JASC 5311
Service difficulty reports · 61,537
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 UIEA2025022500160Frame · corrodedAFT CARGO COMPARTMENT, CUT OUT UPPER DOOR, BETWEEN STA 1263 AND STA 1285, BEHIND OF CARGO DOOR CONTROL PANEL, FRAME WITH CORROSION, L=1", W =0.560".(<P>AFT CARGO COMPARTMENT, CUT OUT UPPER DOOR, BETWEEN STA 1263 AND STA 1285, BEHIND OF CARGO DOOR CONTROL PANELSDR FDEA202503140556Frame · misrepairedEXISTING REPAIR ON FUSELAGE FRAME AT FR20A S37R - S42R REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON FUSELAGE FRAME AT FR20A S37R - S42R WAS EVALUATED AND FOUND NOT IN CONFORMITY WITH DRAWING SR30-53-001 REV.D AND SRM 53-13-13-201 FIG 201. TSDR DALA2025031802038Frame · brokenFOUND FRAME ASSEMBLY, WTBF PN: C02383117-001 BROKEN. REMOVED AND REPLACE FRAME ASSEMBLY, WTBF PN: C02383117-001 IAW CARD 5352-01038-08A AND DWG C02383100 REV. B. (LP# 0856973)SDR SWAA2025042204975Stub Frame · canningCRACK INDICATION ON STUB FRAME LOCATED ON BS 296.5 BTW S-8R TO S-9R AT FWD GALLEY DOOR AREA CRACK LENGTH 1.125 IN. APROX.AT PASSENGER CABIN 2025-202719<REPLACED STUB FRAME LOCATED ON BS 296.5 BTW STR 7R TO STR 9R IAW B737-700 SRM 51-40-02 AND DWG 141A8370 SHEESDR SWAA2025042114931Stub Frame · crackedCRACK INDICATION ON STUB FRAME LOCATED ON BS 296.5 BTW S-8R TO S-9R AT FWD GALLEY DOOR AREA CRACK LENGTH 1.125 IN. APROX.AT PASSENGER CABIN. ] REPLACED STUB FRAME LOCATED ON BS 296.5 BTW STR 7R TO STR 9R IAW B737-700 SRM 51-40-02 AND DWG 141A8370 SHEET 10 REVSDR SWAA2025040705002Stub Frame · crackedCRACK INDICATION ON STUB FRAME LOCATED ON BS 296.5 BTW S-8R TO S-9R AT FWD GALLEY DOOR AREA CRACK LENGTH 0.375 IN. APROX.AT PASSENGER CABIN 2025-203649<[01] REPLACED STUB FRAME AND FASTENERS LOC. BETWEEN STR7R TO STR11R AT FWD GALLEY AREA IAW B737-700 SRM 51-1SDR SWAA2025040715564Stub Frame · crackedCRACK INDICATION ON STUB FRAME LOCATED ON BS 296.5 BTW S-8R TO S-9R AT FWD GALLEY DOOR AREA CRACK LENGTH 0.375 IN. APROX.AT PASSENGER CABIN 2025-203649<[01] REPLACED STUB FRAME AND FASTENERS LOC. BETWEEN STR7R TO STR11R AT FWD GALLEY AREA IAW B737-700 SRM 51-1SDR IPXA2025032604008Frame · brokenFAULT , 53-13,STR= UPPER MAIN CARGO BENEATH SIDE OF FLOOR PANEL # 261BH FRAME FOUND BROKEN . 89-63.ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH UPS EO-93155-REQ1 AND VT-MAE EA 300-5318-27-A3861.SDR DALA2025031201904Frame · crackedCRACK AT FRAME 1037 CROSSING WITH L17L INTERNAL STRUCTURE FUSELAGE. SUMMARY OF NRC 00638: FRAME 1037 CROSSING WITH L17L INTERNAL STRUCTURE FUSELAGE WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 4. (LP #0853086)SDR DALA2025031101889Frame · crackedCRACK AT FRAME STA 1037 AND L17R INTERNAL STRUCTURE OF FUSELAGE. SUMMARY OF NRC 00644: FRAME STA 1037 AND L17R INTERNAL STRUCTURE OF FUSELAGE WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 4. (LP #0851423)SDR FDEA202503110358Frame · dentedCABIN - MAIN DECK CARGO COMPARTMENT LEFT HAND FRAME AT STATION 1661 FOUND DENTED CABIN- MAIN DECK CARGO COMPARTMENT DENT AT LEFT HAND FRAME STATION 1661 LONGERON 12LEFT REPAIRED AS PER MD-11 SRM 53-00-07-2R REPAIR 2 FIGURE 201. INITIAL INSPECTION AT 14,500SDR IXXA20250425001Frame · gougedMAIN CARGO DOOR CUTOUT AFT FRAME IS GOUGED BETWEEN STR 20L AND 21L. HAECO W.O. 320011 AND NR 35218SDR VNAA202504140019Frame · damagedELONGATED HOLE ON FRAME BTW STA FS 661.00 + 62.00 STRG 23LH TO STRG 24LH AT FWD CARGO COMPARTMENT. ELONGATED HOLE ON FRAME BTW STA FS 661.00 + 62.00 STRG 23LH TO STRG 24LH AT FWD CARGO COMPARTMENT WAS REPAIRED PER EA NO: 53-2025-0353 REV.--SDR VNAA202504140018Frame · wornWEAR ON FRAME BTW FS785.15 AT RH AFT EMERGENCY DOOR. WEAR ON FRAME BTW FS785.15 AT RH AFT EMERGENCY DOOR WAS BLENDED PER CRJ 900 SRM 51-12-00-001-001-A01 AND EVALUATED WITHIN LIMITS PER REO 690-53-41-524 REV. - -.SDR SWAA2025040803874Stub Frame · crackedCRACK ON FSD STUB FRAME AT BS 291.5 + 9; .6' ABOVE SEAL DEPRESSOR; 1.2' IN LENGTH (MARKED)<[01] REMOVED AND REPLACED UPPER FWD CORNER FSD STB FRAME PER SRM 51-40-02 AND DWG 141A8370 REV D;[02] COMPLETED ALL STEPS;[03] VERIFIED ACTION 1.<BR>JOB COMPLETE.SDR YENA2025031200254Frame · crackedDURING HEAVY MAINTENANCE: REF AEROMAN WO# 2025 17/1 NR# 2025-120245. CRACK INDICATION ON OPEN HOLE 6 FR20LH JOGGLE AREA. CRACK DEPTH 0.100 INCH, CRACK DIRECTION 3 OCLOCK, (RESOLVED ON W/O: 1353259 TASKCARD: NR-00013) FUR-A320-53-02078. REF AEROMAN WO# 2025 17/SDR YENA2025031200252Frame · crackedDURING HEAVY MAINTENANCE: REF AEROMAN WO# 2025 17/1 NR# 2025-120246. CRACK INDICATION ON FRAME (1 EA) (CRACK INDICATION ON OPEN HOLE 8 FR20LH JOGGLE AREA. CRACK DEPTH 0.100 INCH, CRACK DIRECTION 9 OCLOCK ), (RESOLVED ON W/O: 1353259 TASKCARD: NR-00015) FUR-A32SDR CALA2025031302756Frame · crackedCABIN FRAM CRACKED AT FASTENER. BS 727D BETWEEN STR 8R-9R AT AIR CONDITIONING RAIL (REF. AAR NR 1000033122). ESFR COMPLETED CRACK FOUND IN FRAME DURING AGING AIRCRAFT INSPECTION. ESFR COMPLETED.SDR DALA2025031201940Frame · dented(LOG 0848120) DENT FRAME BS 420 BTW STR 25L TO STR 26L AT FWD CARGO COMPARTMENT. PERFORMED PERMANENT REPAIR ON FRAME BS 420 BETWEEN STR 25 L TO 26 L AS PER B737-800 SRM 53-30-07-2R.SDR VNAA202504140014Frame · corrodedCORROSION ON FRAME 1088.20 BTW STGR 25LH/STGR 27 AT AFT BAGGAGE BAY COMPARTMENT. CORROSION ON FRAME 1088.20 BTW STGR 25LH/STGR 27 AT AFT BAGGAGE BAY COMPARTMENT WAS REMOVED PER CRJ 900 SRM 51-21-06-001-001-A01 AND EVALUATED WITHIN LIMITS PER CRJ-900 SRM 52-3SDR DALA2025031101886Frame · damagedSTA 1225 CANTED FRAME: TAILCONE ALIGNMENT PIN AND CANTED FRAME DAMAGED AT APPROX 7 O'CLOCK POSITION -MARKED-. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY SEE NRC 001-0586:5300-2004/00SDR DALA2025031101866Frame · damaged(LOG 0845549) 5311-01251-02A AND 5311-01251-02B LEFT HAND AND RIGHT HAND STA 727 FRAME INNER CHORD,737 REPAIR. PER TASK CARDS 5311-01251-02A AND 5311-01251-02B STEP 13 A STANDALONE SDR LOG PAGE IS REQ,MAINTENANCE HAS COMPLIED WITH ALL OF THE STEPS 1-13 WITH NOSDR DALA2025031001819Frame · crackedCRACK ON FRAME STA Y=1037 LONG 17 LH. SUMMARY OF NRC 00189: FRAME STA Y=1037 LONG 17 LH WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 4 REPAIR 4. (LP #0845545)SDR VNAA202503070028Frame · corrodedCORROSION BTW FRAME FS1000.00 AND 1015.00 STGR 24RH AT AFT BAGGAGE BAY COMPARTMENT. CORROSION BTW FRAME FS1000.00 AND 1015.00 STGR 24RH AT AFT BAGGAGE BAY COMPARTMENT WAS REPAIRED PER REO 690-53-61-1508 REV. - .SDR VNAA202503070027Frame · corrodedCORROSION ON FRAME FS1051.30 BTWN STGR 26LH AND STGR 26RH AT AFT BAGGAGE BAY COMPARTMENT. REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 AND EVALUATED WITHIN LIMITS PER CRJ-900 SRM 53-00-00-101-001-A01.SDR IXXA202503070001Frame · corrodedLEFT FUSELAGE STATION 1197 +88 APPROX S-12L FOUND CORROSION SPOT ON FRAMESDR SWAA2025042902828Stub Frame · crackedMAIN CABIN R1 DOOR CUTOUT FWD UPPER CORNER CRACK INDICATION AT STUB FRAME 1.25'<[01] REMOVED AND REPLACED R1 DOOR STUBFRAME PN:141A8371U7. IAW BOEING DWG 141A8370 REV.D AND B737-700 SRM 51-40-02;[02] REMOVED AND REPLACED R1 DOOR STUBFRAME PN:141A8371U7. IAW BOSDR SWAA2025032815213Pressure Deck · crackedCRACK INDICATION ON HORIZONTAL PRESSURE DECK WEB RBL 40 STA 663 AT PASSENGER CABIN (1E/A). CRACK LENGTH APPROX. 0.500 INCH APPROXIMATELY.) 2025-185996 <[01] STEPS 6 AND 7 TOOL USED EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 240497907; CAL DUE DATE: 27-AUG-2SDR SWAA2025032815212Pressure Deck · crackedCRACK INDICATION ON HORIZONTAL PRESSURE DECK WEB BTW LBL 30 TO LBL 40 STA 675 AT PASSENGER CABIN (1E/A). CRACK LENGTH APPROX. 0.375 INCH APPROXIMATELY. 2025-185995 <[01] ON STEP 4; TOOL USED: EDDY CURRENT EQUIPMENT; PN: NORTEC 600D; SN: 90023010; DUE DATE: 05SDR IPXA2025032295372Frame · crackedAFT AVI COMP R/H SIDE FRAME STA 475 AT LIGHTING HOLE HAS A CRACKED. INSTALLED THE REPLACEMENT FRAME SPLICE, -3 REPAIR ANGLE, -5 REPAIR STRAP AND ROUND DOUBLER IN CANTED FRAME STA 469.173 RH SIDE AT FWD AVIONICS COMPARTMENT. REF. EA# 011-5310-01-B0421 REV P1 SDR CALA2025031302753Frame · corrodedAFT CARGO FR 58 LST 43 HAS CORROSION PER HAECO LCQ N/R 9290766/ 38766.SDR AALA202507254188Frame · crackedAIRCRAFT IN BASE MAINTENANCE: DURING CURRENT S3 CHECK IN PIT, A CRACK WAS FOUND ON THE AFT FACE OF FRAME 68 RH WHILE ACCOMPLISHING MANDATORY INSPECTIONS. CRACK DEPTH = 0.077 INCH. MAINTENANCE PERFORMED TIME LIMITED REPAIR ON FRAME 68 AFT FUSELAGE RH SIDE, IAW SDR N6WA2025030703Frame · corrodedCORROSION ON FRAME AT FS333.00 BETWEEN STGR18L AND STGR21L. REMOVED AND REINSTALLED NEW FRAME AT FS333.00 BETWEEN STGR18L AND STGR21L IAW CRJ SRM 51-42-06.SDR N6WA2025030702Frame · corrodedFRAME AT FS333.00 BETWEEN STGR21L AND STGR19R HAS CORROSION. REPAIRED FRAME AT FS333.00 BETWEEN STGR21L AND STGR19R IAW EO C550-53MR-049.SDR AALA202506192316Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON FRAME 35 FORWARD FACE TO PRESSURE BULKHEAD A TTACHMENT, (LOCATED BETWEEN STR30L AND STR31L ON FWD CARGO COMPARTMENT. CRACK LENGTH = 0.200 INCHES. MAINTENANCE TIME LIMITED REPAIR INSTRUCTION (INSTALLED REISDR AALA202506138060Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON FRAME 35 FORWARD FACE TO PRESSURE BULKHEAD ATTACHMENT, LOCATED BETWEEN STR30R AND STR31R ON FWD CARGO COMPARTMENTCRACK INDICATION HOLE W1 LOCATED INTERNAL SURFACE ON FR35 AT LEVEL STR30 RH CRACK LENGTH=0.SDR SWIA20250428304Frame · corrodedFRAME SEGMENT ON FS 501.00 CORRODED ON LOWER FLANGE BETWEEN STGR 24LH - 23LH #29735012 (C-CHECK RO 04/26/2025)REMOVED AND INSTALLED NEW FRAME SEGMENT ON FS 501.00 BETWEEN STGR 20LH TO STGR25LH REF. CRJ900 SRM 51-42-06-001-001-A01 REV 38 JUL 25/2020 ND BOMBARSDR IPXA2025032961156Frame · crackedAFT CGO COMP WASTE TANK BILGE AREA STA 1986-2007 LONGERON 45L HAS CRACKED. 74-058 ATA CODE 53. INSTALLED 1EA LONGERON REPLACEMENT 45LH, 1 EA LONGERON SPLICE, 4 EA BRACKET, 3 EA FRAME SPLICE, 2EA FRAME ,1EA FRAME SUPPORT 1EA STANCHION, 1EA FRAME SPLICE, 3EA ISDR IPXA2025032656520Frame · crackedFAULT: CRACK FOUND IN TOP HOLE ON FR40 LH UPPER TENSION FASTENER. REPAIR PER A300-600F SRM REV 41 CHAP 57-10-24-201 PARA 5.A, FIG 206 SHEET 1 (REPAIR WITHOUT BUSH).UPS CONSIDERS THIS A MINOR REPAIR PER GMM 05.04.CAUTION:THE WORK INSTRUCTIONS CONTAINED WITHIN (SDR IPXA2025032656542Frame · crackedFAULT: CRACK FOUND IN MIDDLE HOLE ON FR40 LH UPPER TENSION FASTENER. REPAIR PER A300-600F SRM REV 41 CHAP 57-10-24-201 PARA 5.A, FIG 202 & FIG 206 SHEET 2 (REPAIR WITH BUSH).UPS CONSIDERS THIS A MINOR REPAIR PER GMM 05.04.CAUTION: THE WORK INSTRUCTIONS CONTAINSDR IPXA2025032660851Frame · crackedFAULT: CRACK FOUND IN HOLE A ON LH FR47 HORIZONTAL JUNCTION. AREA MARKED IN BLACK VERIFIED STEP 12 REAM FASTENER HOLE CONCENTRICALLY IN ALL LAYERS FROM TO 0.6235" TO 0.6250" TO THE FINAL SIZE: 0.6250" IAW SRM 51-40-44 AND E.A.#: 300-5710-27-A3836 STEP #9 PRELISDR DALA2025030501709Frame · corrodedCORROSION ON FRAME BTW STA Y=1022 L28L TO L28R AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00177: CORROSION LEVEL 2. FRAME BTW STA Y=1022 L28L TO L28R AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 3, REPAIR 3. PERFORM A DETAIL VISUASDR N6WA2025030401Frame · corrodedCORROSION ON FRAME AT FS364 BETWEEN STRINGER 24L AND 24R. PERFORMED REPAIR ON FRAME AT FS364 BETWEEN STRINGER 24L AND 24R IAW GOJET EO C550/700-53MR-006.SDR DALA2025030401690Frame · dentedSHIP 6702 FUSELAGE FRAME IS DENTED STA 1480 AT LBL STRINGER 26L. CORRECTIVE ACTION: REPAIRED FRAME AT STA 1480 S-25LBTW S-27L IAW B757-200 SRM 53-00 -07-2R REPAIR S FIG 201 SHEET 5 AND SRM 51-40-02-0G PAR 7 774SB. (0838488)SDR LR7A2025030303724Frame · crackedDURING SCHEDULED C-14 CHECK UNDER JOB CARD HC3215, FOUND NLG WHEEL WELL FS140 FRAME REPAIR DOUBLER CRACKED AT LBL46, WL154. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-19. NR# 0310.SDR LR7A2025030303713Frame · crackedDURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5315, FOUND AFT CARGO COMPARTMENT FS803 OVERHEAD RING SEGMENT CRACKED AT LBL2-RBL14, WL285. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 53-50-07. NR# 0130.SDR EE4Y2025030321872Frame · crackedDURING ACCOMPLISHMENT OF ALLEGIANT TASK A32X-53-260-002, UPPER FUSELAGE AFT RH DOOR CUTOUT FR 66 DOOR STOP FITTING # 4 I/B UPPER FASTENER HOLE WITH CRACK INDICATION WAS FOUND. THE FRAME HOLE WAS REPAIRED FOLLOW REPAIR INSTRUCTIONS AS PER A319 SRM 53-41-12-300-SDR EE4Y2025030321871Frame · crackedDURING ACCOMPLISHMENT OF THE ALLEGIANT TASK A32X-53-260-003 UPPER FUSELAGE AFT RH DOOR CUTOUT FR68 DOOR STOP FITTING # 1 I/B LOWER FASTENER HOLE WITH CRACK INDICATION WAS FOUND.THE FRAME HOLE WAS REPAIRED IAW A319 SRM TASK 53-41-12-300-011 FIG 008 PARAG 2A. THSDR SWAA2025040701386Frame · crackedCRACK ON FRAME LOCATED BS 312 BTW STR 5L TO STR 6L AT FWD GALLEY AREA 2025-171916<[01] PERFORMED PERMANENT REPAIR ON FRAME LOCATED BS 312 BTW STR 5L TO STR 6L AT FWD GALLEY AREA IAW B737-800 EA M-22-153-01244. SEE INDIVIDUAL SIGN OFF BELOW.;[02] PERFORMED PERMSDR DALA2025030501736Frame · dented(LOG 0836337) DENT ON FRAME ON BS 767 STR 24L AT AFT CARGO COMPARTMENT. PERFORMED PERMANENT REPAIR ON FRAME LOCATED ON BS 767 BTW STR23L TO STR25L ASPER B737-800 SRM 53-60-07-2R-3 REPAIR 3.
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