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 SWIA2024102812Frame · corrodedFWD FRAME AT FS349 STGR22R HAS CORROSION (C-CHECK RO 10/26/2024) (FILED OPEN)REMOVED CORROSION FROM FWD FRAME AT FS 349 STGR 22R,ORIGINAL MATERIAL THICKNESS IS 0.100" REF DRW. 601R320402 REV NC. REMAINING MATERIAL THICKNESS PER NDT IS 0.035". MATERIAL LOSS IS Aug 12, 2024 · N906EV · Cndair CL6002B19SDR SWAA2024092324545Stub Frame · crackedCRACK INDICATION FOUND OF THE STUB FRAME LOCATED BS 290-296 BETWEEN STR8 AND STR9 AT FWD GALLEY DOOR R1 BEAR STRAP. CRACK LENGTH= 0.912 INCHES. 2024-504165<[01] REPLACED STUB FRAME LOCATED BS 290-296 BETWEEN STR8 AND STR9 AT FWD GALLEY DOOR IAW B737-700 SRM 51Aug 12, 2024 · N7880D · Boeing 7377K5SDR YENA2024081301125Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FASTENER HOLE 8, LOCATED AT FR 16 LH ON DOUB LE JOGGLE AREA, PASSENGER CABIN. CRACK DEPTH = 0.098 INCHES. CRACK DIR ECTION: 9 OCLOCK. CONFIRM INDICATION USING BOROSCOPE VIEW IAW NTM 51-9 0-00; (RESOLVED ON W/Aug 12, 2024 · N580JB · Airbus A320232SDR YENA2024081301124Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FASTENER HOLE A, LOCATED AT FR 16 LH ON DOUB LE JOGGLE AREA, PASSENGER CABIN. CRACK DEPTH = 0.096 INCHES. CRACK DIR ECTION: 9 OCLOCK. CONFIRM INDICATION USING BOROSCOPE VIEW IAW NTM 51-9 0-00; (RESOLVED ON W/Aug 12, 2024 · N580JB · Airbus A320232SDR YENA2024081301123Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FASTENER HOLE B, LOCATED AT FR 16 LH ON DOUB LE JOGGLE AREA, PASSENGER CABIN. CRACK DEPTH = 0.094 INCHES. CRACK DIR ECTION: 9 OCLOCK. CONFIRM INDICATION USING BOROSCOPE VIEW IAW NTM 51-9 0-00; (RESOLVED ON W/Aug 12, 2024 · N580JB · Airbus A320232SDR YENA2024081301122Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FASTENER HOLE C, LOCATED AT FR 16 LH ON DOUB LE JOGGLE AREA, PASSENGER CABIN. CRACK DEPTH = 0.075 INCHES. CRACK DIR ECTION: 1 OCLOCK. CONFIRM INDICATION USING BOROSCOPE VIEW IAW NTM 51-9 0-00; (RESOLVED ON W/Aug 12, 2024 · N580JB · Airbus A320232SDR DALA2024081308077Frame · crackedSHIP 3149 CRACK INDICATION FOUND IN OPEN FASTENER HOLE 7 LOCATED ON FRAME 16L JO GGLE AREA. CORRECTIVE ACTION: CRACK INDICATIONS WERE FOUND AFFECTING FR16LH DOUBLE JOGGLE HOLES #7, #A & #19. (0497473)Aug 12, 2024 · N349NB · Airbus A319114SDR SWIA2024082600010Frame · corrodedFRAME FS574.00 AT CARGO DOOR FWD OPENING HAS CORROSION AT APPROX. WL75.00. (FILED - CLOSED)BLENDED CORROSION ON FRAME FS574.00 AT CARGO DOOR FWD OPENING AT APPROX WL75.00 WITH REFERENCE TO SRM 51-21-06 AND COMPLIED WITH REO 601R-53-61-8212 REV "--" DATED 2024-Aug 10, 2024 · N910EV · Cndair CL6002B19SDR DALA2024081408152Frame · damagedAIRCRAFT 3725, AFT CARGO BAY FRAME DAMAGED AT STA 727E STR 23R WL 165. CORRECTIVE ACTION: REPAIRED DAMAGE AFT CARGO BAY FRAME AT STA 727E STR 23R WL 165 IAW SRM 53-60-07-2R PROCEDURE 3 REPAIR 3 ALTERNATIVE 1 FIGURE 204 DETAIL 1. (LP 0500499)Aug 10, 2024 · N395DN · Boeing 737832SDR DALA2024081208002Frame · crackedSHIP 3149 FUSELAGE FRAME/FORMERS FR16RH AT DOOR STOP #1 & #7 LEVEL DOUBLE JOGGLE CRACK INDICATIONS WERE FOUND AFFECTING HOLE #5. CORRECTIVE ACTION: REPAIRED PER ERA 619634-14AD. (0494945)Aug 10, 2024 · N349NB · Airbus A319114SDR DALA2024081208001Frame · crackedSHIP 3149 FR16LH DOUBLE JOGGLE, CRACK INDICATIONS WERE FOUND AFFECTING HOLES #7, #A & #19. CORRECTIVE ACTION: REPAIRED PER 619627-14AD. (0495207)Aug 10, 2024 · N349NB · Airbus A319114SDR DALA2024081208000Frame · crackedSHIP 3149 CRACK INDICATION FOUND IN OPEN FASTENER HOLE 5 LOCATED ON FRAME 16R JOGGLE AREA. CORRECTIVE ACTION: REPAIRED PER ER/A 619634-14AD. (0495296)Aug 10, 2024 · N349NB · Airbus A319114SDR SWAA2024092324511Stub Frame · crackedCRACK ON STUB FRAME LOCATED BS 294.5 AT LEVEL STR 17R AT FWD GALLEY AREA 2024-504086<[01] REPLACED STUB FRAME LOCATED BS 294.5 AT LEVEL STR 17R AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9 SRM 51-40-02; DWG 141A8370 SHEET 10 REV.D; DWG 141A8370 SHEET 11Aug 9, 2024 · N7880D · Boeing 7377K5SDR SWAA2024092324504Frame · crackedCRACK ON FRAME LOCATED BS 312 BTW STR 5L TO STR 6L AT FWD GALLEY AREA 2024-504066<[01] PERFORMED REPAIR ON FRAME LOCATED AT BS 312 BTW STR 5L TO STR 6L AT FWD GALLEY AREA IAW EA M-22-153-01244. SEE INDIVIDUAL SIGN OFF BELOW;[02] TASK COMPLETED <BR>SEE INDIVIDUAug 9, 2024 · N7880D · Boeing 7377K5SDR AALA202409120699Frame · not reportedAIRCRAFT IN BASE MAINTENANCE: REPLACEMENT OF LEFT HAND FRAME (PICKLE FORK) AT STA 663.75 FROM S10R TO S18R REQUIRED PER EA 3567331A DUE TO REPLACEMENT OF RIGHT HAND FRAME (PICKLE FORK. SEE AALA202409122538 ). REPLACED FRAME PER EA 3567331A .Aug 9, 2024 · N923AN · Boeing 737823SDR AALA202409122538Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN LEFT HAND FRAME (PICKLE FORK) OUTBOARD CHORD AT STA 663.75, LBL 18. REPLACED FRAME PER EA 356731B.Aug 9, 2024 · N923AN · Boeing 737823SDR IPXA2024090388374Frame · crackedFWD AVIONIC COMP RH AFT CANTED AREA BETWEEN STA 457-475 FUSELAGE FRAME HAS CRACKED. 74-069 ATA CODE 53. REPAIRED IAW MD11 SRM 53-10-07-2R-1, REPAIR 1 FIGURE 201 REV 71.Aug 9, 2024 · N253UP · Doug MD11FSDR FDEA202408091106Frame · bentFOUND FRAME WEB DAMAGED AT FR390 BETWEEN STR35L AND STR 36L . FRAME WEB AT FR390 BETWEEN STR35L AND STR 36L REPLACED.Aug 9, 2024 · N270FE · Boeing 7673S2FSDR FDEA202408091104Frame · bentFRAME AT STA 434 BENT BETWEEN STR 36L AND STR 38L FRAME AT STA 434 BENT BETWEEN STR 36L AND STR 38L REPLACED.Aug 9, 2024 · N270FE · Boeing 7673S2FSDR FDEA202408091103Frame · bentFRAME AT STA 412 BENT BETWEEN STR 36L AND 38L FRAME AT STA 412 BENT BETWEEN STR 36L AND 38L REPLACED.Aug 9, 2024 · N270FE · Boeing 7673S2FSDR REXA2024100300825Frame · corrodedPERM REPAIR PRESSURE BLKHEAD @ FS 693 ST 26L- REPAIRED PRESSURE BLKHEAD @ FS 693 ST 26L- IAW MHIRJ REO 690-53-41-496 REV. -(P1) DATED 2024-08-15 AND CRJ900 SRM 51-42-21-001-001-A01 AND MHIRJ REO 690-53-41258 REV. - DATED 2021-04-16.Aug 8, 2024 · N324PQ · Cndair CL6002D24SDR SWAA2024092324299Frame · crackedCRACKED FRAME BS 312 COMMON TO STRINGER 6L.<[01] ACCOMPLISHED REPAIR OF FRAME AT STA 312; STR 7L PER EA M-22-153-01244; DOCUMENTED ON TASK ID TTG8Q00V943A;[02] EDIT: ACCOMPLISHED REPAIR OF FRAME AT STA 312; STR 6L PER EA M-22-153-01244; DOCUMENTED ON TASK ID TAug 8, 2024 · N267WN · Boeing 7377H4SDR SWAA2024092024058Stub Frame · crackedCRACK ON FSD STUB FRAME. LOCATED AT BS 291.5 + 10; .7' ABOVE SEAL DEPRESSOR; .4' IN LENGTH (MARKED) CORRECTION TO FAULT NAME: CRACK FOUND ON FSD STUB FRAME<[01] INSTALLED FWD SERVICE DOOR UPPER STUB FRAME P/N 141A8371-7 I.A.W. SRM 51-40-02-0G0 DWG # 141A8370 RAug 8, 2024 · N267WN · Boeing 7377H4SDR SWAA2024082624165Frame · crackedDOCUMENTATION FOR MEASUREMENT FIELDS ON FAULT 'FED CUTOUT UPPER STIFFER CRACK IN FRAME IB RADIUS AT BS312; STR5L [TTG8Q00UWBHF]'<[01] REPAIR ACCOMPLISHED AT M-22-153-01244 (737-NG - SWA - BS 312 FRAME UPPER CHORD CRACK DAMAGE AT LBL 33 BETWEEN S-5L AND S-6L);[Aug 8, 2024 · N8503A · Boeing 7378H4SDR DU4R202408080042Frame · crackedDURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FL FOUND CRACK INDICATION IN OPEN HOLE #5 AT 9 O-CLOCK IN FRAME LAYER AT UPPER DOUBLE JOGGLE AREA FR 20 RH SIDE. S/O 193151 NR 28487Aug 8, 2024 · N218NV · Airbus A320214SDR DU4R202408080041Frame · crackedDURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FL FOUND CRACK INDICATION IN OPEN HOLE #A AT 2 O-CLOCK IN FRAME LAYER AT UPPER DOUBLE JOGGLE AREA FR 20 LH SIDE. S/O 193151 NR 28489Aug 8, 2024 · N218NV · Airbus A320214SDR ASAA2024080851821Frame Splice · corrodedAFT PIT, FRAME SPLICE STA 787 O/B OF SHEILD PANEL IS CORRODED. GROUNDED - YES. REMOVED DAMAGE FOUND TO BE OUT OFF LIMITS,REMOVED AND REPLACED FRAME SPLICE ON AFT PIT STA 787 IAW B737-700 SRM 51-40-02-0G-0W=1" O=0.063" R=0.053" L=1" D=.010".Aug 8, 2024 · N618AS · Boeing 737790SDR DALA2024080907961Frame · cracked(LOG 0491808) CRACK ON RH FUSELAGE FRAME AT FASTENER HOLE ON STA 500F. BTW S-8R & S-9R. RH FUSELAGE FRAME ON STA 500F. BTW S-8R & S-9R WAS REPAIRED UNDER CARD AMDS 2526-01236-02B.Aug 8, 2024 · N3732J · Boeing 737832SDR DALA2024080907960Frame · cracked(LOG 0491789) CRACK ON RH FUSELAGE FRAME AT FASTENER HOLE ON STA 400. BTW S-8R & S-9R. SUMMARY OF NRC 00300-RH FUSELAGE FRAME ON STA 400 BTW S-8R & S-9R WAS REPAIRED UNDER CARD AMDS 2526-01236-02B.Aug 8, 2024 · N3732J · Boeing 737832SDR DALA2024080907959Frame · cracked(LOG 0491786) CRACK ON RH FUSELAGE FRAME AT FASTENER HOLE ON STA 400. BTW S-8R & S-9R. RH FUSELAGE FRAME ON STA 400 BTW S-8R & S-9R WAS REPAIRED UNDER CARD AMDS 2526-01236-02B.Aug 8, 2024 · N3732J · Boeing 737832SDR DALA2024080907958Frame · cracked(LOG 0491502) CRACK ON RH FUSELAGE FRAME AT FASTENER HOLE ON STA 867. BTW S-8R & S-9R. RH FUSELAGE FRAME ON STA 867. BTW S-8R & S-9R WAS REPAIRED UNDER CARD AMDS 2526-01236-02B.Aug 8, 2024 · N3732J · Boeing 737832SDR DALA2024080907957Frame · cracked(LOG 0491496) CRACK ON RH FUSELAGE FRAME AT FASTENER HOLE ON STA 727D. BTW S-8R & S-9R. FUSELAGE FRAME ON STA 727D. BTW S-8R & S-9R WAS REPAIRED UNDER CARD AMDS 2526-01236-02B.Aug 8, 2024 · N3732J · Boeing 737832SDR DALA2024080907956Frame · cracked(LOG 0491487) CRACK ON LH FUSELAGE FRAME AT FASTENER HOLE ON STA 500C. BTW S-8L & S-9L. LH FUSELAGE FRAME ON STA 500C. BTW S-8L & S-9L WAS REPAIRED UNDER CARD AMDS 2526-01236-02A.Aug 8, 2024 · N3732J · Boeing 737832SDR DALA2024080907955Frame · cracked(LOG 0491456) CRACK ON LH FUSELAGE FRAME AT FASTENER HOLE ON STA 400. BTW S-8L & S-9L. LH FUSELAGE FRAME ON STA 400 BTW S-8L & S-9L WAS REPAIRED UNDER CARD AMDS 2526-01236-02A.Aug 8, 2024 · N3732J · Boeing 737832SDR FDEA202408081094Frame · crackedAFTER INSPECTION PER EO F-5310-E0329085 P6 STEP 3 CRACK WAS FOUND AT FRAME STA 1640 STR 14R. ACCOMPLISHED WITH E.A. WORK CARD # F-5310-T0380133 P1 (FUSELAGE- MAINFRAME-R/H 1640 TYPICAL FRAME SPLICE REPAIR BETWEEN STRINGER S-9R AND S-20R.)Aug 8, 2024 · N799FD · Boeing 757222SDR IXXA2024080830Frame · corrodedFLC LT - RT FRAME @ F/S 498 RBL 33-43 IS CORRODED & SEPERATEDAug 8, 2024 · N359AZ · Boeing 767323SDR IXXA2024080820Frame · corrodedFRAME WEB STA 518-522 RBL 35 CORRODEDAug 8, 2024 · N359AZ · Boeing 767323SDR KCSA202408081097Frame · corrodedEVIDENCE OF CORROSION ON RIENFORCEMENT CHORD ON FRAME STA 520 STR-15R TO STR-17R.Aug 8, 2024 · N708CK · Boeing 7474B5SDR KCSA202408081096Frame · corrodedCORROSION ON MAIN DECK FRAME AT STA 520 BETWEEN STR-16R TO STR-18R.Aug 8, 2024 · N708CK · Boeing 7474B5SDR AALA202411224770Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME OPEN FASTENER HOLE AT FR 16 RIGHT HAND UPPER CORNER. REPLACED FRAME PER EA 357796.Aug 7, 2024 · N750UW · Airbus A319112SDR AALA202411184770Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME OPEN FASTENER HOLE AT FR 16 RIGHT HAND UPPER CORNER. REPLACED FRAME PER EA 357796.Aug 7, 2024 · N750UW · Airbus A319112SDR VNAA202408070018Frame · corrodedFOUND CORROSION ON FS 1000 FRAME BETWEEN STRINGER 25R AND STRINGER 25L. REPAIRED CORRODED FRAME IAW MHIRJ REO 670-53-61-2311 REV.—DATED 2024-07-02.Aug 7, 2024 · N719PS · Cndair CL6002C10SDR DALA2024080907951Stub Frame · corroded(LOG 0489234) CORROSION ON STA 336 STUB FRAME AT STR 23L. REMOVED DAMAGE AND REPAIRED STUB FRAME @STA 336, STR 23L PER ERA 619511-14 REV ORIGINAL.Aug 7, 2024 · N392DA · Boeing 737832SDR DALA2024080907935Frame · corroded(LOG 0489325) CORROSION AFT CARGO BAY UPPER CROWN OF FRAME @STA. 787, RBL20 TO 22. REMOVED DAMAGE AND REPAIRED FRAME IN AFT CARGO BAY @STA. 787, RBL 20 TO 22 PER ER/A 619413-14 REV ORIGINAL.Aug 7, 2024 · N392DA · Boeing 737832SDR DALA2024080807909Frame · corroded(LOG 0487926) DURING INSPECTION, CORROSION DAMAGE WAS FOUND TO THE STA 787 FRAME WEB BETWEEN S-25R AND S-26R. CORROSION REPAIRED PER ERA 619413-14.Aug 6, 2024 · N392DA · Boeing 737832SDR DALA2024080807882Frame · crackedCRACK ON FRAME STA Y=694 LH SIDE AT CANTED KEEL INTERNAL STRUCTURE. SUMMARY OF NRC 00340: LH SIDE FRAME STA Y=694 INBOARD EDGE WAS REPAIRED PER B717-200 SRM 51-70-11-2R PROCEDURE 1 REPAIR 1 AND OUTBOARD EDGE WAS REPAIRED PER ERA 545683-14MA REV ORIGINAL. ASSOCAug 6, 2024 · N980AT · Boeing 717200SDR N6WA2024080708Frame · corrodedFRAME AT FS1015 HAS CORROSION BETWEEN STGR26R AND STGR22L. REPAIRED FRAME AT FS1015.00 IAW STS EA 81-2024-109.Aug 6, 2024 · N531GJ · Cndair CL6002C11SDR N6WA2024080707Frame · corrodedFRAME AT FS985.00 IS CORRODED BETWEEN STINGER 26L AND STRINGER 24R. REPAIRED FRAME AT FS985.00 IAW STS EA126-2024-`173 REV IR.Aug 6, 2024 · N531GJ · Cndair CL6002C11SDR N6WA2024080704Frame · corrodedFS969 FRAME IS CORRODED BETWEEN STRINGERS 26L AND 26R. REPLACED FS969 FRAME IAW STS EA 126-2024-172.Aug 6, 2024 · N531GJ · Cndair CL6002C11SDR DALA2024080707854Frame · corrodedSHIP 3148 CORROSION WEB FRAME 20 AT LEVEL OF STRINGER 23 RIGHT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED WEB LOCATED ON FRAME 20 TO FRAME 24 AT LEVEL OF STRINGER 23 RH SIDE FWD GALLEY AREA AS PER A319 SRM 51-42-11 AND A319 SRM 51-72-11. (0488227)Aug 6, 2024 · N348NB · Airbus A319114
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