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 UIEA2022081300856None · noneLH STA 2598 BULKHEAD LOWER CORNER 2EA FASTENER HOLES FOUND CRACK AT 6 O/C WEB LAYER.(<P>2EA FASTENER HOLES CRACK AREA REPAIRED AS PER RI NO : RI-53-00-15826 REV A</P>)SDR UIEA2022081300855None · noneLH STA 2598 BULKHEAD LOWER CORNER 1EA FASTENER HOLE FOUND CRACK AT 6 O'CLOCK OF FWD INNER SUPPORT LAYER WITH APPROX 0.050" DEPTH(<P>1EA FASTENER HOLE CRACK AREA REPAIRED AS PER RI NO : RI-53-00-15826 REV A </P>)SDR A6WA202209088323Hinge Fitting · gougedL/H ELEVATOR HINGE #2 FITTING GOUGED .550"L X .500"W X .010"D BETWEEN FS 59.02 AND FS 62.02. EVALUATED DAMAGE AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 55-20-00 REV 39. *********AIRCRAFT REMOVED FROM SERVICE*************************** PERFORMED BLESDR CALA2022090702288None · noneL/H HORIZONTAL STAB LOWER SKIN REQUIRES CUTOUT AT STA. 92.70 #1 VERTICAL RIB STIFFENER REPAIR. 41437 ACCOMPLISHED TASKS AND PARTIAL WORK ACCOMPLISHED (HFEC INS TE JULY 6 2022 06:54. HFEC COMPLETED ON UPDATED ENTRY SUB TASK 0 T-76511 PO: 123199. 2.) 7075 T-62 PSDR CALA2022090502278Fitting · noneDURING REMOVAL OF RUDDER HINGE FITTING #4 DUE TO REPLACEMENT SOME ENLONGATED HOLES WERE FOUND. DO REPAIR TO ENLONGATED HOLES AS PER SRM TASK 55-36-45-300-008 REV.141. AS NOTED ON LTPR NR# 5001174244-0010. REMOVED & REPLACED RUDDER HINGE ARM #4.SDR CALA2022090502254Fitting · noneTHE FOLLOWING ITEMS ARE OR MAY BECOME OVERTIME: 13) TASK, A319, ()A-CK ESCALATION 6A1 TO 4A1 PHZ-IN 17-0552-8-0045 14) TASK, A319, ? HYD PWR SYS ACCUM VCK IOL 1C1 17-0529-8-0029 15) TASK, A319, MAG CHP DET / ENG START SVC IOL 1A1 17-0579-8-0001 16) TASK, A319SDR IXXA2022090201Support · corrodedVERTICAL STAB LH AFT TE PANEL SUPPORT CORRODEDSDR CALA2022083102229Skin · noneR/H HORIZONTAL STAB LOWER SKIN AT STA. 101.90 REQUIRES ACCESS HOLES TO BE CUT IN SKIN FOR #3 RIB REPAIR REF. BAM N/R 000804044 AND N/R 000844208. REQUIREMENTS PER SRM 55-10-01-2R REPAIR 11 TABLE 204. INSPECTION PERFORM DETAILED VISUAL INSPECTION AND EXTERNAL LSDR CALA2022082902203None · crackedRIGHT HORIZONTAL STABILIZER-CRACK FOUND AT APPROXIMATE STAB STA 147.90 AND 23.5 INCHESS AFT OF THE FRONT SPAR. REF.BAM N/R 000803532 REQUIREMENTS PER SRM 55-10-01-2R REPAIR 11 TABLE 204. INSPECTION PERFORM DETAILED VISUAL INSPECTION AND EXTERNAL LFEC EVERY 9,0SDR CALA2022082402151Skin · damagedR/H HORIZONTAL STAB LOWER SKIN AT STA. 101.90 REQUIRES ACCESS HOLES TO BE CUT IN SKIN FOR #3 RIB REPAIR REF. BAM N/R 000804044 AND N/R 000844208. REQUIREMENTS PER SRM 55-10-01-2R REPAIR 11 TABLE 204. INSPECTION PERFORM DETAILED VISUAL INSPECTION AND EXTERNAL LSDR QMLA2022FA0000446Doubler · damagedVERTICAL FIN ACCESS PANEL 341CR FASTENER HOLE DAMAGED REF ENGINEERING MEMO DQ35850M1 DATED 8/8/2022SDR UIEA2022070100702None · noneRH HORI STAB UPPER SKIN AND UPPER REAR SPAR CHORD ZONE B INSP 1EA FASTENER HOLE FOUND CRACK.(<P>RH HORI STAB UPPER SKIN AND UPPER REAR SPAR CHORD ZONE B FASTENER HOLE REPAIRED IAW RI 55-00-15706 REV.A</P>)SDR IXXA2022070904Tie Clip · crackedSTRINGER CLIP CRACKEDSDR MK1Y20220706012Repair · discoveredR/H HORIZONTAL STABILIZER – UPPER SKIN: DURING MAINTENANCE PRACTICES AT IAI IN TLV, AN EXISTING UNDOCUMENTED REPAIR WAS FOUND ON R/H HORIZONTAL STABILIZER UPPER SKIN. THE SKIN IS MADE FROM ALCLAD 7075-T6 1.100” IN THICK. THE REPAIR FOUND CONSISTS IN ONE DOUBLESDR CALA2022060601441Skin · puncturedRIGHT ELEVATOR HAS ONE PUNCTURE DUE TO HAIL, 27 INCHES FROM INBOARD EDGE, 31 1/2 INCHES FROM TRAILING EDGE, 1 INCH DIAMETER COVERED UP REF SRM 55-20-01-1A-1, NO DELAMINATION NOTED OUTSIDE DAMAGE AREA, PROTECTED PUNCTURE WITH SPEED TAPE. LOCKED FOR MAINTENANCE SDR IXXA2022060401Panel · separatedVERTICAL STAB LH PANEL SEPERATINGSDR MK1Y20220429024Repair · discoveredLEADING EDGE SKIN, RIGHT HORIZONTAL STABILIZER, LES 342.677 TO 346.177 AND LES 401.577 TO 405.07: DURING CONVERSION PROCESS, DISCOVERED (2 EA) EXISTING (UNDOCUMENTED 3.5” DIAMSDR CALA2022052301313Fitting · gougedDURING REMOVAL OF THE RUDDER, VERTICAL STABILIZER HINGE FITTINGS NO.2 FOUND WITH PLAY AND GOUGE. REPLACEMENT IS REQUIRES AS NOTED ON LTPR NR# 5001156950-0010 REF BQN LHT LOG NUMBER 50001156950-0010. REPLACED RUDDER HINGE FITTING #2 PER SRM 55-36-42-300-008. RSDR CALA2022052301312Fitting · gougedDURING REMOVAL OF THE RUDDER, VERTICAL STABILIZER HINGE FITTINGS NO.7 FOUND WITH PLAY AND GOUGE. REPLACEMENT IS REQUIRED AS NOTED ON LTPR NR# 5001156958-0010. REF BQN LHT LOG 5001156958-0010.REPLACED RUDDER HINGE FITTING #7 PER SRM 55-36-42-300-008. REPLACEMENSDR CALA2022052301311Fitting · gougedDURING REMOVAL OF THE RUDDER, VERTICAL STABILIZER HINGE FITTINGS NO.3 FOUND WITH PLAY AND GOUGE.REPLACEMENTE IS REQUIRED AS NOTED ON LTPR NR#5001156951-0010. REPLACED #3 HINGE FITTING. REPLACEMENT REQUIRED IAW SRM REF BQN LHT NRC 5001156951-0010. 55-36-42-300-SDR CALA2022052301310Fitting · gougedDURING REMOVAL OF THE RUDDER, VERTICAL STABILIZER HINGE FITTINGS NO.6 FOUND WITH PLAY AND GOUGE. REPLACEMENT IS REQUIRED AS NOTED ON LTPR NR# 5001156957-0010. REPLACED #6 HINGE FITTING. REPLACEMENT REQUIRED IAW SRM REF BQN LHT NRC 5001156957-0010 55-36-42-300-SDR CALA2022052301309Fitting · gougedDURING REMOVAL OF THE RUDDER, VERTICAL STABILIZER HINGE FITTINGS NO.4 FOUND WITH PLAY AND GOUGE. REPLACEMENT IS REQUIRED AS NOTED ON LTPR NR# 5001156954-0010. REPLACED #4 HINGE FITTING. REPLACEMENT REQUIRED IAW SRM REF BQN LHT NRC 5001156954-0010 55-36-42-300-SDR CALA2022052301308Fitting · looseRUDDER HINGE BEARINGS/FITTINGS BR2, BR3, BR4 AND BR7 HAVE EXESSIVE PLAY. LTPR NR# 5001148819-0010 RUDDER HINGE FITINGS ASSY''S BR2, BR3, BR4 & BR7 REPL''ED IAW SRM 55-36-42-300-008, CAT "A" MAJOR REPAIR, PERMANENT WITH NO ADD''L INSPECTION REQUIREMENTS RII ACSDR CALA2022052301307Fitting · looseRUDDER HINGE BEARINGS/FITTINGS BR1 AND BR5 HAVE EXCESSIVE PLAY. LTPR NR# 5001148819-0010 AT 60000FC FROM TIME OF COMPONENT FIRST FLIGHT, SUBSEQUENT SRI 55-36-42-205-004 INSPECTION INTERVALS AND METHOD OF INSPECTION ARE TBD IAW RUDDER HINGE FITINGS ASSY''S BR 1SDR CALA2022052301306Fitting · looseRUDDER HINGE BEARINGS/FITTINGS BR1 AND BR5 HAVE EXCESSIVE PLAY. LTPR NR# 5001156747-0010(BR1), 5001156956-010(BR5). AT 60000FC FROM TIME OF COMPONENT FIRST FLIGHT, SUBSEQUENT SRI 55-36-42-205-004 TABLE 001. INSPECTION INTERVALS AND METHOD OF INSPECTION ARE TBDSDR CALA2022052001305None · noneRUDDER HINGE BEARINGS/FITTINGS BR2, BR3, BR4 AND BR7 HAVE EXESSIVE PLAY. LTPR NR# 5001148819-0010 RUDDER HINGE FITINGS ASSY''S BR2, BR3, BR4 & BR7 REPL''ED IAW SRM 55-36-42-300-008, CAT "A" MAJOR REPAIR, PERMANENT WITH NO ADD''L INSPECTION REQUIREMENTSSDR 2022FA0000267None · noneDURING EXECUTION OF TASK CARD 55-880-00-01 CRACK WAS FOUND BETWEEN STA101.90 AND STA 129.50 ON LH HORIZONTAL STABILIZER SKIN. CRCK BETWEEN STA92.70 AND STA101.90 ON RH HORIZONTAL STABILIZER LOWER SKIN.SDR MK1Y20220429006None · noneHORIZONTAL STABILIZER, CENTER SECTION, UPPER SKIN, RBL 28.33, STR-U10: DURING MAINTENANCE INSPECTION, CORROSION DAMAGE WAS FOUND AT DATUM LOCATION AS MENTIONED ABOVE. THE CORROSION WAS REMOVED AND REMAINING MATERIAL THICKNESS MEASUREMENT WAS PERFORMED.SEE RFTASDR CALA2022042701077Skin · puncturedLEFT ELEVATOR HAS 10 PUNCTURES DUE TO HAIL. 1) 97 INCHES FROM INBOARD, 15 INCHES FROM TRAILING EDGE, 1 INCH DIAMETER. 9) 102 INCHES FROM INBOARD, 11.5 INCHES FROM TRAILING EDGE, .5 INCHES DIAMETER. 2) 104 INCHES FROM INBOARD, 11 INCHES FROM TRAILING ESDR CALA2022042701076Skin · puncturedRIGHT ELEVATOR HAS SEVEN PUNCTURES DUE TO HAIL. 1) 21 INCHES FROM INBOARD, 23 INCHES FROM TRAILING EDGE, 1 INCH DIAMETER. 2) 85 INCHES FROM INBOARD, 16 INCHES FROM TRAILING EDGE, 1 INCH DIAMETER. 3) 100 INCHES FROM OUTBOARD EDGE, 12 1/2 INCHES FROM TRAILISDR CALA2022042101047Fitting · crackedAD 2013-08-02 SUPPORT TASK EA 5510-01896 REV C OP 005 1EA CRACK WAS FOUND ON LH ELEVATOR O/B ACTUATOR FITTING APPROX 2 3/4 IN LENGTH ATRADIUS AREA AS MARKED. PLS PRINT & ACCOMPLISH OP 09 OF THS EA. TRANSFER REF.NON-ROUTINE HX NRC WO.699257 AND ORIGINATED BY EMSDR CALA2022041400992Rib · crackedEA 5510-01843 REV H OPERATION 001: LH HORZ STAB AT RIB 147.9 HAS CRACK INDICATION. REFER TO PEMCO N/R 12251.0390. LFEC REQUIRED AT 9,000 FLIGHT CYCLES. INSPECTION THRESHOLD AT 44,098.36. ENTERED BY V927864. WORK PERFORMED BY V934069. 56,000 FLIGHT CYCLES. CURRSDR CALA2022041400991Rib · crackedEA 5510-01843 REV H OPERATION 001: RH HORZ STAB AT RIB 175.50 FWD HAS CRACK INDICATION. REFER TO PEMCO N/R 12251.0392. PRIME, AND TOPCOAT ALL IAW 737-900 SRM 55-10-01-2R-11 REPAIR 11. THRESHOLD AT 56,000 FLIGHT CYCLES. CURRENT FLIGHT CYCLES 15,398 V893964. INSSDR CALA2022041400995Rib · crackedEA 5510-01843 REV H OPERATION 001: RH HORZ STAB AT RIB 175.50 AFT HAS CRACK INDICATION. REFER TO PEMCO N/R 12251.0391. PRIMED, AND TOP COAT ALL IAW B737-900 SRM 55-10-01-2R-11 REPAIR THRESHOLD AT 56,000 FLIGHT CYCLES. CURRENT FLIGHT CYCLES 15,398 V893964. INSPSDR P5CA2022032300097None · noneR/H H-STAB STA BL 421.5 LOWER CHORD CRACKED(<P>LOWER CHORD CRACK AREA REPAIRED AS PER SRM 55-10-09-2R-12 REPAIR 12,FIG.201,DETAIL VII</P>)SDR P5CA2022032500099None · noneVERTICAL FIN FWD L/E FAIRING #321B FOUND DENT MARK(<P>DENT AREA REPAIRED AS PER SRM 55-30-01-2R-4 REPAIR 4 FIG.201</P>)SDR P5CA2022032600100None · noneLH H.STAB REAR WEB AT STA BL 391.9 ANGLE CRACKED.(<P>CRACK ANGLE LOCAL FABRICATED AS PER RI NO. RI-55-00-15458 REV A AND NEW ANLGE INSTALLED AS PER SRM 51-40-02.</P>)SDR P5CA2022032600101None · noneR/H H.STAB BL 421.5 UPPER CHORD CRACKED.(<P>R/H H.STAB BL 421.5 UPPER CHORD REPLACED ACCOMPLISHED IAW SRM 51-40-02 AND SRM 51-40-05 REV 36, 20 FEB 2022 </P>)SDR P5CA2022032600102Web · noneR/H H.STAB, STAB BL 421.5 WEB CRACKED(<P>CRACK WEB REPLACED AS PER SRM 51-10-02 AND NEW WEB INSTALLED AS PER SRM 51-40-02</P>)SDR P5CA2022032600103None · noneL/H STAB TIP FAIRING ATTACH U-CHANNEL CRACKED.(<P>LH STAB TIP FAIRING ATTACH U-CHANNEL P/N 65B03822U11 WAS REPLACED AS PER RI NO. RI-55-10-15472 REV A AND INSTALLED AS PER SRM 51-40-02 REV 36, DATE 20 FEB 2022.</P>)SDR P5CA2022032600104None · noneRH H.STAB TIP FAIRING ATTACH U-CHANNEL CRACKED.(<P>RH H.STAB TIP FAIRING ATTACH U-CHANNEL P/N 65B03822U12 WAS REPLACED AS PER RI NO. RI-55-10-15473 REV A AND INSTALL AS PER SRM 51-40-02 REV 36. DATE 20 FEB 2022.</P>)SDR VNAA202203259994Angle · cracked(N0071) THE R/H DRAG ANGLE WHERE THE VERTICAL STAB, FUSELAGE, AND APU FIREWALL MEET IS CRACKED. PERFORMED PERM. REPAIR ON R/H AFT DRAG ANGLE PER CRJ700 SRM 55-31-00-201-001-A01SDR GTIA2022032436333Hinge Arm · corrodedRUDDER ARM HINGE #6 CORRODED. RAF 275970401 CREATED.-REVIEWED NR#5001140903-0050 AND TASK CARD 1003692350-0010,PERFORMED REPAIR BY REPLACEMENT OF RUDDER HINGE ARM BR # 6 I.A.W. SPIRIT EO 5546-2202 REVISION 00SDR CALA2022032300744Rib · crackedL/H HORIZONTAL STAB STA 101.90 RIB CRACKED AT LOWER FWD FLANGE REF AAR N/R 9642208 INSTALLED REPAIR ANGLE AT LT HORIZONTAL STAB STA 101.90 AT LOWER FWD FLANGE OF RIB REF B737 SRM 55-10-09-2R-5 FIG 205 WORK ACCOMPLISHED BY V920314SDR CALA2022032100721Rib · crackedR/H HORIZONTAL STAB RIB NO.1 AT STA 82.70 CRACKED AT NO.3 VERTICAL STIFFNER LOWER AREA REF AAR N/R 9642159 REMOVED NO.1 RIB AT STA 92.70 REMOVED T-SCETIOC REPAIR EXTRUSION REPAIR AT RIB NO.1 AND REINSTALLED RIB AT FR STA 92.70 REF B737 FOR HEAT TREAT AND REMOVSDR UIEA2022022000148Channel · crackedL/H HORI STAB TIP FAIRING ATTACHED U CHANNEL CRACKED.(<P>L/H HORI STAB T/E BOND ASSY. ATTACHED U CHANNEL WAS REPLACED AND INSTALLED AS PER RI-55-10-15385 REV A.</P>)SDR JJBA20220217019Not Reported · not reported2 BROKEN NUT PLATES AND SKIN DAMAGE ON LH SIDE OF RUDDER 1. PERFORMED REPAIR ON DAMAGED SKIN ON LH SIDE OF RUDDERSSDR 2022F00083None · corrodedHORIZONTAL STABILIZER (LEFT SIDE) UPPER SKIN CORROSION. ACCOMPLISHED TEXTRON AVIATION ENGINEERING LETTER DQ33582M1 DATED FEB/15/2022; 680A-0113 (N563QS) HORIZONTAL STABILIZER (LEFT SIDE) UPPER SKIN CORROSION.SDR IXXA2022021202Stringer · corrodedSTRINGER 4 REPAIR CORRODEDSDR SWAA2022031572029Tail Cone · debondedTAIL CONE R/H SIDE HAS DISBOND AT BS 1156+9' AND 6' FROM TAIL CONE ACCESS DOOR CUTOUT LOWER CORNER / [01] IDENTIFIED TAIL CONE MATERIAL IAW SRM 53-80-70-0I-1 TABLE 2 FIGURE 2 ITEM 1. DAMAGE AT DISCREPANT LOCATION EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM 53-80-7
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