JASC 5534
Service difficulty reports · 820
Reports filed under 5534 · Vertical Stabilizer Miscellaneous 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 = '5534' 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 = '5534' 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 SWAA2014010223757Panel · crackedRT VERTICAL STABILIZER, FWD HORIZONTAL STABILIZER, LOWER SLIDER SEAL PANEL CRACKED ON FWD & AFT EDGES. R & R PANEL IAW MM.SDR SWAA2013121823456Panel · crackedVERTICAL FIN LE LOWER INSIDE REMOVABLE REINFORCEMENT PANEL CRACKED OUT. AREA APPROXIMATELY 30 INCHES UP FROM BOTTOM. REPAIRED PANEL IAW EA.SDR CALA2013102292252Screw · missingTWO SCREWS MISSING ON RT SIDE VERTICAL STABILIZER. THREE EACH SCREWS MISSING ON RT SIDE VERTICAL STABILIZER PANEL 323AR. INSTALLED ONE EACH SCREW, REMAINING TWO ARE MISSING RECEPTACLES. REPLACED TWO EACH MISSING FASTENERS AT AFT END OF PANEL 323AR.SDR SWAA2013111222252Fitting · corrodedRT VERTICAL STABILIZER OTBD REAR DRAG ANGLE FITTING CORRODED. R & R FITTING IAW SRM & DRAWING.SDR CALA2013101792160Strip · crackedVERTICAL STAB FIXED TE BEAM LT & RT ATT STRIP FOUND CRACKED APPROXIMATELY RUDDER STATION 382.4. STRIP REPAIRED IAW ECRA 5530-01725 REV A.SDR CALA2013101792141Support Angle · crackedVERTICAL STAB LT & RT Z SUPPORT ANGLE FOUND CRACKED AT FS 570. REPAIRED IAW ECRA 5530-01729.SDR COEA2013121018923Structure · corrodedHEAVY CHECK, MAJOR REPAIR. AFT DORSAL FIN HAS NUMEROUS AREAS OF LEVEL 2 CORROSION AROUND THE NUT PLATES. REPLACED PART BY FABRICATION IAW ATR42 SRM 55-35-30 REV 100 FIGURE 101.SDR SWAA2013102221382Support · crackedFWD LOWER VERTICAL STABILIZER LE INTERNAL SUPPORT CRACKED AT STATION 113. R & R STRAP IAW SRM & DRAWING.SDR SWAA2013101121077Strap · corrodedVERTICAL STABILIZER SPLICE STRAP CORRODED. R &R STRAP IAW DRAWING & SRM.SDR SWAA2013100220711Cover · crackedVERTICAL STABILIZER COVER CRACKED LOCATED REAR SPAR AT BS 233.09. R & R COVER IAW SRM & DRAWING.SDR SWAA2013100120597Angle · crackedVERTICAL STABILIZER ANGLE CRACKED AT REAR SPAR AT BS 233.09. R &R ANGLE IAW SRM & DRAWING.SDR SWAA2013092620522Angle · crackedVERTICAL STABILIZER ACCESS PANEL NR 9504 ANGLE CRACKED. R & R ANGLE IAW SRM & DRAWING.SDR CALA2013090490988Screw · loose30% OF THE WAY UP THE LT SIDE OF THE VERTICAL STAB HAS A SCREW STICKING OUT. SECURED SCREW & REPLACED ONE MISSING SCREW.SDR 7AHR201308072119Web · puncturedVERTICAL STAB POWER CONTROL UNIT LOWER WEB PUNCTURED AND CRACKED. INSTALLED THE REPAIR IAW B73751-40-2 & 51-30-2.SDR CA130702009Attach Bracket · cracked(CAN) DURING THE POST FLIGHT INSPECTION, IT WAS NOTED THAT THE RT LOWER AUXILAIRY VERTICAL FIN FWD OTBD ATTACH BRACKET WAS CRACKED.SDR SWAA2013070317886Stiffener · crackedRT VERTICAL STABILIZER HORIZONTAL STIFFENER CRACKED JUST ABOVE FWD ATTACH BOLTS. R&R STIFFENER IAW SRM.SDR SWAA2013053116649Attach Bracket · crackedVERTICAL STAB FRONT SPAR SPRING ATTACH BRACKET CRACKED AT BOTH LT AND RT NOTCHED RADIUS. R & R BRACKET IAW SRM.SDR SWAA2013052816570Skate Angle · crackedRIGHT SIDE OF VERTICAL STAB SKATE ANGLE CRACKED. REPAIRED ANGLE IAW EA.SDR SIMA20130508005Drag Angle · crackedDURING 3 C CHECK FOUND LEFT VERTICAL STABILIZER FORWARD AND AFT DRAG ANGLES AT FS1181.00 ARE CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED FORWARD AND AFT DRAG ANGLES IAW EO CR-53MR-164 AND CR-53MR-053. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SWAA2013051516071Support Angle · crackedVERTICAL STABILIZER HORIZONTAL SUPPORT ANGLE CRACKED AT LT AND RT ENDS AFT SIDE OF FWD TERMINAL FITTING JUST ABOVE STAB MOUNT BOLTS. REMOVED AND REPLACED ANGLE IAW SRM.SDR SWAA2013050615618Fitting · crackedVERTICAL STABILIZER FITTING ASSY FOR CROSSMEMBER CRACKED AT BS 1016. REMOVED AND REPLACED FITTING ASSY IAW SRM.SDR SWAA2013050115406Rub Strip · crackedRUB STRIP CRACKED AT ON ACCESS PANEL 9501 VERTICAL STABILIZER DOOR LEFT SIDE. REMOVED AND REPLACED RUB STRIP IAW SRM AND DWG.SDR UALA2013042202759Tape · peelingTAPE ON VERTICAL STAB IS PEELING BACK. CUT OFF LOOSE TAPE AND INSPECTED GFRP. NO DAMAGE IS PRESENT.SDR SWAA2013041714947Retaining Clip · crackedRIGHT VERTICAL STABILIZER LOWER ACCESS PANEL 9508R RETAINER CLIP CRACKED. REMOVED AND REPLACED CLIP PER SRM.SDR SWAA2013041915016Access Panel · crackedVERTICAL STAB T/E ACCESS PANEL 374 CL CRACKED. REMOVED AND REPLACED PANEL IAW SRM.SDR SWAA2013041114745Stiffener · crackedVERTICAL FIN TERMINAL FITTING ASSY LOWER CROSS STIFFENER CRACKED AT BS 1018 ON BOTH ENDS. REMOVED AND REPLACED STIFFENER IAW SRM.SDR REXA2013033000412Structure · damagedVERTICAL STABILIZER HAS TOOL DAMAGE ON THE UPPER LEFT AROUND LEADING EDGE NUT PLATES BETWEEN SPAR STATION 110 AND 117.75 BETWEEN 0.003" AND 0.007". REPAIRED IAW BOMBARDIER REO 601R-55-31-231.SDR WVER2013031951503Drag Angle · damagedPERFORMED MAJOR REPAIR TO VERTICAL STABILIZER LEFT DRAG ANGLE AT SPAR DATUM 67.5% IAW BOMBARDIER REPAIR ENGINEERING ORDER (REO) 670-55-31-018, DATED 16 APRIL 07.SDR COEA2013050306805Structure · delaminatedHEAVY CHECK COE/MAJOR REPAIR: DELAMINATION FOUND ON RIGHT SIDE OF VERTICAL STABILIZER APPROXIMATELY 12 INCH FWD OF MIDDLE SPAR AND 3 FEET ABOVE FUSELAGE. MAJOR REPAIR PER SRAS S553R0016.SDR R61A201302030124Bracket · crackedWHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND BRACKET CRACKED VERTICAL STABILIZER REAR SPAR ABOVE THIRD RUDDER ATTACH HINGE. MAINTENANCE REPAIRED BRACKET IAW EMB ETD02013-170-002161-C REV C. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.SDR SWAA2013013112150Gusset · crackedVERTICAL STAB TO DORSAL FIN FRONT SPAR TERMINATION FITTING LOWER SPRING GUSSET IS CRACKED TO RADIUS ON BOTH FWD SIDES. REMOVED AND REPLACED SPRING GUSSET AS PER SRM 51-40-02.SDR SWAA2013012511869Nut Plate · brokenDORSAL FIN, NUT PLATE 4TH FROM AFT ON RIGHT SIDE IS BROKEN. REMOVED AND REPLACED NUT PLATE AT NR 4 RIB ON RIGHT SIDE OF DORSAL FIN IAW SRM 51-40-02.SDR SWAA2013012411783Plate · crackedCRACK ON PLATE LOCATED ON ACCESS PANEL 9505 VERTICAL STABILIZER. REPLACED PLATE (RETAINER) LOCATED ON ACCESS PANEL 9505 VERTICAL STABILIZER IAW B737-300 SRM 51-10-02 ITEM 8 SRM 51-40-02 AND DRAWING 65-54800.SDR SWAA2013012411782Plate · crackedCRACK ON PLATE LOCATED ON ACCESS PANEL 9503L VERTICAL STABILIZER. REPLACED PLATE (RETAINER) LOCATED ON ACCESS PANEL 9503L. VERTICAL STABILIZER IAW B737-300 SRM 51-10-02-0G-0 ITEM 8 B737-300 SRM 51-40-02-0G-0 AND DRAWING 65-54815.SDR SWAA2013012411781Plate · crackedCRACK ON PLATE LOCATED ON ACCESS PANEL 9502R VERTICAL STABILIZER. REPLACED PLATE (RETAINER) LOCATED ON ACCESS PANEL 9502R VERTICAL STABILIZER IAW B737-300 SRM 51-10-02-0G-0 ITEM 8 B737-300 SRM 51-40-02-0G-0 AND DRAWING 65-48249.SDR SWAA2013012111594Gusset · crackedCRACK ON GUSSET LOCATED FIN STA 136.30 INTERNAL AREA VERTICAL STABILIZER. REPLACED GUSSET LOCATED FIN STA 136.30 INTERNAL AREA VERTICAL STABILIZER IAW SRM B737-300 51-10-02 ITEM 8 AND DWG 65-47401.SDR SWAA2013011411430Plate · crackedCRACK ON PLATE LOCATED AT ACCESS PANEL N. 9501 LEFT FWD FIN VERTICAL STABILIZER. REPLACED PLATE LOCATED AT ACCESS PANEL N. 9501 LEFT FWD FIN VERTICAL STABILIZER IAW SRM B737-300 51-10-02 ITEM 8 AND DRAWING N. 65-48249 AND SRM B737-300 51-40-02.SDR SWAA2012123110983Angle · crackedCRACK ON ANGLE ON ACCESS PANEL 9503. REPLACED ANGLE OF ACCESS PANEL 9503 IAW B737-300 51-10-02 AND DRAWINGSDR SWAA2012121210530Panel · crackedCRACK ON ALL FASTENER HOLE OF BALANCE PANEL 9537 OF VERTICAL STABILIZER. REPAIRED BALANCE PANEL 9537 IAW B737-300 SRM 51-70-07-0G-0.SDR SWAA2012121210519Panel · crackedCRACK ON ALL FASTENER HOLE OF BALANCE PANEL 9538 OF VERTICAL STABILIZER. REPAIRED RUDDER BALANCE PANEL 9538 IAW B737-300 SRM 51-70-07-0G-0.SDR SWAA2012121210518Panel · crackedCRACK ON ALL FASTENER HOLE OF BALANCE PANEL 9536 OF VERTICAL STABILIZER. REPAIRED RUDDER BALANCE PANEL 9536 IAW B737-300 SRM 51-70-07-0G-0.SDR SWAA2012121210517Panel · crackedCRACK ON ALL FASTENER HOLE OF BALANCE PANEL 9535 OF VERTICAL STABILIZER. REPAIRED RUDDER BALANCE PANEL 9535 IAW B737-300 SRM 51-70-07-0G-0.SDR ABXA20121121338Support Angle · crackedLEFT AND RIGHT OUTBOARD WEB SUPPORT ANGLES AT THE BOTTOM OF THE VERTICAL STABILIZER HAS 2 INCH CRACK ON EACH ANGLE. VIEWED THRU PANELS 324LL. REMOVED AND REPLACED ANGLES IAW 51-40-02 SRM, ACFT WAS GROUNDED.SDR ABXA20121127341Web · crackedWEB STIFFENER FORWARD OF STA 1755 ON BOTTOM WEB OF VERTICAL STABILIZER IS CRACKED IN BOTH INBOARD AND OUTBOARD OF CORNERS. REMOVED AND REPLACED WEB STIFFENER IAW B767 SRM 54-40-02. ACFT WAS GROUNDED.SDR SWAA2012112109724Plate · crackedCRACK ON PLATE LOCATED ACCESS PANEL 9505 VERTICAL STABILIZER. REPLACED PLATE LOCATED ACCESS PANEL 9505 VERTICAL STABILIZER IAW SRM 51-10-02 ITEM 8, SRM B737-300 51-40-02 AND DWG.SDR USAA2012111300002Panel · debondedRON VISIT - AREA OF DISBOND ON VERTICAL STABILIZER FORWARD SPAR BOX PANEL BETWEEN BS 1729 TO BS 1786 & BEWTEEN FSS119 TO FSS191. REPLACED VERTICAL STABILIZER FORWARD SPAR BOX PANEL IAW B757 SRM 51-40-02 & BOEING DRAWING 175N2001.SDR SWAA2012111509377Stiffener · crackedVERTICAL STAB STA 127.10 AT REAR SPAR LEFT TRIANGLE STIFFENER CRACKED. (HFEC VERIFIED) REPAIRED GUSSET PER SRM 51-70-11.SDR SWAA2012111509376Stiffener · crackedVERTICAL STAB STA 127.10 AT REAR SPAR RIGHT TRIANGLE STIFFENER CRACKED (HFEC VERIFIED). REPAIRED GUSSET PER EA1-355-1743 AND SRM 51-70-11.SDR USAA2012102300004Panel · delaminatedC2 CHECK - AREA OF DELAMINATION ON LEFT VERTICAL STABILIZER FORWARD TORQUE BOX PANEL AT FSS 220. REPLACED LEFT VERTICAL STABILIZER FORWARD TORQUE BOX PANEL AT FSS 220 IAW B757 SRM 55-30-01 & 51-70-10.SDR 29GA93755101712Channel · crackedDURING SCHEDULED INSPECTION FCD 55-09-19-02 FOUND CRACK IN HAT SECTION OF VERTICAL STABILIZER AREA C.
Back to JASC 5534