JASC 5340

Service difficulty reports · 22,411

Reports filed under 5340 · Fuselage Main, Attach Fittings, 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 = '5340'
  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 RRXA11414Fitting · corrodedDURING A MAINTENANCE VISIT FOUND STA 70 RBL 55 L27R HAS TIE FITTING CORRODED I/B FLANG BROKEN OFF. REMOVED DAMAGED PART FABRICATED REPLACEMENT PART AND INSTALLED ON NR 85752 IAW SRM 51-1-21 AND 51-1-20D AND DWG G37571.00Jul 15, 2001 · N873SJ · Doug DC873FSDR RRXA11409Fitting · corrodedDURING A MAINTENANCE VISIT FOUND C PIT BACK UP FITTING FOR #6 LWR T LATCH CORRODED STA 1232 BETWEEN L33R I/B AND L33R O/B. REMOVED CORROSION IAW DC8 SRM 51-1-8 MATERIAL LOSS OUT OF LIMITS IAW SRM 53-20 FIG F. REMOVED AND REPLACED BACK UP FITTING AND CLIS REFJul 13, 2001 · N873SJ · Doug DC873FSDR RRXA11407Fitting · corrodedDURING A MAINTENANCE VISIT FOUND C-PIT BACK UP FITTING FOR NR 4 LWR T LATCH CORRODED AROUND FASTENERS STA 1215 BETWEEN L33R I/B AND L33R O/B. REMOVED CORROSION FOUND TO BE OUT OF LIMITSA. SRM 51-1-8 AND 53-2-01F. RECEIVED BACK UP FITTING AND CLIP PER SRM 51Jul 13, 2001 · N873SJ · Doug DC873FSDR RRXA11405Fitting · corrodedDURING A MAINTENANCE VISIT FOUND C-PIT BACK UP FITTING HAS CORROSION OUT OF LIMITS AT STA 1206 L33R. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.Jul 10, 2001 · N873SJ · Doug DC873FSDR RRXA11391Fitting · misdrilledDURING A MAINTENANCE VISIT FOUND C-PIT FITTING FWD SIDE OF FRAME 1160 L35L IS MISDRILLED IN AFT UPPER RADIUS. REMOVED AND REPLACED FITTING IAW SRM 51-1-20DJul 2, 2001 · N873SJ · Doug DC873FSDR RRXA11387Doubler · crackedDURING A MAINTENANCE VISIT FOUND FUSELAGE EXT SKIN FWD UPPER CORNER OF R/H FWD SERVICE DOOR JAMB IS CRACKED 4 FASTENERS STA 160 L11R - L12R. *** CORRECTIVE ACTION *** REMOVED DAMAGED AREA, FABRICATED REPLACEMENT PART AND INSTALLED IAW 53-2-0 FIG 14.Jun 30, 2001 · N873SJ · Doug DC873FSDR RRXA11376Fitting · corrodedDURING A MAINTENANCE VISIT FOUND C PI BATH TUB FITTING STA 1180 L33R - L34R HAS LITE CORROSION. REMOVED BATH TUB IAW SRM 51-1-20D. REMOVED CORROSION, TREATED AND PRIMED IAW SRM 51-1-8 AND 53-2-0 FIG 1F. INSTALLED REPLACEMENT PARTS IAW SRM51-1-20 AND DWG 375Jun 26, 2001 · N873SJ · Doug DC873FSDR CALA0100593Fitting · corrodedINSPECTION FOUND ATTACH FITTING(FORWARD OF L-2 DOOR) CORRODED AT FS 1136, LBL 56. THE FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 51-30-1, 51-30-4, AND 51-10-3.Jun 24, 2001 · N16813 · Doug DC982SDR RRXA11370Fitting · corrodedDURING A MAINTENANCE VISIT FOUND C PIT BATH TUB FITTING AT STA 1160 L33R I/B TO 33R O/B HAS HEAVY CORROSION. REMOVED BATH TUB FITTING PER SRM 51-1-20D, REMOVED CORROSION ON BATH TUB FITTING MOUNT POINT. THICKNESS PER NDI SPM 04.00.06 FOUND TO BE WITHIN LIMITJun 23, 2001 · N873SJ · Doug DC873FSDR RRXA11317Fitting · damagedDURING A MAINTENANCE VISIT FOUND ELONGATION DAMAGE TO A-PIT CROSS SLIDE TORQUE BOX BATH TUB FITTING HOLES AT STA.320 AND L29L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRJun 21, 2001 · N606AL · Doug DC873FSDR 0104369927Fitting · crackedDuring Hck at the ATL Maintenance. The LHS MLG door hinge fitting AFT lug was found cracked. Material 7075-t6511, repaired per EA 99-181272Jun 11, 2001 · N8920E · Doug DC931SDR CA010724032Fitting · corroded(CAN) THE FITTING WAS FOUND CORRODED ON 1200 HOUR INSPECTION AND NEW PART 206-033-173-001 WAS INSTALLED. THE ORIGINAL PART IS MANUFACTURED FROM MAGNESIUM WHERE THE NEW PART IS ALUMINUM SO AFTER 13109 OF FLYING ON A AIRCRAFT MANUFACTURED IN 1978 THIS WOULD NOTJun 7, 2001 · Bell 206LSDR RRXA11229Fitting · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO FITTING AT STA.1230 AND L33R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D.Jun 5, 2001 · N606AL · Doug DC873FSDR USAA010685Attach Angle · crackedPIT - FOUND ATTACH ANGLE CRACKED .75 INCH, RIGHT UPPER PYLON ATTACH ANGLE CANTED STATION 1464. STOP DRILLED CRACK PER TYPICAL REPAIR 54-10-06A. (M)Jun 5, 2001 · N829US · Doug DC982SDR RRXA11152Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO BATHTUB FITTING AT STA.540 AND L34L-L35L, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-0 FIG2D, 51-1-20D.May 9, 2001 · N996CF · Doug DC862FSDR RRXA11126Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FWD CARGO PIT CROSS SLIDE DOOR JAMB BACK UP FITTING NR 1 LWR TEE BOLT, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 5Apr 30, 2001 · N996CF · Doug DC862FSDR RRXA11107Fitting · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO L/H SPLICE FITTING AT STA.605-615 AND L31L, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-3-0, 51-1-20D.Apr 27, 2001 · N996CF · Doug DC862FSDR RRXA11088Fitting · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO LONGERON END FITTING AT STA 1530-1540 AND L30R, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 51-1-20D, DWG#464132Apr 21, 2001 · N996CF · Doug DC862FSDR RRXA11084Fitting · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO AFT LONGERON END FITTING AT STA. 1530 AND L28L, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 51-1-20D.Apr 20, 2001 · N996CF · Doug DC862FSDR RRXA11077Fitting · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO END FITTING AT STA 1520-1530 AND L32L, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D AND DWG 4641326.Apr 18, 2001 · N996CF · Doug DC862FSDR RRXA11076Fitting · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO LONG END FITTING AT STA. 1530-1540 AND L32R, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-3-0 AND DWG 4641324.Apr 15, 2001 · N996CF · Doug DC862FSDR RRXA10980Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO C-PIT DOOR FRAME LWR NR 3 LATCH, BACKUP FITTING, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-20D, 53-1-0, AND DWGApr 14, 2001 · N602AL · Doug DC873FSDR RRXA10963Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE BATHTUB FITTING AT STA 1180 BETWEEN L35L & L34R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 53-1-01, 51-1-20D Apr 12, 2001 · N602AL · Doug DC873FSDR RRXA10947Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE BATHTUB FITTING AT STA 1160 TO 1220 AND L34R TO L33R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-21 AND 53Apr 11, 2001 · N602AL · Doug DC873FSDR RRXA11140Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON END FITTING AT STA.1525 AND L33L, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 53-2-5 FIG8C-1.Apr 10, 2001 · N996CF · Doug DC862FSDR RRXA10926Fitting · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE BATHTUB FITTING ON FWD SIDE OF STA 340 BETWEEN L34R-35R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. RECEIVED PART AND INSTALLED IAW DC-8 SRM 53-2-0, FIG 2D AND 51-1-20D.Apr 6, 2001 · N602AL · Doug DC873FSDR UPS01835583Fitting · crackedINSPECTION TYPE: C2, MAIN CABIN STA 780 RT SIDE, BY SEAT TRACK H BEAM FITTING. SUPPORT CRACKED. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20 51-1-24 AND 51-3-0Apr 3, 2001 · N805UP · Doug DC873FSDR UPS01835581Fitting · corrodedINSPECTION TYPE: C2, MLG WW PRESSURE DECK STIFFENER STA 960 LBL 48 HAS POPPED RIVETS AND CORROSION COMING FROM UNDERNEATH. REMOVED & REPLACED FITTING IAW DAC DWG 3640087 AND DC8 SRM 51-1-21 AND 5 1-1-20DApr 3, 2001 · N805UP · Doug DC873FSDR UPS01835769Fitting · crackedINSPECTION TYPE:C2,3 STA. 390 LONG. 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING I.A.W. DWG. 3754473-1N,AND SRM. 51-1-20DMar 30, 2001 · N797UP · Doug DC871FSDR UPS01835596Fitting · crackedINSPECTION TYPE:C2,3 STA. 1240, LONG. 35L INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING I.A.W. DWG.3758495,AND SRM. 51-1-20DMar 28, 2001 · N797UP · Doug DC871FSDR UPS01835648Fitting · crackedINSPECTION TYPE:C2,3 STA. 280 BANANA FITTING IS CRACKED AT LONG. 33R REMOVED AND REPLACED FITTING I.A.W. DWG.3755827,AND SRM. 51-1-20DMar 27, 2001 · N797UP · Doug DC871FSDR 2001UALA00335Fitting · crackedFORWARD GALLEY DOOR FRAME AT THE FOURTH FITTING FROM THE BOTTOM ON THE AFT SIDE IS CRACKED. REPAIRED THE FORWARD GALLEY DOOR FRAME. MAJOR REPAIR ACCOMPLISHED.Mar 27, 2001 · N310UA · Boeing 737322SDR RRXA10896Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE BATHTUB FITTING AT STA 1160 L29L TO L30L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-20D, 53-1-Mar 25, 2001 · N602AL · Doug DC873FSDR RRXA10894Fitting · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE TORQUE BOX BANANA FITTING AT STA 1150 L31R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-20D AND 53-1-0.Mar 25, 2001 · N602AL · Doug DC873FSDR RRXA10890Fitting · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE SPLICE FITTING AT LONGERON 35R AT STA 1050, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-20D, 51-3-0, 53-1-0 AND DWG 370545.Mar 25, 2001 · N602AL · Doug DC873FSDR RRXA10901Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE BATHTUB FITTING AT STA 1220 BETWEEN L34R TO L35R AND L35R TO L36R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAWMar 22, 2001 · N602AL · Doug DC873FSDR RRXA10883Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE C-PIT DOOR FRAME NR 2 LATCH BACKUP FITTING, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-20D, 53-1Mar 22, 2001 · N602AL · Doug DC873FSDR RRXA10882Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE C-PIT DOOR FRAME NR 5 LATCH BACKUP, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-20D, 53-1-0 AND Mar 22, 2001 · N602AL · Doug DC873FSDR RRXA10881Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE C-PIT DOOR FRAME LOWER NR 4 LATCH BACKUP FITTING , DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 53-1-0Mar 22, 2001 · N602AL · Doug DC873FSDR EIA2001124Fitting · crackedMZJ-EAC - FOUND FS 660 RBL 117 WL 199 FLOORBEAM FITTING HAS .250 DIAMETER HOLE BROKEN OUT OF EDGE OF UPT T-CAP AFT FLANGE. REPAIRED FITTING PER ECRA 3203-53-20-2. (M)Mar 21, 2001 · N3203Y · Boeing 747128SDR RRXA10874Fitting · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE BATHTUB FITTING AT STA 300 BETWEEN L34R TO L35R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. RECEIVED PART AND INSTALLED IAAW DC-8 SRM 53-2-0, FIG 2B.Mar 20, 2001 · N602AL · Doug DC873FSDR DHL2001806512Fitting · crackedFWD. CARGO COMPARTMENT - FITTING CRACKED 3 INCH BETWEEN STA. 440.000 AND STA. 460.000. L-31L REMOVED CRACKED FITTING FROM FWD CARGO COMPT. STA. 440-460 L-31L IAW SRM 51-1-20D PAGE 21 CLEANED, TREATED, AND PRIMED IAW SRM 51-1-8 PAGE 12-15 INSTALLED NEW FITTINMar 17, 2001 · N806DH · Doug DC873FSDR DHL2001806513Fitting · crackedFWD CARGO COMPARTMENT - FITTING CRACKED 6 INCHES BETWEEN STA 600.000 AND STA 620.000. L-31R. REMOVED CRACKED FITTING (FWD CARGO COMPT STA 600-620, L-31R) IAW SRM 51-1-20D PAGE 21. CLEANED, TREATED, AND PRIMED AREA IAW SRM 51-1-8 PAGE 12-13. INSTALLED FITTIMar 16, 2001 · N806DH · Doug DC873FSDR IXXA0100041SIntercostal · corrodedDURING ROUTINE C CHECK INSPECTION, CORROSION WAS DETECTED ON INTERCOSTAL AT FUSELAGE STATION 8 LONGERON 35 RIGHT. REPAIR ACCOMPLISHED REMOVAL OF INTERCOSTAL, FABRICATION AND INSTALLATION AN NEW INTERCOSTAL IN ACCORDANCE WITH DOUGLAS DRAWING 5615530 AND ENINEERMar 15, 2001 · N820BX · Doug DC871FSDR CA010403003Beam · cracked(CAN) DURING C-CHECK A CRACK WAS FOUND IN THE ENGINE SUPPORT BEAM LOWER WEB BETWEEN FS 625.30 AND FS 640.00 NEAR LBL 36.20. THE CRACK WAS LOCATED IN THE CORNER OF ACCESS PANEL (P/N 601-35006-39) LANDING AND ENDED NEAR THE PANEL EDGE.Mar 13, 2001 · Cndair CL6002B19SDR RRXA10742Fitting · gougedDURING A MAINTENANCE VISIT FOUND GOUGING DAMAGE TO RT. CANOE FITTING TOP FWD 3 INCHES AT RT. STA 340, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O. #01-024 WITH APPROVED 811Mar 12, 2001 · N8091U · Doug DC871FSDR UPS01435344Fitting · crackedINSPECTION TYPE:C6, CRACK REVEALED AT BS 1265 LT NR 2 STOP FITTING AND FRAME INNER CHORD ATTACH HOLE APPROX .1875 INCH LONG. STOP FITTING REPLACED AS PER SRM 51-10-01.Mar 4, 2001 · N683UP · Boeing 747121SDR UPS01435343Fitting · crackedINSPECTION TYPE:C6, CRACK AT BS 1265 RT NR 2 STOP AND FRAME INNER CHORD ATT FASTENER HOLE, APPROX .25 INCH LONG RUNNING I/B NR 2 STOP FITTING. REMOVED AND REPLACED PER SRM 51-10-01.Mar 4, 2001 · N683UP · Boeing 747121SDR AWXA0001382Bracket · crackedLT FUSELAGE UNDER WING TO BODY FAIRING FWD OF EMERGENCY EXIT HAS CRACKED ATTACH BRACKET. FABED REPAIR ANGLE, REMOVED DAMAGED ANGLE AND INSTALLED REPAIR ANGLE IAW SRM 51-40-02 AND 51-70-11.Feb 20, 2001 · N908AW · Boeing 7572G7SDR UPS01235208Bracket · crackedINSPECTION TYPE:C-CK, TAIL SKID COMPT, 2 UPPER SUPPORT RODS AFT ATTACH BRACKETS, LT AND RT CRACKED. REMOVED AND REPLACED BOTH LT AND RT ATTACH BRACKETS FOR TAIL SKID UPPER SUPPORT RODS.Feb 13, 2001 · N904UP · Boeing 72751C
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