECK RO 5/21/2023) REPAIRED LINTEL STGR3L FS280 REF REO 670-53-21-493 REV-D, 2015-07-10PERFORMED LEAK CHECK IAW CRJ 900 AMM 21-31-00-910-801-A02 LEAK TEST GOOD.COMPLIED WITH 51-900-1002-SKYSDR DALA2023050303432Unknown · unknownCORROSION ON CUSP WEB STA Y=529-530, Y=905-908, Y=923.5-924.5 AND Y=952-953 AND CUSP WEB STA Y=952-953 AND 975-976 RH SIDE AT PAX CABIN IN REF NRC S/N 403. SUMMARY OF NRC 00619: CORROSION LEVEL 2. CUSP WEB STA Y=529-530, Y=905-908, Y=923.5-924.5 AND CUSP WEB SSDR DALA2023050203396Unknown · unknownCORROSION ON RH CUSP WEB SPLICE LOWER SURFACE BELOW ANGLE CUSP SPLICE AT STA Y=900 X -59. SUMMARY OF NRC 00408: CORROSION LEVEL 2. RH CUSP WEB SPLICE UPPER AND LOWER SURFACE BELOW ANGLE CUSP SPLICE AT STA Y=900 X -59 WAS REPLACED PER B717-200 SRM 51-41-05-0G &SDR SWAA2023060143738Frame · crackedSTA 312 FRAME CRACKED IN RADIUS AT FED HEADER SUPPORT.<[01] ACCOMPLISED REPAIR PER EA#M-22-153-01244 ON FAULT#TTG8Q00KVLNJ;[02] 'EA-GENERAL' REPAIR REFERENCE IS SELECTED PER EA#M-22-153-01244 STEP 10;[03] VERIFIED CORRECTIVE ACTION 1 AND 2<BR><BR>VERIFIED MEASSDR DALA2023050303448Unknown · unknownSHIP 672 CORROSION ON FWD/AFT FRAME CLIPS (SHEAR TIE) STA 879 BTW STGR 29L TO 29R AT FWD CARGO COMPARTMENT. CORRECTIVE ACTION: UMMARY OF NRC 00466: FRAME CLIPS (SHEAR TIE) STA 879 BTW STGR 29L TO 29R AT FWD CARGO COMPARTMENT WERE REPLACED PER DWG 140N2002 REV.SDR IPXA2023050293074Frame · unknownINSPECTION TYPE:SEG4*MAJOR REPAIR* AFT CARGO PIT FRAME STA 1300 BETWEEN STR 23L AND 28L HAS AN EXISTING REPAIRREPAIR WAS REMOVED AND REPLACED PER UPS EO B757-5310-27523-C, UPS RCD 279262 AND VT MAE EA 757-5360-27-A3197 REV-.SDR IPXA2023050293073Frame · unknownINSPECTION TYPE:SEG4*MAJOR REPAIR* AFT CARGO PIT, FRAME AT STA 1480 BETWEEN STR 25R AND 28R HAS A EXISTING REPAIR.EXISTING REPAIR WAS REMOVED AND REPLACED PER UPS EO B757-5310-85894-A, UPS RCD 279264 AND VT MAE EA 757-5360-27-A3196 REV-.SDR DALA2023050203395Unknown · unknownCORROSION ON AFT PRESSURE BULKHEAD DOME WEB FORWARD FACE LOW AREA STA Y=1053 BTW LONGERON 29L AND 28R AT AFT CARGO COMPARTMENT. ORIGINAL THICKNESS OF 0.063IN AND REMAINING THICKNESS OF 0.045IN,.THE AREA REWORKED IS OUT OF LIMITS PER B717-200 SRM 53-20-08-2R PRSDR SWIA202306260430Unknown · crackedCLEAT AT FS260.83, STGR 4L IS CRACKED (C-CHECK RO 6/20/2023) REMOVED AND REPLACED CLEAT AT FS260.83, STGR 4L REF CRJ 200 SRM 51-42-06, CRJ 200 SRM 51-42-21 AND DRW 601R33048 REV -T. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY. SEE CONTINUATION CARSDR DALA2023050103351Unknown · unknownSHIP 3237 NEED TO RE-INSPECT EXISTING REPAIR ON FASTENERS HOLES 5, 6, C AND D FRAME 16 RH JOGGLE AREA. CORRECTIVE ACTION: COMPLIED WITH ERA 585215-14AD REV A. (2745493)SDR DALA2023050103352Unknown · unknownSHIP 3237 EXISTING FASTENER HOLES (23 EA) DIAMETER MORE THAN STARTING HOLE DIAMETER ON FRAME 16 LH JOGGLE AREA. CORRECTIVE ACTION: COMPLIED WITH ERA 608098-14AD. (2743971)SDR A6WA202304298588Frame · damagedSKIN DIMPLED AROUND 4 RIVETS ON FRAME FS379.00 BETWEEN STGR23LL AND STGR22L ***** AC REMOVED FROM SERVICE ***** REPAIRED FRAME AT FS 379 BETWEEN STRG23L AND STRG22L REF REO 601R-53-21-3628 REV -- DATED 2023-04-21SDR DALA2023050103355Unknown · unknownSHIP 3237 AT FR16 RHS, HOLES #5,#6,#C AND #D WERE FOUND PREVIOUSLY REPAIRED AND HOLE #7 WAS FOUND CRACKED. CORRECTIVE ACTION: REPAIRED PER ERA 585215-14 AD REV. ORIGINAL. (2742406)SDR DALA2023050103354Unknown · unknownSHIP 3237 AT FR16 LH DBL JOGGLE AREA, SEVERAL FASTENER HOLE LOCATIONS FOUND WITH DIAMETERS LARGER THAN MODIFICATION STARTING HOLE DIAMETERS. CORRECTIVE ACTION: COMPLIED WITH ERA 608098-32. (2742131)SDR CALA2023050101293Frame · crackedFR43 FOOT LH FASTENER HOLE HAS A CRACK LIKE INDICATION AT 12 OCL OCK AND 1 OCLOCK IN FRAME LAYER. REMOVED AND REPLACED CRACKED FR43 LH FRAME AND FRAME FOOT IAW A3 20 SRM 51-72-11-911-001 AIRBUS REPAIR DWG 53370232 AND EA 5330-0 6692-003 AND A320 SRM 51-72-11-SDR A6WA202304288587Frame · corrodedFRAME AT FS 319 HAS CORROSION REF CRJ-200 SRM 51-42-06 AND SRM 51-42-21 AND DWG 601R32003 REV P ***** AC REMOVED FROM SERVICE ***** REPLACE FRAME AT FS 319 REFSDR AALA202306097887Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME FASTENER HOLE #2 AT FR 35 AND S30L. REPAIRED FRAME PER EA 344302.SDR DALA2023042803321Unknown · unknownCORROSION ON LH CUSP WEB UPPER SIDE STA Y=421 ALSO STA Y=468 TO Y=471 IN REF NRC 00401. SUMMARY OF NRC 00614: CORROSION LEVEL 2. LH CUSP WEB STA Y=421 ALSO STA Y=468 TO Y=471 WERE REPAIRED PER B717-200 SRM 53-00-55- 2R FIG 215 AND 216. (LP #2740723)SDR CALA2023042801272Frame · crackedCABIN FRAME IS CRACKED AT I/B FASTENER FOR PSU BRACKET STA.760 BETWEEN S-8R & S-9R. [MARKED AND VERIFIED WITH HFEC] 203 ZONE 3. INSPECTION THRESHOLD 12000 FLIGHT CYCLES FROM REPAIR FIRST. REPEAT INSPECTIONS. METHOD : DETAIL VISUAL INSPECTION, (CATEGORY A REPAISDR IPXA2023051693253Frame · corrodedINSPECTION TYPE:SEG4AFT CARGO DOOR STA 1436 LOWERE INTERIOR ANGLE HAS CORROSIONREMOVED DAMAGED FRAME WEB. INSTALLED NEW FRAME WEB IAW BOEING DWG 146N6603 AND SRM 51-40-02-0GSDR R61A2023051700289Frame · unknown"FR 14 HAS THREE EACH OVERSIZED HOLES AT LOWER END WHERE IT ATTACHES TO LH NLG SPAR. REPAIRED FR 14 THREE EACH OVERSIZED HOLES AT LOWER END WHERE IT ATTACHES TO LH NLG SPAR PER ETD 2023-170-010881.SDR DALA2023042803327Unknown · unknownSHIP 5807 EXISTING REPAIR WAS FOUND IN THE INSPECTION AREA (OVERSIZE HOLE) AT STA 1640 AT LOWER I/B HOLE COMMON TO I-14F TEE. REF: ERA 590914-14. REF: STEP 4 OF AMDS 5311-01218-01A. REF N/R 226. CORRECTIVE ACTION: BHEC COMPLIED WITH ON OVERSIZED FASTENER HOLE SDR DALA2023042803325Unknown · unknownSHIP 672 EXFOLIATION CORROSION ON FRAME CLIPS STA 1480 BTW RBL 8 AND RBL 18 AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00253: FRAME CLIPS STA 1480 BTW RBL 8 AND RBL 18 AT AFT CARGO COMPARTMENT WERE REPLACED PER DWG 140N2002 REV. EU AND PER B75SDR DALA2023042703297Frame · dented(LOG 2737299) DURING INSPECTION FOUND DENT IN FRAME AT STA 727K RBL 23 WL 158 IN AFT CARGO. REPAIRED DAMAGE PER ER/A 607558-14 REV ORIGINAL.SDR DALA2023042703283Unknown · unknownSHIP 3356 DTE, ER/A 603053-14 REV A SECT DTA THRESHOLD SILL REQUIRES 3RD STAGE DTA MONITOR INSPECTION APPROVAL. CORRECTIVE ACTION: REF ER/A 603053-14. (2737701)SDR DALA2023042703281Unknown · unknownSHIP 3356 DTE, ER/A 603053-14 REV A SECT DTA SKIN REQUIRES STAGE 3 DTA MONITOR INSPECTION APPROVAL. CORRECTIVE ACTION: REF ER/A 603053-14. (2737669)SDR DALA2023042603248Unknown · unknownCORROSION ON FLOOR ANGLE BTW STA Y=200 AND STA Y=210 AND X=-54 OF AFT DOOR JAMB AT FWD SERVICE DOOR. SUMMARY OF NRC 00397: CORROSION LEVEL 2. FLOOR ANGLE BTW STA Y=200 AND STA Y=210 AND X=-54 OF AFT DOOR JAMB AT FWD SERVICE DOOR WAS REPLACED PER B717-200 SRM 5SDR DALA2023042603247Unknown · unknownCRACKED FRAME STA Y=1037 LONG 17 RH AT PAX CABIN (W2). SUMMARY OF NRC 00554: FRAME STA Y=1037 LONG 17 RH WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 4 REPAIR 4. PERFORM DECAL INSPECTION CONDITION EVERY "C" CHECK PER TOPP 30-10-70 PAGE 14 PAR I. (LP #27SDR DALA2023042603246Unknown · unknownCRACKED FRAME STA Y=1037 LONG 17 RH AT PAX CABIN (W2). SUMMARY OF NRC 00554: FRAME STA Y=1037 LONG 17 RH WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 4 REPAIR 4. PERFORM DECAL INSPECTION CONDITION EVERY "C" CHECK PER TOPP 30-10-70 PAGE 14 PAR. LOG PAGE SDR DALA2023042503243Unknown · unknownCRACK ON FRAME STA Y=1022 AND LONGERON 7RH AT PAX CABIN. SUMMARY OF NRC 00402: CRACK ON FRAME STA Y=1022 AND LONGERON 7RH AT PAX CABIN WAS REPAIRED PER ER/A 607699-14 REV ORIGINAL SECTION I, PERMANENT REPAIR AND PRI 607699-14 REV 0. ASSOCIATED ER/A 14-607699 ASDR DALA2023042703301Frame · dented(LOG 2737006) DURING INSPECTIONS, DENTS WERE DISCOVERED ON THE INNER CHORD OF THE BS 727K FRAME WEB (P/N: 146A1255-11 & 146A1255-12), BETWEEN S-23R AND S-26R AT APPROX. RBL 22.50 AND RBL 31.50. MAINTENANCE REPAIRED DAMAGE PER ERA 607558-14.SDR VNAA202304270004Frame · corrodedCORROSION ON FRAME FS= 364.00 BETWEEN STRG 26RH TO 26RH AT MAIN AVIONICS COMPARTMENTSDR DALA2023042503242Unknown · unknownCRACK ON FRAME STA Y=1022 AND LONGERON 7LH AT PAX CABIN. SUMMARY OF NRC 00299: CRACK ON FRAME STA Y=1022 AND LONGERON 7LH AT PAX CABIN WAS REPAIRED PER ER/A 607681-14 REV ORIGINAL SECTION I, PERMANENT REPAIR AND PRI 607681-14 REV 0. ASSOCIATED ER/A 14-607681 ASDR DALA2023042503241Unknown · unknownCRACKED FRAME STA Y=1037 LONG 17 LH AT PAX CABIN (W2). SUMMARY OF NRC 00553: FRAME STA Y=1037 LONG 17 LH WAS REPAIRED PER B717-200 SRM. 53-20-07-2R PROCEDURE 4 REPAIR 4. (LP #2735918)SDR CALA2023042401242Frame · crackedLH FR 16 UPPER DOUBLE JOGGLE AREA HOLE 6 HAS CRACK INICATION IN FRAME LAYER AT 2 O''CLOCK DIRECTION PER HAECO LCQ N/R 9298535/ 40535 GEN BY V892444 JOGGLE REPAIRED HOLES #E AND #F PER PART 2 OF THE LATEST 38884 TOTAL AIRCRAFT CYCLES. ACCOMPLISH REPEAT INSPECTISDR LR7A2023042303286Ring · crackedDURING SCHEDULED B-1 CHECK UNDER JOB CARD HB 5302, FOUND FS979 RH RING SEGMENT CRACKED AT RBL66, WL265. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 53-50-07. NR# 1000939823.SDR AALA202305054097Frame · corrodedAIRCRAFT IN BASE MAINTENANCE: CORRODED FRAME LOCATED BETWEEN 312 AND 325, AND STR 23L. REPAIRED FRAME WITH REINFORCEMENT PER EA.
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