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 SWIA2026050476416Frame · corrodedAVIONICS BAY FUSELAGE FRAME AT BS 349 BETWEEN S27 AND S26L CORRODED IN MULTIPLE SPOTS. REMOVED AND REPLACED CORRODED FRAME AT BS 349 WITH NEW FRAME AT BS 349 USING ALL NEW FASTENERS IAW DWG SH670-31351, REV.C, DWG SH670-31350, REV A AND SRM 51-42-06-001-001-ASDR REXA2026070301043Frame · corrodedCORROSION ON FRAMES (5E/A) FS 469 BTW STGR 26L TO STGR 25L,FS 661+74 BTW STGR 26R TO STGR 27, FS 661+62 BTW STGR 26R TO STGR 26L , FS 661+32 STGR 26R TO STGR 27 AND FS 661+41 STGR 26R TO STGR 27 AT FWD CARGO COMPARTMENT. CORROSION ON FRAMES FS 661+74 BTW STGRSDR REXA2026070301041Frame · damagedSECONDARY NRC FROM NRC 006 DURING THE REMOVAL OF AFT RAIL DOUBLER (CHANNEL): TWO ELONGATE HOLES WERE FOUNDED ON FRAME STA 1047 BTW STRINGER 17LH AND 16LH ELONGATE HOLES ON FRAME STA 1047 BTW STRINGER 17LH AND 16LH WERE REPAIRED PER REO 690-53-61-1774 REV. - -SDR SWAA2026060895156Frame · crackedCRACKED FRAME, BS 312, BTW STR 5L & STR 6L IN THE PASSENGER CABIN. REPAIRED THE FRAME IAW EA M-22-153-01244.SDR DALA2026050602884Frame · corrodedCORROSION ON FRAME 75 AFT SIDE JUST FORWARD OF WASTE CUTOUT OTBD OF STR 36L AT GROUND STUD G7329. ACCOMPLISHED ER/A 633524-14 REV-ORIGINAL. ASSOCIATED ER/A 14-633524 ADDED FOR AC 8135. (LP# 1575768; AIRCRAFT WAS GROUNDED)SDR DALA2026050502821Frame · crackedCRACK ON CANTED FRAME AT Y=1200 AND PROJECTION. REPAIRED PER SRM 51-70-11-2R (1574671) (AIRCRAFT GROUNDED)SDR DALA2026050402807Frame · corrodedIN REFRRENCE AMDS 5211-6001-4R: AFTER REMOVAL OF SLIDE INDICATOR POSITION, CORROSION WAS FOUND ON FRAME WEB, R4 DOOR. CORROSION LEVEL 2. FRAME WEB, R4 DOOR WAS REPLACED IAW SRM 51-40-02-0G PAR. 4.B, PAR. 5.B, PAR. 6 .B AND PAR. 7.D. (1574721) AIRCRAFT WAS GRSDR DALA2026050402805Frame · crackedA CRACK WAS FOUND OF 0.156IN LENGTH APROX. ON BS 1640 RT FUSELAGE FRAME INNER CHORD FWD RETURN FLANGE RADIUS JUST BELOW STGR 14R. RH FUSELAGE FRAME STA. 1640 INNER CHORD FWD WAS REPAIRED PER ER/A 588298-14AD REV. C SECTION III: PERMANENT REPAIR #2 AND PRI REVSDR AALA202605010388Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN THE RIGHT HAND SIDE AT BS 328 FRAME WEB BETWEEN STR 20R AND STR 21R. INSTALLED SPLICE STRAP REPAIR ON FRAME WEB. PER EA374061 AND NR# 850.SDR AALA202606221983Frame · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FRAME AT FR 16 BETWEEN S22L AND S23L. REPAIRED FRAME PER EA 375284.SDR SWAA2026052793950Frame · crackedCRACK ON FRAME LOCATED BS 312 BTW STR 5L TO STR 6L AT FWD GALLEY AREA. PERFORMED PERMANENT REPAIR FRAME LOCATED BS 312 BTW STR 5L TO STR 6L AT FWD GALLEY AREA I.A.W B737-800 EA M-22-153-01244.SDR SWAA2026052094057Frame · damagedELONGATED HOLE ON FRAME, BS 727C, WL 156.4, RBL 22. PERFORMED OVERSIZE HOLE LOCATED ON FRAME BS 727C IAW SRM 51-40-02-0G-0.SDR DALA2026050502815Frame · crackedCRACK ON FRAME STA Y=1037 ON LONGERON 17R AT CPAX. REPAIRED PER SRM 53-20-07 (1569682) (AIRCRAFT GROUNDED)SDR DALA2026050102761Frame · corrodedCORROSION LEVEL 2 WEB FRAME 16 AT LEVEL STR 23L AT FWD GALLEY AREA. REPLACED WEB AND FASTENERS LOCATED BTW FR12 TO FR16 AT LEVEL STR23L AT FWD GALLEY AREA AS PER A319 SRM 51-42-11, A319 SRM 51-72-11. (LP 1569531 - AIRCRAFT WAS GROUNDED)SDR CALA2026050115916Frame · mechanic errorAFT CARGO BAY FR. 60 LT FASTENER HOLE STRINGER 37 VERTICAL FLANGE HOLE MISDRILLED. FASTENER HOLE AT FRAME 60, STRINGER 37 LEFT, VERTICAL FLANGE REPAIRED PER EC/RA 5341-01568 AND REQUIRES REPETITIVE INSPECTIONS.SDR DALA2026043002753Frame · crackedERA 588298-14, MONITOR INSPECTION LOG REPAIR TO FUSELAGE BS 1640 FRAME BETWEEN RH INTERCOSTAL 9F AND S -20R CRACKED. REF ERA 588298-14AD. AIRCRAFT WAS GROUNDEDSDR SWIA2026042877017Frame · corrodedFRAME SECTOR F.S.310 IS CORRODED AT SEVERAL LOCATIONS BETWEEN STRINGERS 26L AND 22R (C-CHECK RO 08/28/2026)COMPLIED WITH MAJOR REPAIR OF FRAME SECTOR F.S.310 IS CORRODED AT SEVERAL LOCATIONS BETWEEN STRINGERS 26L AND 22R IAW CRJ 200 SRM 51-40-11, 51-42-06, ANSDR SWIA2026042877011Frame · corrodedFRAME SECTOR F.S.349 IS CORRODED BETWEEN STRINGERS 26L AND 26R. (C-CHECK RO 08/28/2026)REMOVED CORRODED FRAME SECTOR AT FS349 BETWEEN STGR23L - STGR23R, AND LOCATED, DRILLED, AND INSTALLED NEW SERVICEABLE FRAME SECTOR PN# 601R32005-69 AT SAME LOCATION IAW CRJSDR SWIA2026042877006Frame · corrodedFRAME BS 364 IS CORRODED AT STRINGER 26R (C-CHECK RO 08/28/2026)PERFORMED MAJOR REPAI OF REPLACING FRAME SECTOR AT FS364 FROM STRG 24L TO STRG 24R IAW CRJ 200 SRM 51-42-06 AND 51-42-21 REV 39B DATED 10/28/2024. COMPLETED AND ATTACHED MAJOR REPAIR 337 FORM. CSDR SWAA2026051993490Stub Frame · crackedFSD STUB FRAME IS CRACKED AT BS 296; BETWEEN STR 8 AND 9 RT; CRACK IS 0.6' LONG LOCATED IN THE FRAME JOGGLE AREA LOCATED ABOVE THE TOP END OF THE SEAL DEPRESSOR; CONTACT ENGINEERING VIA THE TSR POLICY NOTE THE CRACK WAS FOUND USING HFEC. REMOVED AND REPLACED SDR KCSA202604281037Frame · crackedCRACKED FRAME WEB AT STA 1480 IN R/H BODY GEAR WHEEL WELL.SDR SWAA2026060193394Frame · crackedCRACK FRAME BS 312 BTW STR 5L TO STR 6L AT PASSENGER CABIN. REPAIRED FRAME BS 312 BTW STR 5L TO STR 6L AT PASSENGER CABIN IAW EA M-22-153-01244.SDR SWIA2026042576863Frame · corrodedBS 333 FRAME CORRODED ON THE FWD FACE AND LOWER FLANGE BTWN STR 23R & STR 22R. R & R FRAME SEGMENT AT BS 333 FROM STR 18R TO STR 23R IAW SRM 51-42-06 AND 51-42-21. COMPLETED TASK CARD 51-900-1003-SKY.SDR SWIA2026042576855Frame · corrodedBS 310 FRAME CORRODED ON THE AFT FACE BETWEEN STR 22R & 23R. R & R THE FRAME IAW SRM 51-42-06, 51-42-21, AND SKY CARD 51-900-1003-SKY.SDR SWIA2026042576848Frame · corrodedBS 319 FRAME CORRODED ON THE FWD FACE BTWN STR 23R AND STR 22R. R & R FRAME SPLICE COMMON TO FRAME BS 319.00, S23R - S22R IAW SRM 51-42-06 AND SRM 51-42-21. COMPLETED TASK CARD 51-900-1003-SKY.SDR AALA202606164739Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME AT FR 66 AND S11R AT THE #7 DOOR STOP AREA. REPAIRED FRAME PER SRM 53-41-12-300-011.SDR HNAA2026060200450Frame · corrodedF122812 CORROSION IN CARGO COMPARTMENT ON FRAME 61 WEBBING AT STRINGER 16R. REMOVED AND REPLACED WEBBING PANEL AT FRAME 61 (BANANA PANEL) IAW EMB 145 SRM 51-40-02SDR FDEA202604240530Frame · crackedINSPECTION OF FR40 LOWER JUNCTION FASTENER HOLE NR 3 RT SIDE FOUND CRACK SIGNAL. COMPLIED WITH EA:6-5710-T0387217 P1 TO REPAIR FR40 RH SIDE LOWER JUNCTION CRACKED FASTENER HOLE #3, MAJOR REPAIR IAW FEDEX GMM6-2-100. SEE WRI 57107960 FOR WORK DETAILS.SDR SWIA2026042376865Frame · crackedBS 235, RT UPPER FRAME SECTOR IS CRACKED WHERE IT ATTACHES TO THE RT WINDOW LOWER SILL. REPAIRED THE RT UPPER FRAME SECTOR IAW REO 601R-53-11-4073, REV - AND SKY CARD 51-900-1003-SKY.SDR SWIA2026042376859Frame · crackedBS 235 LT UPPER FRAME SECTOR IS CRACKED WHERE IT ATTACHES TO THE LT WINDOW LOWER SILL. REPAIRED THE LT UPPER FRAME SECTOR CRACK WHERE IT ATTACHED TO THE LH WINDOW LOWER SILL IAW REO 601R-53-11-4072, REV -, & SKY CARD 51-900-1003-SKY.SDR CALA2026042815746Frame · gougedAPU DOOR ASSY FRAME HAS A DEEP GOUGE LOCATED AFT OF THE AFT HINGE. REPAIRED APU DOOR ASSY FRAME STA 1154.60 LBL 18 AS PER EC/RA 5240-01751.SDR DALA2026042802670Frame · damagedDURING HCK, A DISCREPANCY WAS NOTED ON THE STA 1417 FUSELAGE FRAME AT STRINGER 38R. DAMAGED AREA REPAIRED PER ER/A 75-633830 (1557607) (AIRCRAFT GROUNDED)SDR DALA2026042802669Frame · damagedDURING HCK, A DISCREPANCY WAS NOTED ON THE BS 1562 FUSELAGE FRAME AT STRINGER 38L. REPAIRED PER ER/A 633785-14AD (1557529) (AIRCRAFT GROUNDED)SDR DALA2026042302604Frame · crackedINITIAL INSPECTION: CRACK ON CAP IN FRAME Y=1022 AND L 7R AT CPAX. REPAIR AND PRI 633416-14 (1557376) (AIRCRAFT GROUNDED)SDR HNAA2026052000420Frame · crackedCRACKED FRAME 72, BETWEEN STRINGER 17L AND 16L. R & R FRAME 72 IAW ETD-2026-145-007557 AND EO1-53-26-0206.SDR 2A6R2026042175104Frame · dentedA LARGE DENT WAS DISCOVERED ON THE TRANSMISSION DECK SKIN AND CENTER BEAM PN: 355A21-2109-21. THE DAMAGE TO THE DECK SKIN IS APPROXIMATELY 0.060” DEEP AND 3.5” WIDE BY 2.5” LONG. THE DAMAGE TO THE CENTER BEAM HAS AN AREA OF 2.0” WIDE AND 1.3” HIGH ON THE VERTISDR N6WA2026042005Frame · crackedFRAME AT FS235 IS CRACKED. REMOVED AND REPLACED THE RH FRAME AT FS235 IAW CRJ SRM 51-41-06.SDR SWIA2026041776852Frame · corrodedBS 333 FRAME CORRODED BTWN STR 20L TO STR 21L. R & R BS 333 FRAME, STR 20L - 23L IAW SRM 51-42-06, AND SRM 51-42-21, COMPLETED TASK CARD 51-900-1003-SKY.SDR SWIA2026041776845Frame · corrodedBS 319 FRAME CORRODED BTWN STR 20L TO STR 21L. R & R THE FRAME SECTOR AT BS 319 BTWN STR 18L & 21L IAW SRM 51-42-06, & 51-42-21. COMPLETED TASK CARD 51-900-1003-SKY.SDR SWIA2026041776314Frame · chafedDURING AUDIT OF TASK CARD 53-350-500 IT WAS FOUND THAT THERE IS A CHAFED FRAME AREA AFT OF APU EXHAUST BS 654.50. REPAIRED FRAME AFT OF APU EXHAUST BS 654.5 IAW SRM 51-42-06, 51-42-21, DWG 601R35004, REV BJ, AND REO 601R-53-61-8529, REV.--. COMPLIED WITH TASSDR IPXA2026060556348Frame · crackedCWB CENTER SPAR WEB REINFORCEMENT LH SIDE. 1(EA) INBOARD UPPER FASTENER HOLE CRACKED. VERIFIED E.A.#300-5710-27-A4452, PRELIMINARY 3, STEP 14. C/W VERIFIED BLAIN BUSHES (3EA) INSTALLED WITH NITROGEN LIQUID IN AFFECTED HOLE AS PER FIGURE 2, REPAIR DWGS R007-12SDR IPXA2026060556413Frame · crackedCWB CENTER SPAR WEB REINFORCEMENT RH SIDE. 1(EA) INBOARD UPPER FASTENER HOLE CRACKED. ZONE 142 OUT OF SEQ. INSTALLED WITH NITROGEN LIQUID IN AFFECTED HOLE AS PER FIGURE2, REPAIR DWGS R007-12001 ISSUE C. ACCOMPLISH THE PERMANENT REPAIR PER EO-97608-REQ1 AND SDR SWAA2026052090277Stub Frame · crackedCRACK INDICATION FOUND ON STUB FRAME, BS 294.5, 4.2 INCHES BELOW STRINGER 8R. REPLACED STUB FRAME IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 141A8370, SHEET 9, & 10, REV D.SDR DALA2026042002488Frame · not reportedLEFT BS 727 FRAME INNER CHORD, 737 REPAIR; RII; SECTION 02. ACCOMPLISHED AMDS 5311-01251-02A - LEFT HAND STA 727 FRAME INNER CHORD, 737 REPAIR; RII; SECTION 02. SHIM WAS INSTALLED ASSOCIATED AA 5311-01251 ADDED FOR AC 3710. (LOG 1548168 - AIRCRAFT WAS GROUNDEDSDR SWAA2026051289622Frame · crackedBS 312 FRAME UPPER ANGLE CRACKED AT LBL33 BETWEEN S-5L AND S-6L. REPAIRED PER EA# M-22-153-01244.SDR DALA2026041702440Frame · damagedEXISTING REPAIR LOC. FR 53 AT LEVEL STR 36L ON AFT CARGO COMPARMENT REFERENCE WC 5311-01200-01, AD 2023-06-08. NO MAINTENANCE ACTION TAKEN DUE TO INSPECTION ON TACK HOLES FRAME 53 STRG 36L TO 37L IS COVERED BY EXISTING REPAIR AND IS N/A IAW ER/A 598460-14AD RSDR DALA2026041602430Frame · not reportedLEFT HAND STA 727 FRAME INNER CHORD, 737 REPAIR; RII; SECTION 2 IN REFERENCE TO AMDS 5311-01251-02A STEP 13. IN REF TO AMDS 5311-01251-02A STEP 13. SDR REPORTABLE WAS PERFORMED ASSOCIATED WITH THE REPAIR PER TOPP 20-50-20. ASSOCIATED AA 5311-01251 ADDED FOR ACSDR 2A6R2026041475304Frame · crackedCRACKING DAMAGE WAS DISCOVERED ON THE TAIL CONE UPPER FRAME 7 IN THE RADIUS ADJACENT TO THE SKIN FLANGE ON THE R/H SIDE. THE APPROXIMATE LENGTH OF THE CRACK WAS MEASURED AT 0.20”. THE CRACK WAS STOP DRILLED AND AN L-SHAPED REPAIR DOUBLER OF 0.050” ALUMINUM WASDR DALA2026041502387Frame · damagedPERFORM RIGHT BS 727 FRAME INNER CHORD, 737 REPAIR, IAW AMDS 5311-01251-02B STEP 13. PERFORMED ASSOCIATED WITH THE REPAIR PER TOPP 20-50-20. ACFT WAS GROUNDED.SDR DALA2026041402376Frame · damagedFUSELAGE FRAME OUTER FLANGE REINFORCING REPAIR AT FUSELAGE FRAME 67, OUTER FLANGE NEEDS TO BE RE-WORKED. RE-WORKED THE REPAIR PER ERA 632813-14 REV ORIGINAL. (1543868) AIRCRAFT WAS GROUNDED.
Back to JASC 5311