JASC 5342
Service difficulty reports · 578
Reports filed under 5342 · Fuselage, Stabilizer 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 = '5342' 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 = '5342' 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 IXXA05SMN10SFitting · crackedDURING ROUTINE C-CHECK INSPECTION, LT HORIZONTAL STABILIZER FITTING CRACKED 1 IN., XFS 47.000 - XFS 60.000 (LWR PART). REMOVED CRACKED FITTING IAW DC-8 SRM 51-1-20D PAGE 21. CLEANED, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8B. INSTALLED NEW FITTING IAW DC-SDR DHL2004873552Angle · corrodedAFT FUSELAGE ATTACH ANGLE WITH VERTICAL STABILIZER CORRODED (BETWEEN FRONT SPAR AND CTR SPAR RT SIDE). PERFORMED MAJOR REPAIR. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 55-2-0 PG 12. TRIMMED OUT CORRODED AREA IAW SRM 53-2-5 FIGSDR DL73S041044Attach Fitting · corrodedBODY CLEVIS LUGS FOR VERTICAL STABILIZER ATTACH FITTINGS CORRODED. REPAIRIED IAW ERA 095009-14.SDR AWXA200401164Angle · corrodedDURING C-18 CHECK CORROSION WAS FOUND ON HORIZONTAL WEB ATTACH ANGLE AT BS 294, LBL 4, WL 208. MAINTENANCE CUTOUT DAMAGED SECTION OF FLOORBEAM UPPER TEE CAP AT BS 294, FROM LBL 25 TO RBL 55; FABRICATED A NEW REPLACEMENT SECTION OF BEAM AND 2 EACH REPAIR ANGLESSDR AWXA200401163Angle · corrodedDURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON HORIZONTAL WEB ATTACH ANGLE AT BS 294, RBL 55, WL 208. MAINTENANCE REMOVED CORRODED HORIZONTAL WEB ATTACH ANGLE AT BS 294, RBL 55; FABRICATED A NEW REPLACEMENT ANGLE IAW DWG 69-37402; INSTALLED REPAIR PARTSDR USAA040651Fitting · crackedPIT - FOUND CORNER FITTING CRACKED 5 INCHES, RIGHT TOP CORNER FITTING INSIDE HORIZ STAB INTERSECTING, PRIMARY AND THRUST BEAM. REPLACED ANGLE PER SRM 51-40-02. (M)SDR USAA040563Strap · crackedCLT - FOUND STABILIZER STRAP CRACKED .5 INCH, LOWER CHORD STATION 1280 RBL 24. REPAIRED PER SRM 53-10-51 FIG 202 DETAIL IV. (M)SDR 0401279997Angle · crackedDURING M-CHECK FOUND CRACK IN VERTICAL STABILIZER ATTACH ANGLE AT BS 1095. REPAIRED PER EA 99-195833.SDR CALA0400432Fitting · corrodedVERTICAL STABILIZER AFT LEFT ATTACH LUG, AFT FAILSAFE FITTING CORRODED. INSTALLED NEW FITTING PER SRM 51-40-02 & 51-40-03.SDR CALA0400431Fitting · corrodedVERTICAL STABILIZER AFT ATTACH LUG, FWD FAILSAFE FITTING CORRODED. INSTALLED NEW FITTING PER SRM 51-40-02 & 51-40-03.SDR CALA0400349Fitting · corrodedINSPECTION FOUND VERTICAL STABILIZER O/B AFT FUSELAGE FITTING CORRODED AT AFT BOTTOM SIDE OF HOLE CUTOUT, RIGHT AFT CLEVIS, STA 1088. REPAIRED IAW ECRA 5342-01021.SDR SROM200400017Attach Fitting · gougedDURING D CHECK INSPECTION FOUND LT HORZ. STAB T/E I/B ATTACH FITTING HAS SMALL GOUGES. BLENDED AREA, REMOVED DAMAGE, FLAP PEENED, TREATED AND PRIMED IAW ASA EA 5510-01186 AND AAR EA 10289.SDR CALA0300700Angle · crackedINSPECTION FOUND A 2.75 INCH CRACK IN LT VERTICAL STABILIZER ATTACH ANGLE AT STA 1474. A REPAIR ANGLE WAS INSTALLED IAW SRM 53-05, FIGURE 23B.SDR CALA0300651Attach Angle · gougedINSPECTION FOUND ATTACH ANGLE ON LT SIDE OF VERTICAL STABILIZER ON FUSELAGE EXTERIOR AT STA 1121 GOUGED. A NEW ANGLE WAS INSTALLED IAW ECRA 5380-01013.SDR ABXA030432Attach Angle · crackedVERTICAL STABILIZER LEFT ATTACH ANGLE WAS CRACKED AT 99. REPLACED LEFT VERTICAL STABILIZER ATTACH ANGLE IAW DC-9 SRM 53-05.SDR CALA0300476Angle · gougedINSPECTION FOUND LT VERTICAL STABILIZER PANEL ATTACH ANGLE GOUGED AT STA 1065-1085 JUST BELOW VERTICAL STAB ON LT SIDE JUST FORWARD OF RUDDER. THE ATTACH ANGLE WAS REMOVED AND REPLACED IAW ECRA 55380-01013.SDR DL73S030688Attach Fitting · corrodedDURING ACCOMPLISHMENT OF INSPECTIONS IAW SB 737-55-1028 (DAL EO 3-85220-3), CORROSION WAS FOUND ON FIVE (5) VERT STABILIZER CLEVIS LUGS AND THREE (3) VERT STABILILZER ATTACH LUGS. THE BORES WERE OVERSIZED AND THE LUG FACES MACHINED TO REMOVE CORROSION. O/S BSDR GTIA030343Attach Angle · crackedLEFT DORSAL FIN VERTICAL ATTACH ANGLE HAS CRACK IN VERTICAL LEG. REMOVED LEFT DORSAL FIN VERTICAL ATTACH ANGLE. LOCATED AND DRILLED NEW DORSAL FIN VERTICAL ANGLE. INSTALLED LEFT DORSAL FIN OUTSIDE ATTACH ANGLE. (M)SDR GTIA030342Angle · crackedRIGHT DORSAL FIN VERTICAL ATTACH ANGLE HAS CRACKING VERTICAL LEG. ALSO, DOUBLER ATTACHMENT IS OUT OF LIMITS. REMOVED RIGHT DORSAL FIN VERTICAL ATTACH ANGLE. REMOVED DOUBLER ATTACHMENT. FABRICATED NEW DOUBLER ATTACHMENT. FABRICATED NEW GUSSET. LOCATED AND SDR DLM88030427Angle · crackedTHE RT FUSELAGE TO VERTICAL STABILIZER ATTACH ANGLE WAS FOUND WITH A CRACK NEAR CANTED FS 1474. THE CRACK WAS REMOVED WITH A TRIMOUT TO THE HORIZONTAL FLANGE OF THE ANGLE. THE AREA WAS REPAIRED WITH A STEEL REPAIR ANGLE PER ER/A 384977-14, REV A.SDR CA030306003Spar · cracked(CAN) INSPECTION CARRIED OUT AS PER SB 2/47 REV 'D' AD CF-91-42.TAILPLANE SPAR FOUND CRACKED LT AND RT SIDE TOP UNDER PICK-UP BRACKETS C2TP159 AND C2TP160. MODS 2/436, 2/466 AND 2/758 HAD ALREADY BEEN INCORPORATED.AIRCRAFT TTSN 19969.4 HOURS.SDR DL733030147Fitting · corrodedCORROSION WAS FOUND IN THE BORES OF BOTH THE LT AND RT PRIMARY FORWARD CLEVIS LUGS. THE LHS PRIMARY FORWARD CLEVIS LUG WAS OVERSIZED TO A DIAMETER OF 1.440 INCH TO REMOVE THE CORROSION. THE RHS PRIMARY FORWARD CLEVIS LUG WAS OVERSIZED TO A DIAMETER OF 1.408 SDR AALA20030099Attach Angle · crackedTUL - FOUND LEFT AFT END OF VERTICAL STAB JOINT IS CRACKED BETWEEN FASTENERS .5 INCH. INSTALLED SKATE ANGLE REPAIR DOUBLER PER AARD 53-10-00-2. (M)SDR DLM88030071Angle · crackedFUSELAGE / VERTICAL STAB TO FUSELAGE ATTACH ANGLE : CRACK REPAIR THE LH VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE WAS FOUND CRACKED IN THE HORIZONTAL FLANGE AT CANT STA 1474. THE CRACK WAS ROUTEDSDR AALA20021836Attach Angle · crackedTUL - FOUND FUSE TO VERTICAL STABILIZER ATTACH ANGLE CRACKED IN RADIUS STATION 1463 RIGHT SIDE AND CRACKED IN LOWER LEG BETWEEN FASTENERS. STOP DRILLED CRACK IN RADIUS AND CUTOUT CRACKED AREA BETWEEN FASTENERS AND INSTALLED DOUBLER AND FILLER PER AARD 53-10-0SDR GTIA021283Attach Angle · puncturedFTW - FOUND DORSAL FIN, RIGHT OUTBOARD (TWO) ATTACH ANGLE PUNCTURED. REMOVED TWO RIGHT OUTBOARD ATTACH ANGLE. LOCATED AND DRILLED TWO ATTACH ANGLES, INSTALLED. (M)SDR DL733021367Fitting · corrodedCORROSION WAS FOUND IN THE LUB BORE OF THE LHS FORWARD CLEVIS LUG. THE LUG BORE WAS OVERSIZED TO 1.4385" AND AN OVERSIZED BUSHING WAS INSTALLED. THE DAMAGE WAS FOUND AT HMV.SDR GTIA021261Attach Angle · crackedFTW - FOUND DORSAL FIN INBOARD LEFT, RIGHT ANGLE ATTACH IS CRACKED. REMOVED LEFT AND RIGHT FIN INBOARD ATTACH ANGLES. LOCATED AND DRILLED LEFT INBOARD FIN ANGLE. LOCATED AND DRILLED LEFT OUTBOARD ATTACH ANGLE. LOCATED AND DRILLED RIGHT INBOARD FIN ANGLE ANSDR ASAA0240203Angle · gougedPAE - DURING SI CHECKED, FOUND VERTICAL STABILIZER RIGHT SKATE ANGLE GOUGED. REPAIRED IAW SRM. (M)SDR ASAA0240190Angle · wornDURING SI CHECKED, FOUND VERTICAL STABILIZER SKATE ANGLE WORN. REPAIRED IAW SRM. (M)SDR AALA20021616Attach Angle · crackedTUL - FOUND VERTICAL STABILIZER TO FUSELAGE RIGHT ATTACH ANGLE CRACKED, AT AFT END. CUT OUT DAMAGED SECTION OF SKATE ANGLE. INSTALLED FILLER AN DOUBLER REPAIR PER AARD 53-10-00-2. (M)SDR CA021108005Bolt · loose(CAN) AT C02 CHECK FOUND THIS MAIN HINGE FITTING Y-BOLT O/B BEARING MIGRATED BY .0130 INCH AT REAR SPAR ATTACHMENT BOLT REPLACED BY NEW BOLT AT AC 11,599 HRS, 2,322 CYCLSDR GTIA021202Attach Angle · crackedFTW - FOUND VERTICAL STABILIZER RIGHT AND LEFT LOWER LEADING EDGE SKIN ATTACH ANGLES TO FUSELAGE, APPROX FS 1437, CRACKED. REMOVED RIGHT AND LEFT SKIN ATTACH ANGLES. LOCATED AND DRILLED LEFT ANGLE. LOCATED AND DRILLED RIGHT ANGLE. INSTALLED TWO NEW ANGLE. SDR AWXA200201069Angle · chafedMCN - MAJOR REPAIR - DURING C-18 CHECK THE L/H VERTICAL STABILIZER TO FUSELAGE "L" ANGLE WAS FOUND CHAFED AND WORN BS 1016 - BS 1126. MAINTENANCE REMOVED THE L/H VERTICAL STABILIZER TO FUSELAGE "L" ANGLE BS 1016 - BS 1126; FABRICATED A NEW REPLACEMENT ANGLE; ASDR LR7A02080Angle · crackedDURING SCHEDULED C4 INSPECTION PER HST5505 FOUND HORIZONTAL STABILIZER UPPER FWD SPAR CAP TO INTERNAL BULKHEAD ATTACHMENT ANGLE CRACKED. FS1041, LBL20, WL285.REPLACED ANGLE IAW SRM SMP 583-51-60, AND 51-70. NR0070.SDR AALA20021397Attach Angle · crackedTUL - FOUND RIGHT VERTICAL STAB ATTACH ANGLE CRACKED AT CANT STATION 1463. INSTALLED DOUBLER PER AARD 53-10-00-2 PAGE 1 REPAIR 2. (M)SDR AUS20021008Fitting · cracked(AUS) FORWARD FIN ATTACHMENT FITTING CRACKED IN AREA ADJACENT TO THE LH BOLT HOLE. FOUND DURING INSPECTION IAW AD/C206/7A4.SDR CA020731005Fitting · loose(CAN) DURING HUMP INSPECTION THE FOLLOWING DISCREPANCY WERE FOUND. THE HORIZONTAL STAB CENTER HINGE FITTING HAD LOOSE AND MISSING RIVETS. A TOTAL OF 14 RIVETS WERE AFFECTED AND CONSEQUENTLY REPLACED BY HI-LOK AS PER STRUCTURAL REPAIR MANUAL.SDR AUS20020751Bracket · cracked(AUS) STEEL BRACKET ASSEMBLY CRACKED IN TWO PLACES. ONE CRACK LOCATED AT WELD SEAM AND ONE CRACK IN AREA OF ANCHOR NUT ATTACHMENT.BRACKET ATTACHES VERTICAL FIN TO TAILPLANE AND TAILPLANE TO FUSELAGE.SDR MWEA020410Attach Angle · crackedA .5 INCH CRACK IN RIGHT SIDE VERTICAL TO FUSELAGE ATTACH ANGLE AT STATION 1130, APPROXIMATELY 1 FOOT FORWARD OF RUDDER TORQUE TUBE. FABRICATED AND INSTALLED SPLICE, STRAP AND FILTER.SDR GTIA020645Attach Angle · crackedFTW - FOUND RIGHT DORSAL FIN ATTACH ANGLE HAS CRACK (HORIZONTAL) AT FS Y1160, 2 INCHES AND .75 INCHES LONG. STOPPED DRILLED CRACK. FABRICATED AND FORMED REPAIR ANGLES. INSTALLED REPAIR ANGLES TO RIGHT DORSAL FIN ATTACH FS Y1160. (M)SDR ASAA0210146Fitting · corrodedPAE - DURING SCHEDULED C-CHECK, FOUND SPAR LUGS AT BS 1104, LEFT BUTTOCK LINE 45, RIGHT BUTTOCK LINE 45 CORRODED. REPAIRED REAR SPAR LUGS PER EA. (M)SDR CA020904001Spar · cracked(CAN) UPON REMOVAL OF BRACKET TO GAIN ACCESS TO NUT PLATES DISCOVERED THE REINFORCEMENT AND RT SPAR CRACKED ALONG BEND RADIUS UNDER THE BRACKET. CRACKS COULD NOT BE SEEN UNTIL BRACKET WAS REMOVED.SDR AUS20020340Bracket · cracked(AUS) LH REAR HORIZONTAL STABILISER ATTACHMENT BRACKET CRACKED.SDR AUS20020259Mount · corroded(AUS) STABILATOR MOUNTING BLOCK RIVETS SHEARED. INVESTIGATION FOUND THE UNDERSIDE OF THE ATTACHMENT BLOCK BADLY CORRODED AND THE RIVETS CORRODED.SDR CALA0200022Attach Angle · wornINSPECTION FOUND ATTACH ANGLE ON BOTTOM OF VERTICAL STABILIZER ON R/H SIDE WORN THIN AT STA 1104-1121. THE ATTACH ANGLE WAS REPLACED IAW ECRA 5300-01013, REV B.SDR AALA20020023Attach Angle · crackedTUL - FOUND TWO HILOCK HEADS DISHED, ATTACH ANGLE CRACKED FROM HOLE TO HOLE PLUS .125 INCH FORWARD. INSTALLED VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE PER AARD 53-10-00-2. REPLACED 2 DISHED HILOCKS AND LEFT SIDE. (M)SDR AALA20020024Attach Angle · crackedTUL - FOUND 1 HI-LOCK DISHED, ATTACH ANGLE CRACKED FROM HOLE TO HOLE AND AFT PLUS 6 INCHES. REMOVED AND REPLACED CRACKED HI-LOCK. INSTALLED DOUBLER PER AARD 53-10-00-2 ON RIGHT SIDE. (M)SDR UPS02837428Angle · crackedINSPECTION TYPE:C2 STATION 1766 AT LONG 2L FUSELAGE TO VERTICAL STAB ANGLE IS CRACKED AND CORRODED. FABRICATED AND INSTALLED REPAIR IAW SRM 53-2-5 FIG 16A.SDR AUS20011341Bolt · broken(AUS) STABILISER ATTACHMENT FITTING BOLTS BENT (2OFF) AND BROKEN(2OFF). INVESTIGATION FOUND THAT THE BOLTS WERE THE INCORRECT TYPE. THE PART NUMBER OF THE INCORRECT BOLTS WAS PNO NAS425-3-7.UNAPPROVED PART. PERSONNEL/MAINTENANCE ERROR.
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