JASC 5310
Service difficulty reports · 38,528
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 AALA202110190323Channel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION OF Z-CHANNEL NEAR FASTENER HOLES AT STA 990 BETWEEN RBL 34 AND RBL 47, MEASURING L=1.0 IN, W=1.25 IN, D=0.02 IN. REPLACED Z-CHANNEL WITH NEW IAW AARD 51-00-05 AND SRM 51-40-02.SDR AALA202110191454None · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN MAIN CABIN FLOOR BREAK ASSEMBLY AT STA 540 BETWEEN LBL 24 AND RBL 24, MEASURING L=1.0 IN. REPLACED BREAK ASSEMBLY WITH NEW IAW B737-NG SRM 51-40-02-OG AND 51-40-05-OG.SDR FDEA202110152541Seat Track · crackedSEAT TRACK AT STA 580, LBL 45, FLANGE HAS A CRACK. REPAIRED SEAT TRACK LBL45 AT STA 530 - 680 IAW EA# F-5321-T0364473, FUSELAGE - CARGO FLOOR - SECTION 43 - MCD SEAT TRACK FLANGE CRACK AT STA 580 LBL45. MAJOR REPAIRSDR MASA20220329146Intercostal · corrodedCORROSION WERE FOUND ON INTERCOSTALS (4 EIA)BETWEEN FS 349 AND FS364 AND STRGR.26R TO 26L IN REF SB 53-057C AT MAIN AVIONICS COMP.(EIE). INTERCOSTALS (2 EA) ON RBL 2 AND LBL 2 BETWEEN FS349 -FS364 WERE INSTALLED PER CRJ-900 SRM 51-42-06 AND CRJ-900 SRM 51-42-2SDR MASA20220329142Frame · corrodedCORROSION ON FRAME FS319 BETWEEN STRINGER 26L TO 26R AT MAIN AVIONICS COMPARTMENT.(E/E)
CORROSION ON FRAME FS319 BETWEEN STRINGER 26L TO 26R WAS REPLACED PER CRJ-900 SRM 53-00-06SDR FDEA202110142634Door Frame · corrodedAFT CARGO DOOR JAMB - AFT SIDE STA 1959, BETWEEN L40 - L45 HAS INTEGRANULAR CORROSION IN SEVERAL PLACES ON FWD SIDE OF FRAME INSTALLED NEW FRAME P/N: AGA7202-501 REF MD-11 SRM 51-33-01-0G, SRM 51-35-01-0G, AND DRAWING AGA7202, NGA6084. MAJOR REPAIR.SDR ASAA2021101436429Plate · corrodedFWD CARGO RH TRANSITION PANEL HAS AREAS OF CORROSION FROM STA 500D TO 500L. GROUNDED - YES. REPAIRED FWD CARGO RH TRANSITION PANEL FROM STA 500C TO 500L IAW 737-900ER SRM 53-00-53-2R-5 PANEL WAS FOUND TO BE OUT OF LIMITS IAW 737-900ER SRM 53-00-53-1A-2 DETAIL SDR ASAA2021101436428Plate · corrodedFWD CARGO LH TRANSITION PANEL HAS AREAS OF CORROSION FROM STA 500D TO 500L. GROUNDED - YES. REMOVED CORROSION AND CHECKED LIMITS FOUND TO BE OUT OF LIMITS IAW B737-900ER SRM 53-00-53-1A-2 REPAIRED TRANSITION PANEL IAW B737-900ER SRM 53-00-53-2R-5W=2.5 O=.040 RSDR JJBA20211014046None · noneNLG - INTERNAL - UPLOCK SUPPORT STRUCTURE - FWD CROSSBEAM CRACKED. REMOVED AND REPLACED NLG - INTERNAL - UPLOCK SUPPORT STRUCTURE - FWD CROSSBEAMSDR JR2R20211014498Frame · crackedLH WHEEL WELL FRAME 52 CRACKEDSDR SWAA2021112329531Web · crackedCRACK WEB LOCATED BTW BS294 TO BS303.9 AT LEVEL STR16L AT FWD GALLEY AREA ; 2021-460765 / [01] REPLACED WEB (INTERCOSTAL) LOCATED BTW BS294 TO BS303.9 AT LEVEL STR16L AT FWD GALLEY AREA IAW SRM B737-700 51-10-02 AND DRAWING 141A8180 REV:-; SEE INDIVIDUAL SIGN SDR SWAA2021112329545Pressure Deck · crackedCRACK ON PRESSURE DECK WEB, BS 663, LBL 32. REPAIRED THE PRESSURE DECK IAW EA 21-153-03222 AND EA WIP 1 21-153-03222.SDR REXA2021111700989Crossbeam · corrodedFS 280 LH CROSSBEAM CORRODED. - REMOVED AND REPLACED FS 280 LH CROSSBEAM IAW CRJ 900 SRMSDR ASAA2021101336439Transition Panel · corrodedFWD PIT L/H TRANSITION HAS AREAS OF CORROSION STA 500H TO 500L DOT # RSM 13-002. GROUNDED - YES. FWD PIT LH TRANSITION PANEL FROM STA 500H TO 500L OUT OF LIMITS IAW B737-900 SRM 53-00-53-1A-2, REPAIRED IAW B737-900 SRM 53-00-53-2R-5.W= 3 O= .040 R= .015 L= 6 DSDR ASAA2021101336438Web · corrodedFWD PIT DOOR CUTOUT LOWER SILL WEB IS CORRODED. DOT # RSM 13-001. GROUNDED - YES. CORROSION FOUND TO BE 100% MAT LOSS, OUT OF LIMITS IAW 737-900ER SRM 53-30-15-1A-1. REMOVED AND REPLACED SILL WEB IAW 737-900ER SRM 51-40-02-0G-0.W= 6.5" O= .045 R= 0.00 L= 4FT DSDR ASAA2021101336436Transition Panel · corrodedFWD PIT R/H TRANSITION HAS CORROSION JUST FWD OF STA 500I DOT #RSM 13-003. GROUNDED - YES. REPAIRED FWD PIT R/H TRANSITION AT STA 500I IAW B737-900 SRM 53-00-53-2R-5.W= 2 O= .040 R= .032 L= 4 D= .008.SDR ASAA2021101336430Plate · corrodedL/H TRANSITION PANEL CORRODED FROM STA 727B+10 TO STA 787. GROUNDED - YES. REMOVED CORROSION AND CHECKED LIMITS FOUND TO BE OUT OF LIMITS IAW B737-900ER SRM 53-00-53-1A-2 REMOVED AND REPLACED TRANSITION PANEL IAW B737-900ER SRM 53-00-53-2R-5W=2.0 O=.040 R=.021SDR ASAA2021101336422Plate · corrodedR/H TRANSITION PANEL CORRODED FROM STA 727C TO STA 767. GROUNDED - YES. REMOVED CORROSION AND CHECKED LIMITS AND FOUND TRANSITION PANEL TO BE OUT OF LIMITS IAW B737-900ER SRM 53-00-53-1A-2 REMOVED AND REPLACED TRANSITION PANEL IAW B737-900ER SRM 53-00-53-2R-5.SDR IPXA2021102675336Skin · noneINSPECTION TYPE:2CEXTERIOR FUSELAGE SKIN INCOMING REPAIR REQUIRES PERMANENT REPAIR.REPAIRED INCOMING FUSELAGE SKIN REPAIR BETWEEN STA. 970 TO 9801 AND BETWEEN L-43R TO L-48R IAW VT-SAA EA 011-5310-01-A9409 REV. I/R AND UPS EO MD11-5310-80738-A. (MAJOR) REF FAASDR IPXA2021102575298Stiffener · noneINSPECTION TYPE:4CLT MLG W/W VERTICAL STIFFENER CRACK AT AFT O/B WALL.REMOVED,FABRICATED AND REPLACED CRACKED VERTICAL STIFFENER IAW MD-11 SRM 51-35-01 AND SRM 51-33-01 (MINOR).SDR FDEA202110132523None · crackedSTATION 580 FLOORBEAM HAS A CRACK IN AFT UPPER FLANGE RADIUS @ APPROXIMATE LBL 40 REPAIRED FLOOR BEAM IAW FEDEX DRAWING SR57-53-004 & EA # F-5310-T0364849-P1SDR KCSA202110131115Tension Tie · wornL/H TENSION TIE AT FRAME 1120 HAS 2 EA HOLES THAT EXCEED ALLOWABLE LIMITS AS NOTED IN STEP 32 OF WO 745016239SDR KCSA202110131114Tension Tie · severedLH STA. 1160 FWD TENSION TIE SEVEREDSDR KCSA202110131112Tension Tie · crackedTENSION TIE BS 1180 L/H SIDE ONE HOLE CRACKED MARKEDSDR JR2R20211013208Frame · crackedCENTER FUSELAGE, RH WHEEL WELL FR 52 CRACKEDSDR JR2R20211013414Beam · corrodedCABIN FLOOR BEAM AT RBL12 CORRODED FR12-FR17SDR ASAA2021101236509Angle · corrodedZ ANGLE ON R/H SIDE FROM 986 TO 1006 HAS CORROSION. GROUNDED - YES. REMOVED AND REPLACED Z-ANGLE ON R/H SIDE FROM 986 TO 1006 IAW B737-700 SRM 51-40-02-0G-0W= 15" O= .071" R= 0.0 L= 2" D= .071.SDR ASAA2021101236508Floorbeam · corroded986 BEAM HAS SPOTS OF CORROSION FROM LBL 45 TO RBL 45. GROUNDED - YES. REPAIRED FLOOR BEAM IAW 737-700 SRM 53-70-51-2R-6.W= 2" O= .150" R= .115" L= 2" D= .035".SDR R61A2021110300857Shear Tie · corrodedDURING HEAVY CHECK MAINTENANCE FOUND CORROSION ON FWD FUSELAGE LOWER FRAME SHEAR CLIP AT FR17, BETWEEN STGR 26L AND 27L. FWD FUSELAGE LOWER FRAME SHEAR CLIP AT FR17, BETWEEN STGR 26L AND 27L REPLACED IAW SRM 51-41-01 AND SRM 51-41-02.SDR R61A2021110300856Shear Tie · corrodedDURING HEAVY CHECK MAINTENANCE FOUND CORROSION ON FORWARD FUSELAGE LOWER FRAME SHEAR CLIP AT FR17 BETWEEN STRINGER 26R AND 27R. CORRODED FWD FUSELAGE LOWER FRAME SHEAR CLIP AT FR17 BETWEEN STR 26R AND 27R REPLACED WITH NEW IAW EMB 170 SRM 51-41-02 AND 51-43-03SDR R61A2021110300855Shear Tie · corrodedDURING HEAVY CHECK MAINTENANCE FOUND FWD FUSELAGE LOWER FRAME SHEAR CLIP CORRODED AT FR16, BETWEEN STGR 27L AND STGR 28L. FWD FUSELAGE LOWER FRAME SHEAR CLIP AT FR16, BETWEEN STGR 27L AND STGR 28L REMOVED AND REPLACED IAW EMB 170 SRM 51-41-02 AND 51-43-01.SDR FDEA202110122709Floor Panel · damagedAFT CARGO COMPT FLOOR PANEL #152QF WAS FOUND EDGE DAMAGED. ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W A300-600F S.R.M 53-10-20-201 PARA.8B , FIG203 SHEET1 , P209-211.SDR FDEA202110122707Floor Panel · damagedFWD CARGO COMPT FLOOR PANEL #132LG WAS FOUND EDGE DAMAGED. ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W A300-600F S.R.M 53-10-20-201 PARA.8B , FIG203 SHEET1 , P209-211.SDR FDEA202110122705Floor Panel · damagedFWD CARGO COMPT FLOOR PANEL #132RG WAS FOUND EDGE DAMAGED. ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W A300-600F S.R.M 53-10-20-201 PARA.8B , FIG203 SHEET1 , P209-211.SDR ASAA2021101236441None · corrodedAFT PIT DOOR CUTOUT FWD SHIELD PANEL IS CORRODED. DOT # SM91-003. GROUNDED - YES. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW 737-900ER SRM 53-60-15-1A-1 REMOVED AND REPLACED SHEILD PNEL IAW 737-900 ER SRM 51-40-02-0G-0W= 2.5" O= .050 R= .028 L= 2FT D= .02SDR ASAA2021101236440Cargo Track · corrodedAFT PIT CARGO TRACK JUST I/B OF DOOR CUTOUT HAS CORROSION DOT # SM91-002. GROUNDED - YES. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW 737-900ER SRM 53-00-53-1A-2. REPAIRED CARGO TRACK IAW 737-900ER SRM 53-00-53-2R-3 REPAIR 3.W= 2" O= .075 R= .046 L= 3" D= SDR FDEA202110122712Floor Panel · damagedMAIN CARGO COMPT FLOOR PANEL #241GJ WAS FOUND EDGE DAMAGED. ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W A300-600F S.R.M 53-10-20-201 PARA.8A , P201-205 ,FIG201.SDR FDEA202110122710Floor Panel · damagedMAIN CARGO COMPT FLOOR PANEL #231EF WAS FOUND EDGE DAMAGED. ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W A300-600F S.R.M 53-10-20-201 PARA.8A , P201-205 ,FIG201.SDR SCNA20211028087None · noneCORROSION FOUND IN NUTPLATE @STA. 986.5, LBL 43, WL 208. CORROSION FOUND OUT OF LIMITS @ STA. 986.5, LBL 43 WL 208 PER SRM 53-70-51-1A-1, FIG 104. REPAIRED STA. 986.5 FLOOR BEAM PER SRM 53-70-51-2R-4, FIG 204.SDR AALA202110201023None · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION OF RH TRANSITION PANEL IN FWD CARGO BETWEEN STA 500D+10 AND STA 500F+10. REPAIRED TRANSITION PANEL IAW B737-NG SRM 53-00-53-2R-S.SDR ASAA2021101036520Doubler · crackedEXTERNAL POWER DOOR FLANGE IS CRACKED. GROUNDED - YES. REPAIRED EXTERNAL POWER DOOR FLANGE IAW B737-700 SRM 53-10-15-2R-5 REPAIR 5 CAT B REPAIR SIR THRESHOLD IS 50,000 FLIGHT CYCLES AT INTERVALS OF 6,000 FLIGHT CYCLES IAW B737-700 SRM 53-10-15-2R-5.SDR FDEA202110102716None · wornN00301 FR38.2/FR40 RH NO.4 DUMMY SEAT TRACK GAP OVER 1.0MM. I.A.W A300-600 SRM 53-15-16-201 PARA 5A P.201~210 FIG.201 PFM REPAIR ACCOMPLISHED.SDR FDEA202110102715None · wornN00302 FR54/FR54.2 LH NO.5 DUMMY SEAT TRACK GAP OVER 1.0MM. I.A.W A300-600 SRM 53-15-16-201 PARA 5A P.201~210 FIG.201 PFM REPAIR ACCOMPLISHED.SDR FDEA202110102714None · wornN00303 FR54/FR54.2 RH NO.5 DUMMY SEAT TRACK GAP OVER 1.0MM. I.A.W A300-600 SRM 53-15-16-201 PARA 5A P.201~210 FIG.201 PFM REPAIR ACCOMPLISHED.SDR JR2R20211010416Doubler · corrodedCABIN FLOOR SUPPORT WEB AT FR13 - FR14 RBL 40 CORRODED OUT OF LIMITSSDR FDEA202110092786Shear Tie · corrodedAFT CARGO - CENTER SHEAR-TIE AFT SIDE OF FRAME STA 1967 SHOWS SIGN OF EXFOLIATED CORROSION.(MARKED) REMOVED AND REPLACED SHEAR TIE PER DWG AGA7134 AND SRM51-33-01-OG.SDR ASAA2021100936502Frame · crackedFRAME CRACKED AT STA 907 JUST ABOVE STR 9 R/H AT I/B HOLE. GROUNDED - YES. REPAIRED CRACKED FRAME IAW AD20090102-700-25-1R FIG 14.SDR ASAA2021100936501Frame · crackedFRAME AT STA 867 IS CRACKED JUST ABOVE STR 9 R/H, AT I/B HOLE. GROUNDED - YES. REPAIRED FREAME IAW AD20090102-700-25-1R FIG 6.SDR ASAA2021100936500Frame · crackedFRAME AT STA 787 IS CRACKED JUST ABOVE STR 9 R/H, AT I/B HOLE. GROUNDED - YES. REPAIRED FRAME IAW AD20090102-700-25-1R, FIG 6.SDR ASAA2021100936499Frame · crackedFRAME AT STA 727D CRACKED JUUST ABOVE STR 9 R/H AT I/B HOLE. GROUNDED - YES. REPAIRED FRAM IAW AD20090102-700-25-1R FIG 6.
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