JASC 5310

Service difficulty reports · 38,548

Reports filed under 5310 · Fuselage Main, Structure, 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 = '5310'
  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 DALA2020020500889Failsafe · crackedAD/EM EO TASK-UT INSPECTION FOUND CRACKING INDICATION IN RH STA955 FAIL SAFE STRAP PER W/C 5312-01170-06 STEP 8 AND TO REPAIR THE FAIL SAFE STRAP IN ACCORDANCE WITH EM 5312-01170 FAIL SAFE STRAP AT RH STA 955 REPAIRED AS PER W/C 5312-01170-10B -02. (1476361)Feb 5, 2020 · N838MH · Boeing 767432ERSDR DALA2020020500888Failsafe · crackedAD/EM-EO TASK-UT INSPECTION FOUND CRACKING INDICATION IN LH STA955 FAIL-SAFE STRAP PER W/C 5312-01170-05 STEP 8 AND TO REPAIR THE FAIL SAFE STRAP IN ACCORDANCE WITH EM 5312-01170 FAIL-SAFE STRAP AT LH STA955 REPAIRED AS PER W/C 5312-01170-10A- 02. (1476343)Feb 5, 2020 · N838MH · Boeing 767432ERSDR SWIA2020032649354Stop Fitting · chafed* L/H AFT AVIONICS DOOR STOP FITTING ON FUSELAGE IS CHAFED. (C-CHECK) RO 3/25/2020 REPLACED L/H AFT AVIONICS DOOR STOP FITTING ON FUSELAGE. REF CRJ200 SRM AND BOMBARDIER ENG. DWG. COMPLIED WITH (CL600-2B19) STRUCTURAL MAJOR REPAIR (**RII**)Feb 4, 2020 · N709BR · Cndair CL6002B19SDR SWIA2020032649353Stop Fitting · chafed* R/H FORWARD AVIONICS DOOR STOP FITTING ON FUSELAGE IS CHAFED. (C-CHECK) RO 3/25/2020 REPLACED R/H FORWARD AVIONICS DOOR STOP FITTING ON FUSELAGE. REF CRJ200 SRM AND BOMBARDIER ENG. DWG. COMPLIED WITH (CL600-2B19) STRUCTURAL MAJOR REPAIR (**RII**).Feb 4, 2020 · N709BR · Cndair CL6002B19SDR SWIA2020032649352Stop Fitting · chafed* L/H FORWARD AVIONICS DOOR STOP FITTING ON FUSELAGE IS CHAFED. (C-CHECK) RO 3/25/2020 REPLACED L/H FORWARD AVIONICS DOOR STOP FITTING ON FUSELAGE. REF CRJ200 SRM AND BOMBARDIER ENG. DWG. COMPLIED WITH (CL600-2B19) STRUCTURAL MAJOR REPAIR (**RII**)Feb 4, 2020 · N709BR · Cndair CL6002B19SDR SWAA2020022094570Web · corrodedFORWARD CARGO COMPARTMENT DOOR CUT OUT BOTTOM WEB CORRODED BETWEEN BS. 440 TO BS. 492, BETWEEN RBL 23 TO RBL 30. / REPAIRED WEB IAW SRM & DWG.Feb 4, 2020 · N799SW · Boeing 7377Q8SDR CALA2020020800371Window Frame · crackedDURING C-2 CHECK AT AAR DLH "REFNON-ROUTINE 9622631" FOUND WINDS HIELD CENTER POST LOWER ATTACHMENT INTERNAL R/H WINDSHIELD FRAME HAS CRACK INDICATION IN UPPER RADIUS OF CUTOUT EMINATING OUT OF UPPER BOLT HOLE. ACCOMPLISHED INTERIM REPAIR PER PART 1 OF ECRA 53Feb 4, 2020 · N825UA · Airbus A319131SDR CALA2020020800370Window Frame · crackedDURING C-2 CHECK AT AAR DLH "REF NON-ROUTINE 9622630" FOUND WINDSHIELD CENTER POST LOWER ATTACHMENT INTERNAL LH WINDSHIELD FRAME HAS CRACK INDICATION IN UPPER RADIUS OF CUTOUT EMINATING OUT OF UPPER BOLT HOLE. ACCOMPLISHED PART 1 OF ECRA 5311-02243. NEED TO ACFeb 4, 2020 · N825UA · Airbus A319131SDR DALA2020020500886Service Panel · corrodedCORROSION ON LAVATORY SERVICE PANEL (FUS) ( AMDS 5300-2264) SUMMARY OF NRC 00033. CORROSION LEVEL 2: LAVATORY SERVICE PANEL WAS REPLACED PER MD-90 SRM 51-30-02 AND 51-30-05 VOL. II (1475820)Feb 4, 2020 · N908DA · Doug MD9030SDR CALA2020020870333Angle · corrodedB757-53-3-0593 FUSELAGE CUTOUT SUPPORT STRUCTURE FOR APU AIR INL ET DOOR HOUSING ASSY HAS CORROSION. RL024 REF. ST.ENGINEERING N/ R 0086925 FOUND CORROSION OUT OF LIMITS ON APU AIR INLET SUPT STRUCTURE BE TWEEN STA 1787-1825 AND S-3R TO 6R,UPPER ANGLE L=28.5 WFeb 3, 2020 · N57852 · Boeing 757324SDR CALA2020020870332Door Frame · corrodedAFT CARGO COMPARTMENT DOOR CUTOUT, BOX BEAM UPPER SKIN, FR 52.5- 56 STGR 39R-41R, MULTIPLE AREAS OF CORROSION - {A3NB-53-4-6179} - REMOVED AND REPLACED AFT CARGO COMPARTMENT DOOR CUTOUT BOX BEAM UPPER SKIN AT FR52.5-56 STR 39R-41R IAW A320 SRM 51-72-11-911-00 Feb 3, 2020 · N466UA · Airbus A320232SDR CALA2020020870330Crease Beam · corrodedB757-53-3-0557 RH CREASE BEAM INNER CHORD HAS CORROSION ON UPPER SURFACE,LEADING UNDER DRAIN PAN,FROM STA 730-STA 740.(96-86) RE F. ST. ENGINEERING N/R 0087599 FOUND CORROSION REMOVAL OUT OF LIMITS ON CABIN CREASE BEAM INNER CHORD AT STA 730-740 RBL 60,L=6.0 WFeb 3, 2020 · N57852 · Boeing 757324SDR CALA2020020700329Crease Beam · corrodedB757-53-3-0557 LH CREASE BEAM INNER CHORD HAS CORROSION ON UPPER SURFACE LEADING UNDER DRAIN PAN AT L-2 SILL,STA 735. (96-81) RE F ST. ENGINEERING N/R 0087573 FOUND CORROSION REMOVAL OUT OF LIMITS ON CABIN CREASE BEAM INNER CHORD AT STA 735-733 CBL 60,L=2.0,W=Feb 3, 2020 · N57852 · Boeing 757324SDR SWAA2021082319875Door Frame · crackedCRACK IN RADIUS OF FRAME AT B.S. 312; JUST ABOVE FORWARD ENTRY DOOR CUT OUT. / CRACK IN RADIUS OF FRAME @ BS 312 JUST ABOVE FORWARD ENTRY DOOR CUTOUT WAS NOTCHED OUT IAW EA 1-753-36506 REV IR DATED 02/24/2020 & ATS ER 20-01622 REV IR DATED 02/24/2020Feb 2, 2020 · N425LV · Boeing 7377H4SDR SWAA2020022641698Stub Frame · crackedR1 DOOR STUB FRAME CRACKED AT BS. 294.5, RBL 56. / R&R STUB FRAME IAW SRM AND IAW DWG.Feb 2, 2020 · N425LV · Boeing 7377H4SDR R61A202002220231Crossbeam · corrodedDURING HEAVY CHECK MAINTENANCE FOUND CORROSION ON AFT WET AREA CROSSBEAM AT FR84 LBL 30" IN 2 LOCATIONS AS MARKED. PERFORMED CUTOUT AND INSTALLED REPAIR INNER DOUBLER, FILLER 2EA, AND SHIM AT CROSSBEAM FR 84 LBL 30'' REF ETD2020-170-003716 AND SRM 53-00-10 TAFeb 2, 2020 · N232JQ · Emb ERJ170200LRSDR DALA2020020620926Structure · damaged(AIRCRAFT 7108, L/P 1471791) FWD CARGO LH SIDE FRAME INTERIOR SURFACE FOUND TOOL MARKS AT APPROX STA 1010-1014BTW =35L-36L AS MARKED. CORRECTIVE ACTION: REMOVED AND SMOOTHED OUT AS PER B777-200 SRM 51-10-02.Feb 2, 2020 · N708DN · Boeing 777232SDR DALA2020020300794Door Frame · crackedINITIAL INSPECTION: CRACK ON DOOR JAMB WEB STA 207, LONG 11 LH ( L1) CRACK ON DOOR JAMB WEB STA 207, LONG 11 LH WAS REPAIRED PER. MD-90 SRM 53-60-02 FIG. 15 VOL. I. (1472823)Feb 2, 2020 · N908DA · Doug MD9030SDR DALA2020020300793Door Frame · crackedCRACK ON DOOR JAMB WEB STA 207, LONG 15 LH ( L1) CRACK ON DOOR JAMB WEB STA 207, LONG 15 LH WAS REPAIRED PER. MD-90 SRM 53-60-02 FIG. 15 VOL. I. (1472815)Feb 2, 2020 · N908DA · Doug MD9030SDR DALA2020020320786Pressure Deck · corroded-LH CABIN CANTED PRESSURE DECK WEB FOUND CORROSION AT STA 960 LBL 92 & LBL 95.REFER TO CPCP TASK 53-510-00. C/A CORROSION ON LH CABIN CANTED PRESSURE DECK WEB AT STA 960 LBL 92 AND LBL 95 REPAIRED AS PER PRI 584152-14 REV.0. THE PRI 584152- 14 REV.0 COMPLIED TFeb 2, 2020 · N838MH · Boeing 767432ERSDR DALA2020020320784Pressure Deck · corrodedRH CABIN CANTED PRESSURE DECK WEB FOUND CORROSION AT STA 960,RBL 95,REFER TO CPCP TASK 53-510-00. C/A CORROSION ON RH CABIN CANTED PRESSURE DECK WEB AT STA 960 RBL 95 REPAIRED AS PER PRI 584153-14 REV.0.THE PRI 584153-14 REV.0 COMPLIED THE ERA 584153-14 REV.ORFeb 2, 2020 · N838MH · Boeing 767432ERSDR SWAA2020022874839Crease Beam · corrodedFORWARD GALLEY DOOR INBOARD CREASE BEAM CHORD (MOP SEAL) CORRODED BETWEEN BS. 316+10 TO BS. 328, RBL 60. / REPAIRED CREASE BEAM PER ER.Feb 1, 2020 · N8601C · Boeing 7378H4SDR SWAA2020022874838Crease Beam · corrodedAFT GALLEY DOOR INBOARD CREASE BEAM CHORD CORRODED BETWEEN BS. 951 TO BS. 992.8, RBL 50. / REPAIRED CHORD IAW SRM AND ER.Feb 1, 2020 · N8601C · Boeing 7378H4SDR SWAA2020022871773Crease Beam · corrodedAFT ENTRY DOOR INBOARD CREASE BEAM CHORD CORRODED BETWEEN BS. 951 TO BS. 992.8, LBL 50. / REPAIRED INBOARD CREASE BEAM IAW EA AND ER.Feb 1, 2020 · N8601C · Boeing 7378H4SDR EE4Y202002010590Structure · corrodedLOWER FUSELAGE AFT CARGO COMPT. AT BS 727F BTWN S-27L AND S-27R WITH LOWER SECTION CLIPS CORRODED. THE MENTIONED CLIPS WERE REPLACED.Feb 1, 2020 · N309GT · Boeing 7374Q8SDR DALA2025011500351Door Frame · damagedR1 DOOR CUTOUT SURROUND WAS DAMAGED BY GROUND EQUIPMENT. PERFORM A DAILY INSPECTION OF THE R1 DOOR REWORK AREA REF ER/A 584985-14 REV ORIGINAL, SECTION 2. ACCOMPLISHED DURING LAYOVER IN MSP 31JAN20. FOLLOW ON ACTION IS REQUIRED. ACCOMPLISH SECTION II EVERY DAYJan 31, 2020 · N921AT · Boeing 717200SDR DALA2020020100775Door Frame · corrodedCORROSION ON PREVIOUS REPAIR SPACER AT AFT CARGO COMPT LOWER DOOR JAMB STA 1211 TO 1268 MRB 53-123-02 CARGO COMPT LOWER DOOR JAMB STA 1211 TO 1268 WAS REPLACED PER MD90 VOL. L SRM 53-60-02 FIG. 9 (1469805)Jan 31, 2020 · N908DA · Doug MD9030SDR DALA2020013100731Rib · crackedFOUND CRACK IN AFT TAIL COMPARTMENT 3RD RIB FWD OF AFT RIB ON RIGHT SIDE, MARKED BY TAPE. FWD TO N.R 001,& NR 002. (AWAITING SUPPLEMENTAL INFORMATION). (LP6466754)Jan 31, 2020 · N960DL · Doug MD88SDR RAIA2020020400002Skin · crackedCAPT TOP EXTIRIOR LATERAL POST SKIN IS CRACKED...(MAJOR REPAIR) REPAIRED PER ETD2020-145-002977 AND EO-EMB145-53-070-OJan 30, 2020 · N835HK · Emb EMB145LRSDR DALA2020020310847Door Sill · corrodedSHIP 5801 INITIAL INSPETION : CORROSION ON LH EMERGENCY EXIT DOOR # 3 LOWER SILL AT PAX CABIN. CORRECTIVE ACTION: SUMMARY OF NRC 00193 CORROSION LEVEL 2 ON LH EMERGENCY EXIT DOOR # 3 LOWER SILL WAS REMOVED AND MEASURED AND IT IS BEING OUT OFF LIMITS THEREFORE Jan 30, 2020 · N581NW · Boeing 757351SDR SIMA202002030005Crossbeam · corrodedCENTER OMEGA BEAM CORRODED AT CROSS BEAM FRAME 49-C/A-ACCOMPLISHED REPAIR OF CENTER OMEGA BEAM CROSS BEAM FRAME 49 IAW EMB 145 SRM 53-00-10 FIG 203 AND ERS-EM-5300-4002 FOR USE OF ALTERNATE FASTENERSJan 30, 2020 · N676AE · Emb EMB145LRSDR CALA2020020200307Beam · crackedINIATE A DTA DIP TO ACCOMPLISH INSPECTION REQUIREMENTS ON OR BEFORE THE AIRCRAFT REACHING 75000 TOTAL AIRCRAFT FLIGHT CYCLES PLANNING TO CONTACT ENGINEERING AFTER 69000 TOTAL AIRCRAFT FLIGHT CYCLES BUT BEFORE 70000 TOTAL AIRCRAFT FLIGHT CYCLES FOR THE INSPECTIJan 30, 2020 · N76254 · Boeing 737824SDR SROM202001302003Structure · corrodedCORROSION ON Z SECTION AT STA. X32 LBL 38 UNDER FLOOR US BEYOND LIMITS. Z SECTION REPLACED WITH MANUFACTURED PART IAW DHC-8-400 SRM 53-20-43, ITEM 211, AND 51-24-35 REV. 19. INSTALLED Z SECTION FOLLOWING SRM REV. 19 SECTION 51-42-05.Jan 30, 2020 · N794CP · Bombdr DHC8402SDR SWAA2020021941525Pressure Deck · crackedHORIZONTAL PRESSURE DECK CRACKED L/H OUTBOARD SIDE BETWEEN BS. 666 TO BS. 670, LBL 69. / R&R WEB IAW EA, DWG, & ER.Jan 29, 2020 · N7824A · Boeing 7377BKSDR SWAA2020021241283Beam · crackedR1 DOOR AT FORWARD GALLEY AREA LOWER BEAM CRACKED. / R&R LOWER BEAM IAW SRM AND DWG.Jan 29, 2020 · N7874B · Boeing 7377Q8SDR DALA2020013000700Pressure Panel · damagedCRACK INDICATION FOUND IN OPEN HOLES (2 E/A) LOCATED ON PRESSURE PANEL AT FRAME 36 RH SIDE AND -Y1292+2", AND OTHER -Y1292+3" A CRACKS THAT DOES NOT EXCEED THE AUTHORIZED REPAIR AREA WAS FOUND AT THE PRESSURE PLATE AREA BETWEEN FR 35RH AND FRAME 36 RH. REPAIR Jan 29, 2020 · N330NB · Airbus A319114SDR C77A2020013080010Crossbeam · corrodedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIR OF CORROSION DAMAGE DISCOVERED DURING BASIC CHECK AT EAMS ON THE UPPER FLANGE OF THE FR84 CROSSBEAM IN THE CABIN FLOOR STRUCTURE OF THE CENTER FUSELAGE III. THE DAMAGE IS LOCATEJan 29, 2020 · N206NN · Emb ERJ170200LRSDR SWIA2020031049188Door Frame · crackedFRAME AT FS1144 IS CRACKED AT THE LH SIDE OF THE AEB DOOR OPENING (C-CHECK) RO 3/6/2020 REPLACED FS.1144 LOWER FRAME ASSY WITH NEW FRAME REF BOMBARDIER DWG. CRJ 900 SRM.Jan 28, 2020 · N821SK · Cndair CL6002D24SDR REXA2020020580164Floorbeam · corroded"UPON REMOVAL OF FS 280 J-ANGLE FOUND CORROSION ON FS 280 L/H BEAM. REMOVED AND REPLACED LH BEAM IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01 AND 51-40-11-001-001-A01.Jan 28, 2020 · N181PQ · Cndair CL6002D24SDR REXA202002058161Post · corroded"R/H F.S. 280 ENTRY WAY POST AT F.S. 280 IS CORRODED AT THE BOTTOM. ""CUT & REMOVED LOWER END OF F.S. 280 DOOR POST AT RBL 11.128 AND REPAIR ED IAW CRJ 900 SRM 53-11-10-201-006-A01. WVAC STAMP EMP# 712 MTC "Jan 28, 2020 · N181PQ · Cndair CL6002D24SDR C77A2020012800001Service Panel · corrodedWASTE SERVICING PANEL 152AR HAS CORROSION ON THE FORWARD LEFT CORNER OF THE INTERNAL SURFACE. REMOVED AND REPLACED WASTE SERVICING PANEL 152AR REF EMB AMM 20-10-02.Jan 28, 2020 · N206NN · Emb ERJ170200LRSDR VNAA2020012899905Crossbeam · crackedWHILE PERFORMING SB670BA-53-041 FOUND RH FS 280 CROSSBEAM CRACKED. REMOVED RH FS 280 CROSSBEAM REF CRJ 700 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 AND 51-42-13-001-001-A01. INSTALLED NEW SERVICEABLE BEAM IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-Jan 28, 2020 · N539EA · Cndair CL6002C10SDR VNAA2020012899901Post · corrodedFS 280 VERTICAL FLOOR POST AT RBL 9.00 IS CORRODED AT LWR POSITION. REMOVED FASTENERS COMMON TO FS 280 WEB IAW SRM 51-42-06-001-001-A01, 51-40-21-001-001-A01, 51-42-22-001-001-A01. DRILLED, LOCATED NEW SERVICEABLE CC670-34180-8 POST IAW SRM 51-40-06-001-001-Jan 28, 2020 · N539EA · Cndair CL6002C10SDR SWIA2020031649324Stop Fitting · chafed* THE AVIONICS BAY DOOR SURROUND STRUCTURE'S FWD LH AND FWD RH STOP FITTING ASSY'S ARE CHAFED. (MARKED WITH RED SHARPIE) (C-CHECK) RO 3/13/2020 REMOVED AND REPLACED THE AVIONICS BAY DOOR SURROUND STRUCTURE'S FWD LH AND FWD RH STOP FITTING REF CRJ-200 SRMJan 27, 2020 · N461SW · Cndair CL6002B19SDR R61A202002190200Beam · corrodedWHILE IN HEAVY CHECK FOUND CORROSION ON FWD WET AREA L/H BEAM BETWEEN FR16 AND FR19 IN 4 LOCATIONS AS MARKED. BLENDED CORROSION OUT IN 3 PLACES ON THE L/H BEAM PN170-03264-001 BETWEEN FR16 AND FR19 AS MARKED. FR 16-17 H=0.019", L=1", W=2". FR 17-18 H=0.023", LJan 27, 2020 · N230JQ · Emb ERJ170200LRSDR SWIA2020020648263Door Frame · corrodedFWD GALLEY SERVICE DOOR CUTOUT- BETWEEN FS 319.00 AND FS 349.00 STR 17R AND STR 18R THERE ARE 2 AREAS OF FLAKING /MISSING PAINT AND LIGHT CORROSION ON FLOOR SUPPORT BEHIND SERVICE DOOR LOWER LATCH FITTINGS. (C-CHECK) RO 2/04/2020 REPAIRED FWD GALLEY SERVICJan 27, 2020 · N943SW · Cndair CL6002B19SDR CALA2020020200290Door Frame · corrodedAFT CABIN DOOR CUTOUT FR68 ST22L-23L FWD FACE HAS CORROSION PER HAECO LCQ NR LP 9299010 CORROSION FOUND OUT OF LIMITS AROUND ANCHOR NUT AT FR 68 STRG 22 L-23L.ACCOMPLISHED REPAIR IAW SRM 53-41-12-300-002 PARAGRAPH 2 F IG 001.REQUIRES DETAILED VISUAL INSPECTIOJan 27, 2020 · N466UA · Airbus A320232SDR AALA2020013189018Doubler · crackedAIRCRAFT IN BASE MAINTENANCE, L1 DOOR CUT OUT, UPPER AFT CORNER DOUBLER COVER PLATE WAS CRACKED. REPLACED THE DOUBLER COVER PLATE IAW SRM 51-72-11.Jan 27, 2020 · N665AW · Airbus A320232SDR DALA2020013180733Structure · corrodedCORROSION ON BS 1470, LBL 2.90 IN THE AFT CARGO COMPARTMENT FLOOR STRUCTURE. REPAIRED IAW SRM 53-00-53-2R-1, REPAIR 1. HFEC INSPECTION WAS ACCOMPLISHED AND NO CRACKS WERE FOUND ON CUT EDGES IAW SRM 53-00-53-2R-1, REPAIR 1, PARAG 4.C. AND NDTM PART 6, 51-00-1Jan 27, 2020 · N547US · Boeing 757251SDR SWAA2020051829282Crease Beam · corrodedAFT CABIN INNER CREASE BEAM STA 947+17 - 967+17; RBL52; WL208 UPPER SURFACE HAS CORROSION / FOUND AFT CABIN CREASE BEAM STA 947+17 TO 967+17 RBL 52; WL 208 WAS OUT OF LIMITS; .090' ORIG; .079 REMAINING; .011 LOSS; REMOVED; LOCATED; DRILLED; AND INSTALLED NEW CJan 26, 2020 · N8603F · Boeing 7378H4
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