JASC 5500
Service difficulty reports · 490
Reports filed under 5500 · Empennage 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 = '5500' 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 = '5500' 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 2005FA0000837Plate · crackedPART FOUND TO BE CRACKED FROM BOTH REAR CORNER EXTENDING 2 INCHES IN LENGTH. PART HAS 9702 HOURS. STA 398-414. (K)SDR DHL2005784511Skin · dentedEMPENNAGE SKIN CREASED BS 1243 AT STR.24R DAMAGED AREA FOUND TO BE OUT OF LIMITS IAW B727 SRM 53-30-1 FIG 1. WITH NO DEFECTS NOTED TO STRINGER. REPAIED IAW B727 SRM 51-10-2 AND 53-30-3 FIG 3.SDR 2005FA0000348Bracket · inoperative(1) RIVET SHEARED AND BRACKET ROTATED, PARTIALLY. THIS WAS CAUSED BY FLAP CABLES BEING RIGGED TOO TIGHT. THIS CAUSED A TWIST IN THE CABLES ALLOWING (1) CABLE TO RIDE UP AND OVER THE OTHER CAUSING IT TO COME OFF AN210-2A PULLEY. THE PILOT REPORTED GREAT DIFFSDR DHL2005782556Rib · gougedRT NR 5 BALANCE PANEL I/B RIB GOUGED. REMOVED RT NR 5 BALANCE BAY I/B SEAT PLATED FOR ACCESS IAW 727 SRM 51-30-2. EVALUATED DAMAGED TO BE OUT OF LIMITS IAW SRM 55-10-1 FIG 1. REMOVED RT NR 5 BALANCE PANEL I/B RIB IAW B727 SRM 51-30-2 AND INSTALLED NEW RIB SDR 04FDEA03184Panel · crackedDURING AIRPLANE'S CONVERSION FROM P-F/ACF FOUND BY ULTRASONIC INSPECTION 1 PANEL P/N ALC7438-2 (19 POSITION) CRACKED. REPLACED PANEL PER SB 55-16 FIG 20 GROUP 1 (KIT SB10550016-57).SDR 04FDEA01862Skin Panel · damagedPERFORMING REPAIR PROVIDED BY SB 55-16, INTERESTED PANEL HAS BEEN CUT OVER THE LAYOUT TRIM LINE REQUIRED. DAMAGED SKIN PANEL PORTION REPLACED AND SPLICED TO EXISTING SKINS IAW FEDEX EA 8-2740-75698 (REF FEDEX NRC N0747, N0940).SDR ASAA0480057Tab · dentedOKC - DURING 15K CHECK, FOUND LEFT ANTI-FLOAT TAB UPPER SURFACE IS DENTED. APPLIED FILLER PER SRM 55-04. (M)SDR AUS20031321Structure · corroded(AUS) STABILIZER STRUCTURE CORRODED.SDR 2003FA0001197Support Bracket · crackedSUPPORT BRACKET WAS FOUND TO HAVE A CRACK IN THE WELD WHILE INSPECTING NUTPLATES IAW AD. CRACK WAS LOCATED JUST FORWARD OF NUTPLATE INSIDE BRACKET ABOUT .7500 INCH LONG. WITH DYE PENETRANT INSPECTION, DYE PENETRATED COMPLETELY THROUGH WELD TO OUTSIDE BRACKETSDR ASOA03429Angle · crackedDURING A C-CHECK IN MCN, THE VERTICAL STABILIZER RIGHT VISOR PANEL ANGLE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE VERTICAL STABILIZER RIGHT VISOR PANEL ANGLE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)SDR TSAA0255265Skin · dentedCUT OUT DAMAGED AREA. FABRICATED REPAIR .063 DOUBLER AND .040 FILLER FROM 2024 T3 CLAD. INSTALLED REPAIR PARTS AND FASTENERS WET WITH MBS 5-95 SEALANT. REPAIR COMPLETED IAW SRM 55-10-1 FIGURE 2. AIRCRAFT RETURNED TO SERVICE. (M)SDR 2003FA0001199Fitting · crackedDISCOVERED CRACKS DURING ROUTINE INSPECTION. AD 58-01-06 HAD BEEN COMPLIED WITH BY REPLACEMENT OF PN 1709303.SDR USAA030197Balance Arm · damagedFOUND RUDDER BALANCE ARM HAS HOLE 1.25 INCH BY .75 INCH, UPPER SURFACE. ROUTED OUT DAMAGE AND INSTALLED DOUBELR PER EA 76691. (M)SDR SIMA200319002Elevator · damagedCLT - FLT 4430 - DURNG TAKEOFF ROLL AT ABOUT 60 KNTS CREW NOTED YOKES BEING SLAMMED TOWARDS THEM. CREW ABORTED TAKEOFF AND RETURNED TO GATE SAFELY. DURING POST FLIGHT NOTED LEFT ELEVATOR TRIM STUCK DOWN IN THE 90 DEGREE POSITION. MAINTENANCE REMOVED AND RESDR QXEA200300657Structure · crackedCKB - RIGHT LUNCHBOX CRACKED AT NR 10 FITTING AT FS 1070 1088. REPAIRED IAW QX SUPP AND SRM 51-40-00, 51-40-15.SDR 2003FA0000607Arm · inoperativeWITH GUST LOCK INSTALLED BALANCE ARM LOCKED ON DOWN STOP WHILE A/C WAS TIED DOWN IN GUSTY WIND CONDITIONS.SDR ASAA0380355Fairing · crackedOAK - DURING 15K CHECK, FOUND RIGHT STABILIZER OUTBOARD LOWER HINGE FAIRING IS BENT AND CRACKED. REPLACED FAIRING PER SRM 51-30-1. (M)SDR JEM2003F00000Trim Tab · mismanufactured2 EACH NR 4 RIVETS WHICH HELP HOLD TRIM TAB HORN TO TRIM TAB, WERE MISSING, AND HOLES HAD NOT BEEN DRILLED FOR RIVETS.SDR UPS03840366Fitting · crackedINSPECTION TYPE: C2, EMPENNAGE LT FITTING CRACKED FROM LBL 2-LBL 8 SECOND J BEAM FROM BELLY SKIN. PERFORMED HFEC IAW NDT SPM 06-10-01. FOUND CRACK ON FITTING REMOVED FITTING TO FOM. LOCATED DRILLED DEBURRED AND INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D.SDR AUS20030371Spar Cap · corroded(AUS) RH STABILATOR LOWER SPAR CAP CORRODED.SDR EIA2003021Skin PanelImpact damage on R/H bottom of Horizontal Stab at STA 240, 30" from L/E. CORRECTIVE ACTION: Repaired damaged skin and Rib lower chord per B747 SRM 55-10-02, 55-10-03, 51-1002, 51-4--04, & ECRA 481-53-180-2SDR JIK2003F00000Spring · brokenELEVATOR BUNGEE SPRING WAS FOUND BROKEN ON PRE-FLIGHT. TOTAL TIME ON THE SPRING 677 HOURS. THIS SPRING IS REQUIRED TO BE REPLACED EVER 1000 HOURS, TIS, IAW AD. THIS IS FIRST FAILURE OF THE (PN 7105603) SPRING.SDR CA030120003Frame · cracked(CAN) CRACKS FOUND AT FUSELAGE FRAME RIVETS FOR VENTRAL FIN POSSIBLE REASON RIVET SPACING TO SMALL CRACKS AT RIVETS WHERE FRAME AND VENTRAL FIN JOIN.SDR 2003FA0000066Structure · crackedCRACK FOUND IN LOWER RT ATTACH BOLT HOLE FROM HOLE CENTER AT THE 2 O`CLOCK POSITION. FOUND DURING INSPECTION FOR AD. CRACK LENGTH .250 INCH.SDR EGR2003F00000Fitting · crackedFOUND SUPPORT FITTING CRACKED AT RT UPPER STABILIZER ATTACH POINT FLANGE. REPLACED SUPPORT FITTING WITH NEW PART.SDR DL72S021475Rib · crackedVERT. STAB RIB L/H ATTACH ANGLE CRACKED AT FIN STA 133.800 AND STR 9LEFT REPAIR PER M/M 55-30-000-8SDR C2XA02SH155Bracket · crackedSHV- DURING C CHECK PULLEY BRACKET INSIDE PANEL 325 LR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED AFFECTED BRACKET IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH151Rib · bentSHV DURING C CHECK RIB WAS FOUND BENT ON RUDDER NUMBER ONE AT LOWER SIDE OF UPPER CENTER HINGE BRACKET. MAINTENANCE REMOVED AND REPLACED AFFECTED RIB IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR AALA20021682Plate · corrodedFOUND CORROSION AND PITTING ON 8 HINGE LUG PLATES FOR HORIZONTAL STABILIZER PIVOT, STATION YV170. INSTALLED NEW HINGE PLATES FOR HORIZONTAL STABILIZER PIVOT PER KF0488. (M)SDR 2002FA0001284Spar · crackedMAIN SPAR OF TAILPLANE (STABILATOR) WAS FOUND TO CONTAIN MULTIPLE CRACKS IN WOOD STRUCTURE AFT MOUNTING HOLES. PLYWOOD FACE PLATES WERE DELAMINATED AND HIDING CRACKS. ALL ATTACHMENT HARDWARE WERE RUSTED. TAILPLANE WAS LOOSE WITH EXCESSIVE PLAY AFTER HARD LASDR VJ32002F00087Bulkhead · crackedDURING A PROGRESSIVE INSPECTION OF THE EMPENNAGE SECTION OF THIS AIRCRAFT A MECHANIC FOUND A CRACK IN THE RADIUS BEND AREA UPPER LEFT CORNER OF THE BULKHEAD.SDR VJ32002F00086Bulkhead · crackedDURING PROGRESSIVE INSPECTION OF THE EMPENNAGE SECTION OF THIS AIRCRAFT, A MECHANIC FOUND A CRACK IN THE RADIUS BEND AREA UPPER LEFT CORNER OF THE BULKHEAD.SDR C2XA02SH067Structure · damagedDURING C CHECK LT SPEED BRAKE OUTER TRAILING EDGE IS WRAPED. MAINTENANCE REMOVED AND REPLACED LT SPEED BRAKE. OPERATIONAL CHECK GOOD IAW EMB 145 AMM 27-63-01. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR CA021001004Bracket · cracked(CAN) IN THE PROCESS OF DOING A 3000 HOUR INSPECTION ON THE TAILBOOM LEFT HAND ELEVATOR, THE ENGINEER FOUND THE ELEVATOR ATTACHMENT LUG BRACKET CRACKED. THE CRACK WAS ON THE AFT SIDE ATTACHMENT LUG BRACKET B ELOW THE ATTACHMENT LUG, BETWEEN THE 1ST AND 2ND RISDR ABXA020144Skin · corrodedRIGHT HORIZONTAL STABILIZER, UPPER SKIN P/N 182T3200-2, AT STRINGER 3, RSS 42, WAS CORRODED OUT OF LIMITS. REPAIRED AREA IAW REA B655-43586-MR.SDR USAA020315Attach Angle · crackedPIT - FOUND ATTACH ANGLE CRACKED 6 INCHES IN RADIUS, RIGHT THRUST BEAM UPPER INBOARD ATTACH ANGLE. DEFECTIVE PART REPLACED WITH IDENT PART NR. (M)SDR SIMA200219110Support · crackedABI - FOUND PULLEY SUPPORT ANGLE IS CRACKED ON LEFT END BETWEEN VERTICAL SPARS 3 AND AUX SPAR 52 PERCENT AND BELOW ZV 3145.0 MM. (M)SDR SIMA200218102Spar · corrodedDURING MBV-1 INSPECTION, RIGHT HORIZONTAL STABILIZER AFT SPAR HAS AREA OF CORROSION. C/A: REPAIRED CORROSION IAW EO. AIRCRAFT RETURNED TO SERVICE.SDR AUS20020697Structure · corroded(AUS) BOTH HORIZONTAL STABILISER AND FIN CONTAINED EXTENSIVE SURFACECORROSION.SDR CA020606008Angle · cracked(CAN) DURING SCHEDULED MAINTENANCE, IT WAS DISCOVERED THAT THE ANGLE - TAILCONE REINFORCEMENT RT IN THE TAILCONE BULKHEAD ASSEMBLY WERE CRACKED. NEW PARTS 0712048-7 (LT) AND 0712048-6 (RT) WERE INSTALLED USING THE EXISTING RIVET SIZE AND PATTERN.SDR 2002UALA00539Rudder · delaminatedPREVIOUS REPAIR DELAM ON RUDDER TRAILING EDGE RS 245.00 SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.REMOVED DELAM REPAIR AND INSTALLED NEW REPAIR PLIES.SDR AALA20020444Spar · damagedAFW - FOUND SEVERAL SMALL HOLES RANGING .15 INCH DIAMETER TO .40 INCH DIAMETER THROUGH SURFACE PLIES AT FRONT SPAR. NO CORE DAMAGE. (M)SDR DL72W020207Stringer · crackedVERT. STAB R/H SIDE STRINGER CRACKED SIXTH FROM BOTTOM 3RD BAY DOWN REPAIR PER MM 55-30-000-8SDR C2XA02TY009Fitting · gougedTYS During a scheduled inspection the right hand horizontal stabilizer bearing forward fitting was found to have a internal gouge. Maintenance accomplished a blend-out repair including dye penetrant inspection IAW Embraer GST-0095/02. The repair was satisfSDR DL72S020020Skin · crackedFOUND ON E2 LETTER CK 3/8 INCH CRACK VERT STAB OUTER SKIN APPROX 6 INCHES ABOVE 3RD FROM TOP VORTEX GENERATOR R/H SIDE. REPAIRED PER SRM 55-30-3.SDR COMA0160970Bushing · scoredTHE VERTICTAL STABILIZER HINGE BUSHINGS DAMAGED AND REQUIRE REPLACEMENT.REMOVED AND REPLACED VERTICAL STABILIZER HINGE BUSHING I/A/W WVAC EO 601R-55-2892.SDR COMA0160935Bushing · faultyVERTICAL STABILIZER, L/II HORIZONTAL ATTACH LUG BUSHING MIGRATED.REPLACED BUSHING P/N #600-21061-7 IAW SERVICE BULLETIN 601R-55-007, REF MAINT LOG PAGE #243117 AND COMAIR W/O #169071.SDR C2XA01BT176Rudder · crackedBTV---CO3389, DURING 2A INSPECTION MAINTENANCE FOUND #2 RUDDER ON RIGHTHAND LOWER SIDE IS CRACKED AND HAS A HOLE IN IT......MAINTENANCE REMOVED DAMAGED AREA ON #2 RUDDER RIGHTHAND LOWER SECTION. FABRICATED NEW SKIN PART AND EXTERNAL STRAPS IAW EC5540-01015. INSDR DL72W011716Elevator · cracked1/4" CRACK AT RIVET UPPER SKIN OF R/H ELEVATOR APPROX. 14" FWD OF TAB CENTER HINGE. REPAIRED PER DRD 55-20-3D,AND RESTENCILED ELEVATORSDR ABXA010576Rib · crackedLEFT HORIZONTAL STABILIZER RIB WAS CRACKED AT XFS 77. REPAIRED RIB EDGE IAW DC-9 SRM 55-01. PROTECTED AREA AGAINST CORROSION IAW DC-9 SRM 51-10-3.
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