JASC 5311
Service difficulty reports · 61,524
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 YENA2026092300895Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION FOUND IN HOLE C LOCATED AT DOUBLE JOGGLE AREA, FR16 RT SIDE. CRACK DIRECTION IS 9 OCLOCK VIEW FROM OUTSIDE. CRACK DEPTH IS 0.165 INCH APPROX. CONFIRM CRACK INDICATION USING BOROSCOPE VIEW IAW NTM 51-90-00. PERFORMED SDR YENA2026092300894Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION FOUND IN HOLE 7 LOCATED AT DOUBLE JOGGLE AREA, FR 20 R H SIDE. CRACK DIRECTION IS 3 OCLOCK VIEW FROM OUTSIDE. CRACK DEPTH IS 0.165 INCH APPROX. CONFIRM CRACK INDICATION USING BOROSCOPE VIEW IAW NTM 51-90-00. PERMANESDR YENA2026092300893Frame · crackedDURING HEAVY MAINTENANCE, A CRACK INDICATION WAS FOUND IN HOLE B IN DOUBLE JOGGLE AREA, FR 16. CRACK DIRECTION IS 3 OCLOCK VIEWED FROM OUTSIDE. CONFIRMED CRACK INDICATION USING BOROSCOPE IAW NTM 51-90-00. PERFORMED A PERMANENT REPAIR OF FRAME 16 IAW SRM 53SDR AALA202610230574Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON FRAME 16 LEFT SIDE UPPER DOUBLE JOGGLE AREA OPEN FASTENER HOLE 6, CRACK DIRECTION IS 3 O'CLOCK, CRACK DEPTH IS 0.120 INCH APROXIMATELY AT FORWARD GALLEY AREA. MAINTENANCE PERFORMED TIME LIMITED REPAIR ON FRAME SDR ABXA20260918425Frame · crackedDURING AIRCRAFT C-5 CHECK, MAINTENANCE DISCOVERED A CRACK IN THE BS 1809.5 BULKHEAD AFT OUTER FRAME BETWEEN S-5L AND S-6L. THIS CRACK IS OUT OF LIMITS IAW SRM AND NO APPLICABLE REPAIR IS GIVEN IN THE SRM. THE BS 1809.5 BULKHEAD AFT OUTER FRAME IS CONSIDERED SDR ABXA20260918421Frame · crackedDURING AIRCRAFT C5 CHECK, MAINTENANCE DISCOVERED CRACK INDICATIONS ON THE RT INNER FRAME AT STA 903.5 WHILE ACCOMPLISHING AN HFEC SURFACE SCAN IAW REF D. AN OPEN HOLE HFEC WAS COMPLETED IAW REF D WHERE IT WAS DISCOVERED THAT THE UPPER MOST FASTENER HOLE HADSDR CALA2026092119626Frame · corrodedAFT CARGO FR 59 HAD CORROSION AT FASTENER HOLES. PERFORMED PERMANENT A REPAIR AT FR 59 IAW EC/RA 5341-01583.SDR YENA2026091800851Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 35 BULK HEAD RH SIDE AT LEVEL OF STGR 30 AT OPEN FASTENER HOLE LOWER OUTBOARD COMMON TO MILLED COUPLING, CRACKED DIRECTION IS 9OCLOCK, CRACK DEPTH IS 0.120 INCH APPROX., IN FWD CARGO COMPARTMENT (1EA); (RESOSDR YENA2026091800850Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 35 BULK HEAD LH SIDE AT LEVEL OF STGR 30 AT OPEN FASTENER HOLE LOWER OUTBOARD COMMON TO MILLED COUPLING, CRACK DIRECTION ARE 4 AND 9OCLOCK, CRACKDEPTH IS 0.120 INCHAPOROX., IN FWD CARGO COMPARTMENT (2EA); (RESDR YENA2026091800849Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 35 RH SIDE AT LEVEL OF STGR 30 AT OPEN FASTENER HOLE LOWER AFT COMMON TO SKIN,CRACK DIRECTIONS ARE 2 AND 6 OCLOCK, CRACK DEPTH IS 0.110 INCH APPROX, IN FWD CARGO COMPARTMENT (2EA); (RESOLVED ON W/O: 1435456 TSDR YENA2026091800848Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 35 LH SIDE AT LEVEL OF STGR 30 AT OPEN FASTENER HOLE LOWER AFT COMMON TO SKIN,CRACK DIRECTIONS ARE 11 AND 6 OCLOCK, CRACK DEPTH IS 0.110 INCH APPROX, IN FWD CARGO COMPARTMENT (2EA); (RESOLVED ON W/O: 1435456SDR YENA2026091800847Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 RH SIDE IN PRESSURE DECK MEMBRANE OPEN FA STENER HOLE 2 INCH O/B FROM -Y1292 APPROX.,CRACK DIRECTION IS 12 OCLO CK, CRACK DEPTH IS 0.085 INCH APPROX., IN FWD CARGO COMPARTMENT (1 EA ); (RESOLVED ON W/O: 14SDR YENA2026091800846Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 RH SIDE IN PRESSURE DECK MEMBRANE OPEN FA STENER HOLE 3 INCH O/B FROM -Y1292 APPROX.,CRACK DIRECTION IS 6 OCLOC K, CRACK DEPTH IS 0.085 INCH APPROX., IN FWD CARGO COMPARTMENT (1 EA); (RESOLVED ON W/O: 1435SDR YENA2026091800845Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 RH SIDE IN PRESSURE DECK MEMBRANE OPEN FASTENER HOLE 5 INCH O/B FROM -Y1292 APPROX.,CRACK DIRECTION IS 12 OCLO CK, CRACK DEPTH IS 0.085 INCH APPROX., IN FWD CARGO COMPARTMENT (1 EA ); (RESOLVED ON W/O: 143SDR YENA2026091800844Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 RH SIDE IN PRESSURE DECK MEMBRANE OPEN FA STENER HOLE Ñ 20, CRACK DIRECTION IS 12 OCLOCK, CRACK DEPTH IS 0.085 I NCH APPROX., IN FWD CARGO COMPARTMENT; (RESOLVED ON W/O: 1435456 TASKCARD: NR-00058 ) ACCOMSDR YENA2026091800843Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 RH SIDE IN PRESSURE DECK MEMBRANE OPEN FA STENER HOLE Ñ 19, CRACK DIRECTION IS 12 OCLOCK, CRACK DEPTH IS 0.081 I NCH APPROX., IN FWD CARGO COMPARTMENT; (RESOLVED ON W/O: 1435456 TASKCARD: NR-00059 ) ACCOMPSDR YENA2026091800842Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 RH SIDE IN PRESSURE DECK MEMBRANE OPEN FA STENER HOLE Ñ 14, CRACK DIRECTION IS 6 OCLOCK, CRACK DEPTH IS 0.094 IN CH APPROX., IN FWD CARGO COMPARTMENT ALL WORK ACCOMPLISHED ON AEROMAN WO 2026 279/1 NR2026-3SDR YENA2026091800841Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 RH SIDE IN PRESSURE DECK MEMBRANE OPEN FA STENER HOLE Ñ 22, CRACK DIRECTION IS 12 OCLOCK, CRACK DEPTH IS 0.085 I NCH APPROX., IN FWD CARGO COMPARTMENT; (RESOLVED ON W/O: 1435456 TASKCARD: NR-00061 ) ACCOMPSDR YENA2026091800840Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 RH SIDE IN PRESSURE DECK MEMBRANE OPEN FA STENER HOLE Ñ 23, CRACK DIRECTION IS 12 OCLOCK, CRACK DEPTH IS 0.079 I NCH APPROX., IN FWD CARGO COMPARTMENT; (RESOLVED ON W/O: 1435456 TASKCARD: NR-00062 ) ACCOMPSDR YENA2026091800839Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 RH SIDE IN PRESSURE DECK MEMBRANE OPEN FA STENER HOLE Ñ 24, CRACK DIRECTION IS 12 OCLOCK, CRACK DEPTH IS 0.082 I NCH APPROX., IN FWD CARGO COMPARTMENT; (RESOLVED ON W/O: 1435456 TASKCARD: NR-00063 ) ACCOMPSDR YENA2026091800834Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 LH SIDE IN PRESSURE DECK MEMBRANE OPEN FA STENER HOLE 6 INCH O/B FROM Y1292 APPROX.,CRACK DIRECTION IS 6 OCLOCK , CRACK DEPTH IS 0.085 INCH APPROX., IN FWD CARGO COMPARTMENT (1 EA);(RESOLVED ON W/O: 143545SDR YENA2026091800832Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 RH SIDE IN PRESSURE DECK MEMBRANE OPEN FA STENER HOLE Ñ 16, CRACK DIRECTION IS 12 OCLOCK , CRACK DEPTH IS 0.080 INCH APPROX., IN FWD CARGO COMPARTMENT; (RESOLVED ON W/O: 1435456 TASKCARD: NR-00070 ) ACCOMPSDR HNAA2026102901052Frame · damagedAFTER REMOVAL OF SILL FOUND ELONGATED HOLE IN FR 54. PERFORMED CUTOUT AND SPLICE REPAIR OF ELONGATED HOLE IN FR 54 IAW SRM 53-00-04-RE, ITEM 14, FIG 206, AND ETD2026-145-016208.SDR IPXA2026100101667Frame · crackedMAJOR REPAIR. CENTER FUSELAGE BASE FRAME FITTING FR44 LT HAS SIGNS OF CRACK. CRACK EXTENDS ENTIRE TOP SURFACE AND STOPS JUST PAST EDGE ON FWD SURFACE OF FRAME. ACCOMPLISHED REPAIR IAW EO 46789-JIC 7 AND EO-46789-REQ 6 (APPX J).SDR IPXA2026100101697Frame · crackedMAJOR REPAIR. CENTER FUSELAGE BASE FRAME FITTING FR45 LH SIDE HAS SIGNS OF CRACK. AFTER FURTHER EVALUATION FOUND CRACK LENGTH IS 0.100". ACCOMPLISHED REPAIR IAW EO 46789-JIC 7 AND EO-46789-REQ 6 (APPX J).SDR AALA202610198019Rib · crackedAIRCRAFT IN BASE MAINTENANCE: RH HORIZONTAL STABILIZER - CRACKED RIB AT STAB STA 92.70 LOCATED ON THE 2ND STIFFENER AFT OF THE FRONT SPAR (20" FROM THE FWD SPAR). REPAIRED IAW 55-10-09-2R-4.SDR AALA202610194023Rib · crackedAIRCRAFT IN BASE MAINTENANCE: LH HORIZONTAL STABILIZER RIB CRACKED AT STAB STA 101.92, 2ND STIFFENER FROM FWD SPAR. REPAIRED IAW 55-10-09-2R-4.SDR N6WA2026091816Frame · corrodedCORROSION BS 250 BETWEEN STRG 25L - 25R. REMOVED AND REPLACED FRAME AT BS 250 BETWEEN STRG 25L & 25R IAW SRM 51-42-06.SDR DALA2026091805204Frame · crackedCRACK ON FRAME STA Y=1200, REPAIRED FRAME PER B717-200 SRM 53-30-08-2R. (1816798) (AIRCRAFT GROUNDED).SDR 2A6R2026091675406Frame · crackedDAMAGE WAS DISCOVERED ON THE CABIN OVERHEAD LONGERON (PN: L533M1017282) IN THE FORM OF TWO CRACKS ON EITHER SIDE OF THE CUTOUT. THE CRACK MEASURES APPROXIMATELY 0.50” LONG (AFT) AND 1.00” LONG (FWD)SDR IPXA2026100555363Frame · not groundedEXISTING REPAIR FOUND AT AFT CARGO COMPARTMENT FRAME STA 1460 L/H. ACCOMPLISHED THE REPAIR PER EO-98750-REQ1 AND STE-PNA EA 757-5360-27-A4633, REV. -.SDR CALA2026091719502Frame · dentedAFT CARGO THROUGH SIDEWALL PANEL AT STA 1560, RT FRAME HAS A DENT, STR 25R - 26R. REPAIR ACCOMPISHED IAW ECRA 5360-02211 AND EA 757-5360-13-A4610, REV, EA 8110-3.SDR SWAA2026102118881Frame · crackedCRACKED FRAME, BS 312, STR 5 - 6L IN THE FWD GALLEY AREA. PERFORMED A REPAIR TO THE FRAME IAW M-22-153-01244.SDR DALA2026091805225Frame · crackedA CRACK WAS FOUND OF 0.125IN LENGTH APROX. ON FUSELAGE FRAME STA. 1640 JUST BELLOW STGR 14 LH. REPAIRED PER ERA 636323-14AD (1813334)(AIRCRAFT GROUNDED)SDR REXA2026091501828Frame · corrodedFS 549 FRAME IS CORRODED BETWEEN STGR 17L AND STGR 18L. COMPLIED WITH REO 690-53-31-1169 REV -- DATED 2026-09-09.SDR SWAA2026102142780Stub Frame · crackedCRACK INDICATION ON STUB FRAME BTWN BS 294.5 & 296.5, STRINGER 8R & 9R ON THE FWD GALLEY DOOR AREA . REPLACED THE STUB FRAME IAW SRM 51-10-02-0G-0, ITEM 9, SRM 51-40-02-0G-0, DWG 141A8370, SHT 10, REV -, & DWG 141A8380, SHT 21, REV -.SDR SWIA2026091177516Fastener · missingFASTENER MISSING IN FR18 BETWEEN STR 2R-3R. PERFORMED PERMANENT BUSHING REPAIR AT FR18 BETWEEN STGR 2R-3R REF ETD2026-170-015731.SDR DALA2026091605165Repair · abnormalEXISTING REPAIR WAS FOUND ON AFT FACE OF FRAME, THAT PREVENT THE LINER HOLE GENERAL VISUAL INSPECTION. STA. 1640 BTW S-14RL TO S-16RL AT FUSELAGE. REPAIRED PER ER/A 00-570836. (1808051)(AIRCRAFT GROUNDED)SDR VNAA2026091115Frame · crackedBS 333 FRAME IS CRACKED BETWEEN STR 1R AND STR 2R. REPAIRED BS 333 FRAME IAW REO 670-53-21-2830, REV-.SDR UIEA2026083100832Frame · crackedONE CRACK FOUND ON BS 1809.5 BULKHEAD FWD OUTER FRAME BTWN STRS 6R-7R. RADIUS AREA APPROX 3/4 LENGTH. OUTER FRAME AREA REPAIRED IAW EO 6753A030, REV 16, PART 10, AND RI-53-80-18470, REV A. NO FURTHER DEFECTS NOTED.SDR UIEA2026083100833Frame · crackedLEFT BS 1809.5 BULKHEAD OUTER CHORD HOLE, FOUND CRACK IN SKIN LAYER. CRACKED FASTENER HOLE, REPAIRED IAW RI-53-81-18478, REV A. NO FURTHER DEFECTS NOTED.SDR HNAA2026101500984Frame · crackedFR 59 CRACKED BTW STR 15-16L. REPAIRED IAW ETD2026-145-015641SDR SWAA2026101433592Frame · crackedCRACKED FRAME, BS 312, STR 5L - 6L. REPAIRED THE FRAME IAW EA M-22-153-01244.SDR KCSA202609091204Frame · crackedDURING EO 5312-21-02 OPEN HOLE HFEC INSPECTION, A CRACK SIGNAL INDICATION ON FRAME AT BS 860 RT 3 EA HOLE.SDR KCSA202609091201Frame · crackedDURING OPEN HOLE HFEC INSPECTION, CRACK SIGNAL INDICATIONAT LT BS 840 FRAME AND CHORD 3EA, FWD DOUBLER 1 EA, AFT DOUBLER 1 EA.SDR ASAA2026090869245Doubler · corrodedAFT CARGO RH FRAME BS 787 DOUBLER CORRODED. GROUNDED - YES. REMOVED DAMAGE, FOUND TO BE OUT OF LIMITS, REMVOED AND REPLACE DOUBLER IAW SRM 51-40-02-0G-0SDR DALA2026091105088Frame · corrodedCORROSION R/H SIDE FRAME PART # C02382152-102 AT MULTIPLE LOWER PANEL FASTENER HOLES. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0537:2090-2001/007 00307 REMOVED AND REPLACED FRAME PER REF A220 ASRP 51-42-00. (LP# 1800973; AIRCRAFT WAS GROUNDED)SDR DALA2026090905056Frame · damagedLEFT BS 727 FRAME INNER CHORD,737 REPAIR; RII; SECTION 02 IN REF TO THE AMDS 5311-01251-02A. IN REF TO THE AMDS 5311-01251-02A STEP 13. SDR REPORTABLE WAS PERFORMED ASSOCIATED WITH THE REPAIR PER TOPP 20-50-20. ASSOCIATED AA 5311-01251. (1802180) AIRCRAFT WASSDR DALA2026090905055Frame · damagedRIGHT HAND BS 727 FRAME INNER CHORD, 737 REPAIR; RII; SECTION 02 IN REF TO THE AMDS 5311-01251-02B. IN REF TO THE AMDS 5311-01251-02B STEP 13. PERFORMED THE REPAIR PER TOPP 20-50-20. (1802165) AIRCRAFT WAS GROUNDEDSDR IPXA2026101816920Frame · crackedAFT CARGO COMPARTMENT FUSELAGE FRAME HAS A CRACK APPROX AT BS 1500, STGR 26R. ACCOMPLISHED REPAIR IN ACCORDANCE WITH EO-98861REQ1 AND EA 757-5360-01-B0826, REV IR.
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