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.

SDR REXA2024111101458Frame · corrodedF.S. 295 FRAME IS CORRODED BETWEEN STGR 19L TO STGR 20L. REPLACED FRAME PER SRM.Sep 6, 2024 · N668CA · Cndair CL6002C10SDR REXA2024102200912Frame · corrodedF.S. 364 FRAME IS CORRODED ON THE FWD AND AFT SIDE BETWEEN STGR 19L TO STGR 20L. NEW SEGMENT OF FRAME P/N:SH670-31158-3 WAS INSTALLED IAW CRJ700 SRM TASK 51-42-06-001-001-A01.Sep 6, 2024 · N668CA · Cndair CL6002C10SDR REXA2024101000867Frame · corroded"F.S. 333 IS CORRODED BETWEEN STGR 25L TO STGR 27. REMOVED CORROSION ON FS 333 BETWEEN STGR 25L-27 IAW CRJ 700 SRM 51-21-06-001-001-A01. MINIMUM REMAINING THICKNESS AT ALL BLEND LOCATIONS TO FS333.00 FRAME SEGMENT FROM STR 25L TO STR 26L AND STR 27 TO STR 26R Sep 6, 2024 · N668CA · Cndair CL6002C10SDR REXA2024100700848Frame · corrodedF.S. 310 IS CORRODED BETWEEN STGR 26R TO STGR 26L. REPAIRED IAW CRJ 700 SRM 53-00-06-201-006-A01.Sep 6, 2024 · N668CA · Cndair CL6002C10SDR SWIA2024091900006Frame · crackedFOUND 2 CRACKS AND SKIN OIL CANNING ON CENTER FRAME SECTOR P/N 600-34014-277 LOCATED OFF FS235.00 AND BETWEEN STGR-26L AND STGR-26R AFT OF NLG. THIS HAS BEEN CLASSIFED AS A MAJOT REPAIR. FORM M-337 INITIATED. (FILED CLOSED) PERFORMED SHORING OF THE AIRCRSep 6, 2024 · N466SW · Cndair CL6002B19SDR YENA2024091001239Frame · crackedDURING HEAVY MAINTENANCE: FR 20 DOUBLE JOGGER AREA HOLE "C" WITH CRACK INDICATION ON FRAME; REF MEXICANA WO#1316755 S/N 00329 FOR WORK PERFORMED; FUSELAGE LH FR20 DOUBLE JOGGLE AREA, HOLE "C" CRACK ON FRAME WAS REPAIRED, IAW A320 SRM TASK 53-11-12-300-012 REVSep 6, 2024 · N516JB · Airbus A320232SDR YENA2024091001237Frame · crackedDURING HEAVY MAINTENANCE: RH FR20 DOUBLE JOGGER AREA HOLDS "A" AND "C" WITH CRACK INDICATION ON FRAME; REF MEXICANA WO#1316755 S/N 0330 FOR WORK PERFORMED; RH FR20 DOUBLE GOGGER AREA HOLD "A" CACK ON FR WAS REPAIRED IAW A320 SRM 52-11-12-300-012 MAY 01/24 RESep 6, 2024 · N516JB · Airbus A320232SDR DALA2024091008881Frame · corrodedCORROSION ON FRAME BTW STA Y=1023 LONGERON 29L AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00754: CORROSION LEVEL 2. CORROSION ON FRAME BTW STA Y=1023 LONGERON 29L AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 3. (LP #0542411)Sep 6, 2024 · N989AT · Boeing 717200SDR AALA202411145130Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME FITTING AT FR 57 AND S23R. REPLACED FRAME ASSEMBLY PER EA 358297.Sep 5, 2024 · N750UW · Airbus A319112SDR SWAA2024101634707Stub Frame · crackedCRACK FOUND ON FSD STUB FRAME AT BS291.5 + 8; 0.8' ABOVE SEAL DEPRESSOR 1.2' IN LENGTH (MARKED)<[01] REMOVED FSD STUB FRAME IAW SRM 51-40-02-0G-0 AND INSTALLED NEW FSD STUB FRAME IAW SRM 51-40-02-0G-0 AND DWG 141A8370 REV. D.;[02] CORRECTIVE ACTION COMPLETED.Sep 5, 2024 · N265WN · Boeing 7377H4SDR SWAA2024101634640Stub Frame · crackedCRACK STUB FRAME LOCATED STA294.5 AND STR17R AT PASSENGER CABIN 2024-565307<[01] EQUIPMENT P/N PHASEC 3D; S/N 587435/07; DUE DATE 20-MAR-25 WAS USED ON STEP 7;[02] TOOL USED: EDDY CURRENT EQUIPMENT; P/N: NORTEC600D; S/N: 220272512; CAL DUE DATE: 08-JAN-25;[03]Sep 5, 2024 · N7738A · Boeing 7377BDSDR SWAA2024101634644Stub Frame · crackedCRACK INDICATIONS ON STUB FRAME LOCATED ON BS 294.5 BTW S-8R T O S-9R (2 EA) AT FWD GALLEY DOOR AREA CRACKS LENGTH 0.312 IN.AT PASSENGER CABIN 2024-565314<[01] REPLACED STUB FRAME LOCATED ON BS 294.5 BTW S-7R TO S-9R AT FWD GALLEY SERVICE DOOR AREA IAW B737-70Sep 5, 2024 · N7738A · Boeing 7377BDSDR DALA2024090608783Frame · corrodedSHIP 3148 CORROSION WEB FRAME 16 AT LEVEL STRINGER 23 LEFT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED WEB LOC. FRAME 16 AT LEVEL STRINGER 23 LEFT FWD GALLEY AREA SIDE, AS PER A319 SRM 51-42-11 AND A319 SRM 51-72-11. (0541035)Sep 5, 2024 · N348NB · Airbus A319114SDR REXA2024092600723Frame · corrodedFRAME FS517 CORRODED BETWEEN STRINGERS 18L AND 19L REMOVED STUB FRAME TO BLEND DAMAGE AREA AT FS517 BETWEEN STR18L TO STR19L, IAW CRJ-700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.EVALUATED AND FOUND TO BE OUT OF LIMITS DUE TO THE DAMAGE IS ON TWO ELEMSep 4, 2024 · N668CA · Cndair CL6002C10SDR AALA202412197821Frame · noneAIRCRAFT IN BASE MAINTENANCE: EXISTING REPAIR TO FRAME 16 BETWEEN S6L AND S14L AT DOOR STOP FITTING 7. PARTIAL FRAME REPLACEMENT ACCOMPLISHED PER EA 358113.Sep 3, 2024 · N190UW · Airbus A321211SDR AALA202412186271Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON FR 16 RIGHT HAND SIDE UPPER CORNER DOUBLER AT S5R. REPLACED FRAME DOUBLER PER EA 358139.Sep 3, 2024 · N190UW · Airbus A321211SDR AALA202411192169Frame · crackedAIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK CENTER WINDSHIELD FRAMING RIGHT HAND CENTER POST FRAME CRACKED AT FR 2 AND Y0. REPAIRED FRAME PER EA 357766.Sep 3, 2024 · N750UW · Airbus A319112SDR REXA2024111101455Frame · corrodedFRAME F.S. 1015 STR21L-23R FWD SIDE OF STATION IS CORRODED REPAIRED PER EA CRJ753-17405Sep 3, 2024 · N668CA · Cndair CL6002C10SDR LR7A2024090303503Frame · crackedDURING SCHEDULED C-15 CHECK UNDER JOB CARD HC5313, FOUND FS825 UPPER RING SEGMENT CRACKED AT RBL20, WL285. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 53-50-07. DRC# 0660. / PSE# 53-50-05, AD 2012-06-09Sep 3, 2024 · N402LC · Lkheed 382GSDR LR7A2024090303491Frame · crackedDURING SCHEDULED C-15 CHECK UNDER JOB CARD HC5315, FOUND FS817.0E LH RING SEGMENT CRACKED THROUGH A BOLT HOLE AT LBL65, WL152. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. DRC# 0451.Sep 3, 2024 · N402LC · Lkheed 382GSDR SWAA2024101533296Frame · crackedCRACK ON FRAME LOCATED BS 312 BTW STR 5L TO STR 6L AT FWD GALLEY AREA 2024-558762<[01] REPAIR FRAME LOCATED BS 312 BTW STR 5L TO STR 6L AT FWD GALLEY AREA. IAW EA M-22-153-01244.;[02] REPAIR FRAME LOCATED BS 312 BTW STR 5L TO STR 6L AT FWD GALLEY AREA. IAW EA Sep 2, 2024 · N8325D · Boeing 7378H4SDR DALA2024090308640Frame · corrodedSHIP 3143 CORROSION WEB FRAME 20 AT LEVEL STR 23RH SIDE AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED WEB FRAME 20 TO FRAME 24 AT LEVEL STR 23RH SIDE AT FWD GALLEY AREA AS PER A319 SRM 51-72-11 AND SRM 51-42-11. (0535450)Sep 2, 2024 · N343NB · Airbus A319114SDR EE4Y2024090220806Frame · crackedDURING INSPECTION AS PER ALLEGIANT WORK CARD 53-260-003 IN THE FR68LHS DOOR STOP FITTING 1 LOWER INBOARD HOLE CRACK WAS FOUND. THIS DAMAGE WAS REPAIRED IN ACCORDANCE A320 SRM 53-41-12-300-011 AND 53-41-12-300-011 PARAG 2A FIG 008. THIS REPAIR IS MAJOR CAT B. TSep 2, 2024 · N273NV · Airbus A320214SDR AALA202409096093Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN STUB FRAME LOCATED ABOVE CENTER WING BOX AT STA 616, RBL 70.85. REPLACED STUB FRAME PER EA 357237.Sep 1, 2024 · N906AN · Boeing 737823SDR YENA2024090301217Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON OPEN FASTENER HOLE B FRAME 16 R/H SIDE AND CONFIRM INDICATION USING BOROSCOPE VIEW AS PER REF NTM 51-90-00; REF AEROMAN N/R 2024-458273, PERFORMED REPAIR HOLE B ON FRAME LAYER LOC ON DOUBLE JUGGLE AREA FRAME Sep 1, 2024 · N589JB · Airbus A320232SDR JR2R20240831305Frame · gougedRH HORIZONTAL STAB FITTING FR100 HAS EVIDENCE OF TOOLING MARKSAug 31, 2024 · N87318 · Emb ERJ170200LRSDR JR2R20240831312Frame · chafedFR100 UPPER SECTION HAS CHAFE MARKS WHERE LATERAL FITTINGS ATTACHAug 31, 2024 · N87318 · Emb ERJ170200LRSDR JR2R20240831311Frame · chafedFR100 LOWER SECTION HAS CHAFE MARKS ON BOTH LH AND RH SIDES WHERE LATERAL FITTINGS ATTACHAug 31, 2024 · N87318 · Emb ERJ170200LRSDR SWAA2024100932520Frame · crackedCRACK FRAME ON BS 312 BTW STR 5L TO STR 6L AT FWD GALLEY AREA 2024-528711<[01] PERFORMED TRIM OUT ON FRAME LOCATED AT BS 312 BTW STR 5L TO STR 6L AT FWD GALLEY AREA IAW EA M-22-153-01244 SEE INDIVIDUAL SIGNOFFS BELOW;[02] PERFORMED TRIM OUT ON FRAME LOCATED ATAug 30, 2024 · N256WN · Boeing 7377H4SDR ABXA20240830164Frame · corroded"WHILE 762CK WAS UNDERGOING C-CHECK IN OSC, MAINTENANCE FOUND CORROSION ON THE FRAME WEB AT STA 1307, BETWEEN S-371 & S-381 ATLBL 11. CORROSION REMOVAL EXCEEDED THE LIMITS GIVEN IN SRM 53-00-07, AD 1, FIGURE IO I. THE PURPOSE OF THIS REA IS TO AUTHORIZE AND DOAug 30, 2024 · N762CK · Boeing 7673P6SDR SWI2024F01170Frame Splice · corrodedFRAME SPLICE STRAP IS CORRODED AT FS319 APPROX. WL72 (RH SIDE) (C-CHECK RO 11-6/2024) REMOVED AND REPLACED NEW FRAME SPLICE BRACKET LOCATED AT FS319.00 APPROX. WL72, R/H SIDE, FLOOR LEVEL REF CRJ 700 SRM 51-42-21-001-001-A01 AND SRM 51-42-13-001-001Aug 29, 2024 · N755EV · Cndair CL6002C10SDR 2A6R2024082971103Frame · corrodedCORROSION DAMAGE WAS DISCOVERED ON FRAME 3 (PN: L533M1028221) AND ON THE FRAME 3 UPPER T CAP (PN: L533M1028203) AT APPROXIMATELY FUSELAGE STATION 3,150MM. REPLACEMENT PARTS WERE NOT AVAILABLE; THEREFORE, A REPLACEMENT FRAME AND T CAP WERE FABRICATED OUT OF 0Aug 29, 2024 · N534LN · Urocop EC135P2SDR 2A6R2024082971102Frame · corrodedCORROSION DAMAGE WAS DISCOVERED ON THE LOWER ANGLE (PN: L533M1043427) AT APPROXIMATELY FUSELAGE STATION 2,675MM. REPLACEMENT PARTS WERE NOT AVAILABLE; THEREFORE, A REPLACEMENT ANGLE WAS FABRICATED OUT OF 0.050” 2024-T3 PER AIR METHODS ENGINEERING AUTHORIZATIOAug 29, 2024 · N534LN · Urocop EC135P2SDR 2A6R2024082971101Frame · corrodedCORROSION DAMAGE WAS DISCOVERED ON THE LOWER FLANGE OF FRAME 1 (PN: L533M1011103) ON THE LH AND RH SIDES. A DETAILED DESCRIPTION OF THE DAMAGE AND AN APPROVED REPAIR PROCEDURE IS PROVIDED IN AIRBUS REPAIR DESIGN APPROVAL SHEET RDAS-EC135-53-2024-1387, ISSUE AAug 29, 2024 · N2A6R · Urocop EC135P2SDR 2A6R2024082871701Frame · crackedDURING A 1000 HOUR INSPECTION, FOUND A 0.25MM CRACK ON THE TAIL CONE UPPER FRAME 7Aug 28, 2024 · N935AC · Urocop EC135P2SDR U2RA2024100200060Frame · crackedCRACK FOUND AT STA 1480 RH BULKHEAD FRAME WL 150 INBRD OF RBL 118Aug 27, 2024 · N702CA · Boeing 747412SDR SWAA2024100731279Frame · crackedCRACK FRAME ON BS 947.5 BETWEEN STRINGER 25L TO STRINGER 26L AFT CARGO COMPARTMENT 2024-533479<[01] REPLACED FRAME LOCATED ON BS 947.5 BETWEEN STRINGER 25L TO STRINGER 26L AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 Ï¿½TEM 9; SRM 51-40-02 AND DRAWING # 147Aug 27, 2024 · N266WN · Boeing 7377H4SDR SWI202409230863Frame Splice · corrodedL/H SPLICE @ FR 90 HAS CORROSION (C-CHECK RO 9/20/2024) REMOVED AND REPLACED L/H SPLICE @ FR 90. REF SRM 51-40-08. SEE CONTINUATION CARD FOR WORK PERFORMED.Aug 27, 2024 · N110SY · Emb ERJ170200LRSDR SWI202409230862Frame Splice · corrodedCENTER SPLICE @ FR 90 HAS CORROSION (C-CHECK RO 9/20/2024) REMOVED AND REPLACED CENTER SPLICE AT FR 90 IAW REF EMB SRM 51-40-08. SEE CONTINUATION CARD FOR MAINTENANCE PERFORMED.Aug 27, 2024 · N110SY · Emb ERJ170200LRSDR SWI202409230861Frame Splice · corrodedR/H MID SPLICE @ FR 89 HAS CORROSION (C-CHECK RO 9/20/2024) REMOVED AND REPLACED R/H MID SLPICE AT FR 89, REF SRM 51-40-08. SEE CONTINUATION CARD FOR MAINTENANCE PERFORMED.Aug 27, 2024 · N110SY · Emb ERJ170200LRSDR SWI202409230860Frame Splice · corrodedR/H SPLICE @ FR 89 HAS CORROSION (C-CHECK RO 9/20/2024) REMOVED AND REPLACED R/H SPLICE AT FR 89, REF SRM 51-40-08. SEE CONTINUATION CARD FOR MAINTENANCE PERFORMED.Aug 27, 2024 · N110SY · Emb ERJ170200LRSDR DALA2024082808513Frame · crackedSHIP 3164 CRACK INDICATIONS WERE FOUND ON FR16RH, FASTENER HOLES #6 AND #7. CORRECTIVE ACTION: REAPIRED PER ERA 593392-14AD. (0524989)Aug 27, 2024 · N364NB · Airbus A319114SDR SWIA202411150826Frame · chafedFOUND CHAFE DAMAGE ON FS 718.00 BETWEEN STGR 16R AND STGR 17R (FILED CLOSED) COMPLIED WITH REO 601R-53-61-8219 DATED: 2024-09-11 REV -- REPAIR TO FRAME FS718.00 BETWEEN STR16R - STR17R. ALL NDTS COMPLIED WITH AND NO DEFECTS NOTED AT THIS TIME. COMPLIED WAug 26, 2024 · N958SW · Cndair CL6002B19SDR SWAA2024100830586Stub Frame · crackedCRACK INDICATION ON STUB FRAME LOCATED ON BS 294.5 LOCATED BTW S-8R TO S-9R AT FWD GALLEY DOOR AREA CRACK LENGTH 3.625 IN.AT PASSENGER CABIN 2024-533435<[01] REPLACED STUB FRAME LOCATED ON BS 294.5 BETWEEN STR-7R AND STR-10R FWD SERVICE DOOR AT FWD GALLEY AREAAug 26, 2024 · N266WN · Boeing 7377H4SDR SWIA202409300001Frame · corrodedEVIDENCE OF CORROSION LOCATED ON FR.87 BETWEEN STR.27R AND 28R AS MARKED. (C-CHECK RO 9/26/2024) REMOVED AND REPLACED FR. 87 BETWEEN STR. 26R - 26L REF: SRM 51-40-08. FRAME WAS REPLACED WITH OEM PART NO CHANGE TO WEIGHT AND BALANCE NOTEDAug 26, 2024 · N613CZ · Emb ERJ170200LRSDR SWIA2024092000826Frame · chafedFOUND CHAFE DAMAGE ON FS 718.00 BETWEEN STGR 16R AND STGR 17R (FILED OPEN) COMPLIED WITH REO 601R-53-61-8219 DATED: 2024-09-11 REV -- REPAIR TO FRAME FS718.00 BETWEEN STR16R - STR17R. ALL NDTS COMPLIED WITH AND NO DEFECTS NOTED AT THIS TIME. COMPLIED WITAug 26, 2024 · N958SW · Cndair CL6002B19SDR SWAA2024091930070Stub Frame · crackedDURING HFEC OPEN HOLES INSPECTION; CRACK NOTED AT HOLE COMMON TO VERTICAL FLANGE OF MOPSILL AND STUB FRAME AT BS294.5; RBL 54; WL208.5<[01] VERIFIED STEPS 1;2 COMPLETE.;[02] VERIFIED STEPS 4;5 COMPLETE.;[03] ACCOMPLISHED REPAIR ON VERTICAL FLANGE OF MOPSILL ANAug 25, 2024 · N267WN · Boeing 7377H4SDR R61A2024091900414Frame · corrodedFWD WET AREA R/H FR17 HAS CORROSION PERFORMED ''L'' ANGLE REPAIR DOUBLER ON FWD WET AREA RH CROSSBEAM FR 17 PER SRM 53-- 00-10-/R03. RESTORED SURFACE PROTECTION AND CIC TO REWORKED AREA REFER SRM 51-23-05, 51-23-06 AND CPM 51-25-00. SEE WIPS AND TASK FOR WORK Aug 25, 2024 · N126HQ · Emb ERJ170200LRSDR R61A2024091900413Frame · corrodedFWD WET AREA R/H FR 14 HAS CORROSION PERFORMED ''L'' ANGLE REPAIR DOUBLER FOR FWD WET AREA RH CROSSBEAM FRAME 14 PER SRM 53-00-10/REPAIR 03. RESTORED SURFACE PROTECTION ON NEW DOUBLER REPAIR REF EMB SRM 51-23-06 AND CPM 51-25-00.Aug 25, 2024 · N126HQ · Emb ERJ170200LRSDR IXXA20241002007Frame Splice · crackedCRACK INDICATION FOUND 1 EA HOLE, AT R1 DOOR CUT OUT LOWER AFT CORNER, MARKED 4 O'CLOCK POSITION EXTERNALLY .500" DEEP TO .540" FROM SKIN SURFACE. HAECO WO 320008 NON ROUTINE 40323Aug 24, 2024 · N491AZ · Boeing 767323
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