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.
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
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 SWAA2021081574512Plate · corroded*** SURFACE CORROSION *** FOUND AT FWD CARGO COMPARTMENT DOOR CUTOUT LOWER SILL WEB. PLATE MKD DOTS WL 153.5. / REMOVED AND REPLACED WEB PLATE AT FWD CARGO COMPARTMENT DOOR CUTOUT LOWER SILL IRW B737-700 SRM 51-40-02-0G-0 9 DRWG# 143A8330SDR SWIA2020060950999Door Frame · corrodedFWD BAG BAY DOOR SURROUND, LOWER STUB FRAME BELOW THE SILL PLATE HAS CORROSION AT APPROXIMATELY FS565.00. (C-CHECK) RO 4/23/2020 REMOVED AND INSTALLED NEW LOWER STUB FRAME AT FS 565 BETWEEN STR 25L AND STR26L REF SRM AND DRAWING. COMPLIED WITH TASK CARD AND PSDR SWIA2020060950998Door Frame · corrodedFWD BAG BAY DOOR SURROUND, LOWER STUB FRAME BELOW THE SILL PLATE HAS CORROSION AT APPROXIMATELY FS549.00. (C-CHECK) RO 4/23/2020 REMOVED AND INSTALLED NEW LOWER STUB FRAME AT FS 549.00 REF SRM AND DRAWING. SEE CONTINUATION CARD FOR DETAILS.SDR EE4Y2020043011335Beam · corrodedLOWER FUSELAGE FWD CARGO DOOR CUTOUT LOWER SECTION FROM FR24 TO FR27, HORIZONTAL SILL BEAM WITH CORROSION. NOTE: THE BEAM WAS REPLACED AS PER NOM ROUTINE JOB A1H251 ITEM 1-94.SDR FDEA2020051890836Door Frame · crackedAGING AIRCRAFT - EXISTING REPAIR AT MAIN DECK CARGO - R3 DOOR FORWARD JAMB LOWER WEB BOX STATION 1250.75 TO STATION 1256.75 LONGERON 26 RIGHT HAND TO LONGERON 27 RIGHT HAND . EXISTING REPAIR AT MAIN DECK CARGO - R3 DOOR FORWARD JAMB LOWER WEB STATION 125SDR FDEA202004290835Door Frame · crackedAGING AIRCRAFT - EXISTING REPAIR AT MAIN DECK CARGO - L3 DOOR AFT JAMB LOWER WEB BOX STATION 1305.25 TO STATION 1315.42 LONGERON 26 LEFT HAND TO LONGERON 27 LEFT HAND. EXISTING REPAIR AT MAIN DECK CARGO - L3 DOOR AFT JAMB WEB STATION 1305.25 TO STATION 1SDR FDEA2020051390835Door Frame · crackedAGING AIRCRAFT - EXISTING REPAIR AT MAIN DECK CARGO - L3 DOOR AFT JAMB LOWER WEB BOX STATION 1305.25 TO STATION 1315.42 LONGERON 26 LEFT HAND TO LONGERON 27 LEFT HAND. EXISTING REPAIR AT MAIN DECK CARGO - L3 DOOR FORWARD JAMB WEB STATION 1305.25 TO STATISDR FDEA2020043090831Beam · dentedAFT CARGO COMPARTMENT STATION 1841 BEAM WEB LEFT HAND X = 0 TO X = 9 FOUND DENTSDR FDEA202004260795Strap · gougedFUSELAGE EXTERIOR AFT CAGO DOOR CONTROL ANEL CUT OUT LOWER EDGE IS GOUGED ACCOMPLISHED BLEND REPAIR PER FEDEX EA F-5330-T0305556-P2SDR FDEA2020042760789Crease Beam · corrodedMAIN CABIN BETWEEN STA 860-879 CREASE BEAM CORRODED. REMOVED CORR ON RH CREASE BEAM STA 860-879 IAW B757 SRM 51-10-02. ORIG MAT .071 LOWEST REM .054 LOSS .017 FOUND OUT OF LIMITS IAW B757 SRM 53-30-13-1A. REPAIRED CREASE BEAM IAW B757 SRM 53-00-13-2R REP 1SDR DALA2020042902313Stop Fitting · cracked(AIRCRAFT 3159, L/P 1552579) CRACK INDICATION ON FRAME 68 AT INBOARD LOWER HOLE, DOOR STOP 1 AT AFT GALLEY AREA (1 EA) (CRACK DIRECTION:06 O'CLOCK ). CORRECTIVE ACTION: PERFORMED REPAIR ON HOLE LOC. FR68 AT INBOARD LOWER HOLE DOOR STOP 1 LH SIDE AT AFT GALLEY SDR DALA2020042902312Stop Fitting · cracked(AIRCRAFT 3159, L/P 1552577) CRACK INDICATION ON FRAME 68 AT INBOARD UPPER HOLE DOOR STOP 7 LH SIDE AT AFT GALLEY AREA (1EA) (CRACK DIRECTION:6 O CLOCK). CORRECTIVE ACTION: PERFORMED REPAIR ON HOLE LOC. FR68 AT INBOARD UPPER HOLE UPPER STOP 7 LH SIDE AT AFT GASDR UIEA2020042800858Structure · corrodedRH WLG BS 1241 RBL 94 CENTER FUEL PUMP LOWER AREA FOUND CORROSION.(<P>RH WLG BS 1241 RBL 94" CENTER FUEL PUMP LOWER AREA (WCS REAR SPAR WEB) CORROSION AREA REPAIRED IAW RI-57-10-14018 REV. A. </P>)SDR SWAA2021080544250Floor Panel · corrodedAFT PIT FLOOR PANEL 140 DF HAS CORROSION AT PERIMETER EDGES. / AFT PIT FLOOR PANEL 140DF HAS CORROSION AT PREMETER GOUGES. FABRICATED NEW FLOOR PANEL 140DF IAW B737 AMM 25-52-01-201-801. AND BOEING DWG 453A2610 REV B P/N 2024-T3-071 ATAG A48963SDR SWIA20205070543Beam · corroded* THE FS280 BEAM HAS CORROSION ON 2 SPOTS BETWEEN LBL9 AND RBL9, MARKED IN RED. (48 MO INSP) RO 5/6/2020 BLEND ON FS 280 BEAM BETWEEN LBL 9 AND RBL 9 IS LOCATED ON A REPAIR ANGLE P/N 601R-53-11-2930-6. NO ALLOWABLE DAMAGE LIMITS FOR BLENDS ON REPAIR PASDR AALA2020050109012Window Post · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FLIGHT DECK CAPTAINS L1 WINDOW CUT OUT UPPER OUTBOARD C-D WINDOW POST AT BS 219 AND S10L. REPAIRED WINDOW POST PER EA 304419 AND 304691.SDR AALA2020042749010Window Post · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FIRST OFFICERS # 3 WINDOW POST. REPAIRED WINDOW POST PER EA # 304780.SDR AALA2020042749009Window Post · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK SUSPECTED ON CAPTAINS # 3 WINDOW POST. REPAIRED # 3 WINDOW POST PER EA #304779.SDR IPXA2020060856217Door Frame · crackedINSPECTION TYPE:3C MAIN CABIN L3 DOOR LWR FWD DOOR JAMB WEB CRACKED BETWEEN STA 1256.75 AND 1250.75 BETWEEN DOOR STOP 7 AND Z-19. CUTOUT DAMAGE, FABRICATED REPAIR DOUBLER AND ACCOMPLISHED PERMANENT REPAIR AT MAIN CABIN L3 DOOR JAMB BETWEEN STA 1256.75 AND 1250SDR SWAA2020052643083Crease Beam · corrodedPASSENGER CABIN FLOOR; AFT GALLEY DOOR SURROUND CREASE BEAM OUTER ANGLE CORRODED STA.947-987 WL208. REMOVED CORROSION FROM CABIN FLOOR AFT GALLEY DOOR SURROUND CREASE BEAM OUTER ANGLE STA 947 - 987 WL208 RBL 66 IAW SRM 51-10-02-0G-0 AND INSPECTED W/ 10X MAG GSDR SWAA2020052643087Crease Beam · corrodedPASSENGER CABIN FLOOR, AFT ENTRY DOOR WAY CREASE BEAM STA 947-987 CORRODED AROUND FASTENER HOLES WL208 LBL 52. REMOVED CORROSION FROM AFT ENTRY DOOR WAY CREASE BEAM AT STA 947-987. ORIGINAL MATERIAL .080 LOSS OF .012 WITH .068 REMAINING IS OUT OF LIMITS IAW SDR SWAA2020052643415Crease Beam · corrodedCABIN FLOOR RIGHT CREASE BEAM WEB STA 727D+6' RBL 68.5 WL 208 LOWER SURFACE HAS CORROSION JUST OUTBOARD OF LIGHTNING HOLE. BLENDED CORROSION ON RT CREASE BEAM WEB PN 146A5925-24 AT STA 727D+6' RBL 68.5 WL208. LOWER SURFACE ORIGINAL THICKNESS .036', LOSS .005'SDR DALA2020042002283Pressure Panel · cracked(AIRCRAFT 3163, L/P 1549513) CRACK FOUND AT HOLE A LH. CORRECTIVE ACTION: REPAIRED ON PRESSURE PANEL AT FRAME 36L/H SIDE WAS ACCOMPLISHED WITH WORK CARD 5311-01171-04A. RII INSPECTION COMPLETE.SDR SIMA2020041716008Door Frame · corrodedDURING HMBV INSPECTION, QC FOUND CORROSION ON FR 22 AT SERVICE DOOR LOWER CUT-OUT.-C/A-PERFORMED PERMANENT REPAIR TO FR 22 AT SERVICE DOOR CUT-OUT IAW EMB 145 SRM 53-00-04RE.SDR SWAA2021081542648Plate · corrodedAFT CARGO COMP.DOOR SURROUND; FLOOR AFT CORNER PLATE CORRODED BOTTOM SIDE / EVALUATED CORNER PALTE CORROSION AT AFT CARGO DOOR SURROUND FLOOR AFT CORNER PLATE NO ALLOWABLE MATERIAL LOSS FOUND SRM PLATE OUT OF LIMITS REPLACED PLATE PART #453A2611-2 IAW BOEING DSDR MASA20200416008Door Frame · corrodedCORROSSION E&E DOOR CUT OUT FRAME FS364 STGR26R & STRG 25R. C/W EA 24-2020-024SDR KCSA202004151046Door Frame · crackedL3 DOOR FWD UPPER DOOR FRAME HAS CRACK AT LOWER SECTIONSDR KCSA202004151045Stop Fitting · crackedL3 DOOR FWD SIDE UPPER DOOR HINGE STOP FITTING CRACKEDSDR SWIA20205060497Door Frame · corroded*PASSENGER DOOR SURROUND STRUCTURE €“ FRAME FS319 €“ STGR18L TO 21L, HAS CORROSION AT GROUND STUDS. (MARKED) (C-CHECK) RO 5/4/2020 REMOVED AND INSTALLED NEW FRAME (P/N SH670-31891-3S) WITH NEW FASTENERS AT FS319.00 BETWEEN STGR18L AND 21L, REF BOMBARDIESDR DALA2020042802307Bushing · not reported(AIRCRAFT 3149, L/P 1548688) FR68, WHILE WORKING AMDS CARD 5311-01216-08 STEP #11 EXISTING REPAIR FOUND AT FR 68 RT DOOR STOP #1 LWR I/B FASTENER HOLE BUSHING REPAIR. LIAISON ENGINEERING EVALUATION AND DISPOSITION REQUIRED BEFORE FLIGHT. AD RELATED. CORRECTIVESDR CALA2020041300833Door Frame · crackedPERFORME ROTO INSP FND 2EA HOLE CRACK AT LH-FR68, DOOR STOP NO.1 LOWER INBOARD HOLE & LOWER OUTBOARD HOLE REF NON-ROUTINE NO.9407 207 - ORIGINATED EA 5340-01724 OP002 STEP 3.1. PERFORMED AT LH-FR68 DOOR STOP NO.1, 2EA CRACKED HOLES REPAIRED AS PER ECRA 5341-01SDR CALA2020041700837Crease Beam · corroded(B757-53-3-0557) CREASE BEAM INNER CHORD HAS CORROSION ON UPPER SURFACE,-LEADING UNDER DRAIN PAN AT L-2 LWR SILL, STA 730-740. R EF ST-SAA NR 0091960. FOUND LH CREASE BEAM INNER CHORD AT STA 660 TO 760 OUT OF LIMITS IAW B757-3 SRM 53-30-15-A1 - FIG 101 L=8 W=1SDR AALA2020050109013Window Post · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FLIGHT DECK FIRST OFFICERS R1 WINDOW CUT OUT UPPER OUTBOARD C-D WINDOW POST AT BS 219 AND S10R. REPAIRED WINDOW POST PER EA 304420 AND EA 304691.SDR ASAA2020042232664Beam · corrodedAFT MAIN CABIN HAD CORROSION AT FR 68 Y -1162 GROUNDED - YES. REMOVED AND REPLACED MAIN CBIN LONGITUDINAL BEAM AT FR 68 Y -1162 IAW AIRBUS DWG D53472780SDR ASAA2020042232661Beam · corrodedAFT MAIN CABIN R/H LONGITUDINAL BEAM HAD CORROSION ON UPPER SURFACE BETWEEN FR 68 AND FR 69 Y -1162 GROUNDED - YES. REMOVED AND REPLACED AFT MAIN CABIN LONGITUDINAL BEAM BETWEEN FR 68-69 Y -1162 IAW AIRBUS DWG D53472458 AND D53472089SDR VGCA2020041309006Pressure Panel · puncturedPRESSURE PAN WEB PUNCHTURED BETWEEN BS. 880 - 890 AND LBL. 48 - 68 AT MAIN CARGO DECK FLOOR. REPLACED WITH PART IN ACCORDANCE WITH B727 SRM.SDR VGCA2020041309005Pressure Panel · puncturedPRESSURE PAN WEB PUNCTURED BETWEEN BS. 880 - 890 AND RBL. 48 - 68 AT MAIN CARGO DECK FLOOR. REPLACED WITH NEW PART IN ACCORDANCE WITH B727 SRMSDR SWAA2021082036470Plate · corrodedAFT CARGO PIT; INTERIOR EDGE OF THE DOOR CUTOUT; METAL END PLATE AT FLOOR TRANSITION IS CORRODED. / EVALUATED CORROSION TO METAL ENDPLATE AT AFT CARGO PIT INTERIOR EDGE OF DOOR CUTOUT. NO ALLOWABLE LIMITS IN SRM. REPLACED PLATE 453A2611-1 IAW AIPC 25-52-10-02 SDR AALA2020041399002Expansion Joint · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED EXPANSION JOINT AT BS 540 BETWEEN BL 0 AND LBL 20. REPLACED EXPANSION JOINT PER AARD 51-00-05-1.SDR DALA2020040602184Stop Fitting · crackedCRACK INDICATION ON FRAME 16 RH SIDE ON DOOR STOP FITTING 7 HOLE 1, CRACK AT 7 O CLOCK ON UPPER FUSELAGE (1 EA), REPLACED NEW LOC. FR.16 RH SIDE ON DOOR STOP #7 7 ASPER A320 SRM 51-42-11 AND 51-72-11 AND DWG D53112300SDR CALA2020040300774Pressure Panel · crackedWHILE PERFORMING EA 5330-05216 OPS 3 R/H SIDE CENTER FUSELAGE PRESSURE PANEL FR35-36 FOUND SEVERAL HOLES CRCKED PERFORMED REPAIR PER EA 5330-05216 REV A OPS 3 AND ECRA 5331-02660 PART 1 ALL STEPS AND PLACED ON DIP PER ECRA PART 1 PARA C TO ACCOMPLISH A PERMANESDR CALA2020040300775Pressure Panel · crackedWHILE PERFORMING EA 5330-05216 OPS 2 L/H SIDE CENTER FUSELAGE PRESSURE PANEL FR35-36 FOUND SEVERAL HOLES CRCKED REPAIRED PER EA 5330-05216 REV A OPS 2 AND ECRA 5331-02661 PART 1 ALL STEP PLACED ON DIP PER EC/RA PART 1 PARA TO ACCOMPLISH A PERMANENT REPAIR BY OSDR CALA2020040300772Pressure Panel · crackedLH SIDE PRESSURE PANEL BETWEEN FR 35-36. NOTED CRACKS IN THE FOL LOWING HOLES: #1/2/4/5/6/7/8/9/10/13/14/17/20/22/26. NOTED REJEC TABLE INDICATIONS ON THE FOLLOWING HOLE # 30/32/34/35/38/39/40/4 3/45/46/48/53/54/58/59/60/63/65 AND I/B BRACKET HOLES: UPPER AND SDR CALA2020040300760Door Frame · corrodedWHILE AT AAR DLH DURING HMV-3 CHECK FOUND CORROSION ON FR68 AT STR23 AND A CRACK AT THE DOOR STOP #1, REPAIR BEFORE NEXT FLIGHT. ACCOMPLISHED INTERIM REPAIR PER PART 1 OF ECRA 5341-01220. ACCOMPLISH A PERMANENT REPAIR AT RH FR68, STR23 PER PART 3 OF ECRA 5341-SDR SWAA2021081235902Structure · damagedDAMAGED/ELONGATED FASTENER HOLE @ BS 727B; RBL 45.50 POS#4 REFERENCE EA 20-153-00054. / COMPLIED WITH EA 20-153-00106; FOR WORK PERFORMEDSDR SWAA2021081235017Structure · damagedDAMAGED/ELONGATED FASTNER HOLE @ BS 727B; RBL 45.50; POS #4 REFERENCE EA 20-153-00054. / (REF LP 0049247) COMPLIED WITH EA 20-153-00106; FOR WORK PERFORMED C/L # 35420SDR SWAA2021080534864Floor Panel · corrodedAFT CARGO COMPT; FLOOR PANEL 140CF HAS APPROXIMATELY 50' SQ OF CORROSION ON UPPER SURFACE. / FABRICATED NEW FLOOR PANEL 140CF I.A.W. SRM 51-40-05-0G-0 & BOEING DWG # 453A2610; REV: 16; EVALUATED CORROISON ON AFT CARGO FLOOR PANEL 140CF; FOUND TO BE OUT OF LIMISDR CALA2020033000747Door Frame · crackedAD 2018-25-02 L1 FRAME 16 DOOR STOP #1 INBOARD LOWER HOLE IS CRACKED IN THE WEB AND INTERCOSTAL LAYERS ON HAECO LCQ REF 9296352 SPEC A3NB-53-4-0017 GENERATED HAECO TECHNICIAN AND QC REPAIRED FR16 LH STOP FIT TING #1 HOLES #3 AND #4 IN WEB IAW ECRA 5311-02428 PSDR CALA2020033000743Door Frame · crackedAD 2018-25-01 FRAME 2O R1 DOOR STOP #1 INBOARD LOWER HOLE IS CRA CKED IN THE WEB AND INTERCOSTAL LAYERS ON HAECO LCQ REF 9296200 SPEC A3NB-53-4-0018 GENERATED HAECO AND REPAIRED FR20 RH STOP FITT ING #1 HOLES #3 AND #4 IAW ECRA 5311-02427 PART 1. DTA LOG PAGE SDR SWAA2020041335271Stud · damagedRH EMERGENCY DOOR EXIT CUT OUT FWD MID AND LOWER STUD COMMON TO SURROUND PANEL INSTALL DAMAGED / REMOVED AND REPLACED RH EMERGENCY DOOR EXIT CUT OUT FWD MID AND LOWER STUDS IAW SOPM 20-50-01. 59908U 28MAR20.
Back to JASC 5310