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 CALA2022021100353Skin · cracked(SUPPORT TASK) C-SCAN INDICATION FOUND ON RH HORIZONTAL STABILIZ ER LOWER SURFACE 29" FROM TE AND 67.5" FROM I/B EDGE. 120.30 TO STA 157.10) PER SRM 55-10-01-2R-11 REPAIR 11. REPAIR REPEAT EVERY 9,000 FLIGHT CYCLES. DATA TRANSCRIBED FROM PAPER INSPECTION REQUISDR IXXA2022020404Skin · corrodedANGLE CORRODED BEYOND LIMITS.SDR IXXA2022020307Stringer · corrodedHORIZONTAL LOWER RIB CORRODED BEYOND LIMITSSDR R61A2022021400143Rib · crackedLH HORIZONTAL STABILIZER RIB 14 CRACKED ON UPPER O/B SIDE AS MARKED : PERFORMED PERMANENT REPAIR BY CUTOUT, FILLER AND DOUBLER REPAIR ON LH HORIZONTAL STABILIZER RIB 14 IN ACCORDANCE WITH, REF ETD2022-170-004532. SEE WIP'S AND TASKS FOR WORK PERFORMED.SDR P5CA2022012600018None · noneL/H STAB TIP FAIRING RIB #2 (COUNT FROM FWD) FOUND CRACKED(<P>HORI STAB TIP RIB - STRUCTURE WITH 11 RIBS-REPAIR</P>)SDR P5CA2022012600019None · noneL/H STAB TIP FAIRING RIB #9 (COUNT FROM FWD) FOUND CRACKED(<P>HORI STAB TIP RIB - STRUCTURE WITH 11 RIBS-REPAIR</P>)SDR 2022FA0000044None · noneLH AND RH HORIZONTAL CUFF PANEL LE, AND AREA ABOVE LH CUFF PANEL, EXPOSED COMPOSITE. REPAIRED IAW TEXTRON AVIAITON ENGINEERING REPORT NO: DQ33272 DATED JAN 23, 2022.SDR IXXA2022012002Stringer · corrodedSTRINGER CORRODED BEYOND LIMITSSDR CALA2022011400128Skin · cracked(SUPPORT TASK) FOUND C-SCAN INDICATION ON R/H HORZ STAB LOWER SU RFACE AT A LOCATION 18.5 INCHES FROM REAR SPAR AND 8.75 IN. FROM RIB 4 OF THE HORIZONTAL STABILIZER REPAIRED CRACK FOUND BY C-SCAN INDICATION ON R/H HORIZONTAL STAB TRANSCRIBED FROM PAPER DOC AERSDR IXXA2022010803Rib · damagedDAMAGE ON RIB BULB STRIP.SDR IXXA2022010802Rib · gougedRIB WEB GOUGEDSDR CALA2022010500024Elevator · puncturedLEFT ELEVATOR HAS FOUR PUNCTURES DUE TO HAIL 1. 31 INCHES INBOARD FROM OUTBOARD EDGE 15 INCHES FROM TRAILING EDGE 1 INCH DIAMETER 2. 127 INCHES INBOARD 24 INCHES FROM TRAILING EDGE .75 INCH DIAMETER 3. 172 INCHES INBOARD 21 INCHES FROM TRAILING EDGE 1.250 INCHSDR CALA2022010500021Elevator · dentedRIGHT ELEVATOR UPPER SURFACE FOUND HAS MULTIPLE DENTS REF HAECO NON-ROUTINE NO.9470106 - ORIGINATED BY EMP V923294. PERFORMED BY EMP V923294,RH ELEVATOR UPPER SURFACE MULTIPLE DENTS REPAIRED AS PER SRM 55-20-01-2R-1 REPAIR 1 TABLE 201 PARA 4D AND SRM 51-70-04-SDR MK1Y202201016None · noneHORIZONTAL STABILIZER, CENTER SECTION, UPPER SKIN, REAR SPAR – AT RBL10.33 STR U3 TO REAR SPAR: DURING MAINTENANCE INSPECTION AT IAI, CORROSION WERE FOUND.THE CORROSION WAS REMOVED AS PER SRM 51-20-01.THE SKIN REMAINING MATERIAL THICKNESS WAS ACCOMPLISHED. THESDR MK1Y202201015None · noneHORIZONTAL STABILIZER, CENTER SECTION, UPPER SKIN, REAR SPAR – AT LBL10.83 STR U3 TO U2 AND LBL 11.83 STR U2 TO U1: DURING MAINTENANCE INSPECTION AT IAI, CORROSION WERE FOUND.THE CORROSION WAS REMOVED AS PER SRM 51-20-01.THE SKIN REMAINING MATERIAL THICKNESS WSDR MK1Y202201014None · noneHORIZONTAL STABILIZER, CENTER SECTION, UPPER SKIN, REAR SPAR – AT RBL10.33 STR U1 TO REAR SPAR: DURING MAINTENANCE INSPECTION AT IAI, CORROSION WERE FOUND.THE CORROSION WAS REMOVED AS PER SRM 51-20-01.THE SKIN REMAINING MATERIAL THICKNESS WAS ACCOMPLISHED. THESDR CALA2021122902470Elevator · dentedRIGHT ELEVATOR UPPER SURFACE FOUND HAS MULTIPLE DENTS REF HAECO NON-ROUTINE NO.9470106 - ORIGINATED BY EMP V923294. PERFORMED BY EMP V923294,RH ELEVATOR UPPER SURFACE MULTIPLE DENTS REPAIRED AS PER SRM 55-20-01-2R-1 REPAIR 1 TABLE 201 PARA 4D AND SRM 51-70-04-SDR CALA2021122902460Rib · cracked(B737 -55-3-0239) RH HORIZONTAL STABLIZER INSPAR RIB AT STA 101.0 HAS CRACK AT FWD UPPER WEB EDGE WHERE IT MEETES THE T-CHORD. REF AAR NR 9644092 ACCOMPLISHED REPAIR AT RIGHT HORIZONTAL STAB AT STA 101.0 REF B737-900 SRM 51-40-02-0G-0 AND RES-WI 2017928-30 ANDSDR CALA2021122302429Rib · crackedL/H HORIZONTAL STAB STA 92.70 RIB NO.1 STIFFENER NO.2 CRACKED AT LOWER END REF AAR N/R 9643347 REMOVED DAMAGED AREA INSTALLED 1EA REPAIR ANGLE AND 1EA T SEC ON THE L/H HORIZONTAL STAB STA 92.70 RIB NO.1 STIFFENER NO.2 LOWER END AS PER B737 SRM 55-10-09-1R-4 INSDR CALA2021122202427Pressure Web · crackedSUPPORT TASK-NDT INSPECTION FOUND A CRACK AT CENTER WING REAR SPAR VERTICAL PRESSURE WEB BETWEEN RBL 40.00 AND RBL 45.64,BETWEEN WL192.0 AND WL 200.6 CRACK LENGTH 0.394IN REF AAR NR 9643110 INICIAL WEB CUTOUT IN REFERENCE WITH B737-900ER REPAIR AREA. FABRICATESDR CALA2021122202421Rib · crackedRT HORIZONTAL STAB RIB AT STA 101 LOWER CHORD I/B FASTNER HOLE HAS A SMALL CRACK JUST BELOW CENTER LIGHTING HOLE REF AAR N/R 9644094 REMOVED ANGLE AREA INSTALLED 1EA REPAIR ANGLE ON R/H HORIZONTAL STAB RIT AT STA 101 LOWER CHOED AS PER B737 SRM 55-10-09-2R-5 FSDR 2021F00359None · noneAPU STINGER LH AND RH SKINS HAVE BUBBLING PAINT. REPAIRED IAW CESSNA TEXTRON AVIATION ENGINEERING MEMO DQ32785M1 DATED DECEMBER 13,2021SDR CALA2021121702392None · crackedRT HORIZONTAL STAB RIB AT STA 101 LOWER CHORD I/B FASTNER HOLE HAS A SMALL CRACK JUST BELOW CENTER LIGHTING HOLE REF AAR N/R 9644094 REMOVED ANGLE AREA INSTALLED 1EA REPAIR ANGLE ON R/H HORIZONTAL STAB RIT AT STA 101 LOWER CHOED AS PER B737 SRM 55-10-09-2R-5 FSDR CALA2021121702390Stiffener · crackedL/H HORIZONTAL STAB STA 92.70 RIB NO.1 STIFFENER NO.2 CRACKED AT LOWER END REF AAR N/R 9643347 REMOVED DAMAGED AREA INSTALLED 1EA REPAIR ANGLE AND 1EA T SEC ON THE L/H HORIZONTAL STAB STA 92.70 RIB NO.1 STIFFENER NO.2 LOWER END AS PER B737 SRM 55-10-09-1R-4 INSDR CALA2021121302354Elevator · damagedRT ELEVATOR STRUCK BY JLG, DAMAGE IS 83" OB OF IB EDGE 12" AFT OF LEADING EDGE 52" FORWARD OF TRAILING EDGE. APPROX PENETRATION 7.5" PERFORMED CONDITIONAL INSECTION PER AMM 05-51-59, NO ADDTIONAL DAMAGE FOUND. TAP TESTED EXISTING DAMAGE , NO DELAMINATION NOTEDSDR CALA2021121202347Elevator · damagedRIGHT ELEVATOR HAS FOUR PUNCTURES CAUSED BY HAIL. 1. 17.5 OUT FROM THE INBOARD EDGE, 51.5 UP FROM THE TRAILING EDGE, 1.0 DIAMETER. 2. 25.0 OUT FROM THE INBOARD EDGE, 56.50 UP FROM THE TRAILING EDGE 1.0 DIAMETER. 3. 19.5 OUT FROM THE INBOARD EDGE, 30 UP FROM THSDR CALA2021121202346Elevator · damagedLEFT ELEVATOR HAS TWO PUNCTURES CAUSED BY HAIL. 1. 144 INBOARD OF THE OUTBOARD EDGE,23.0 UP FROM THE TRAILING EDGE .50 DIAMETER. 2. 23.0 OUTBOARD OF THE INBOARD EDGE 23 UP FROM THE TRAILING EDGE 1.0 DIAMETER. REF SRM 55-20-01-1A-1FIGURE 102 DAMAGE 1 WITHIN LIMSDR R61A2021122001027Skin · damagedPIN HOLE ON UPPER SKIN OF RH HORIZONTAL STABILIZER AT REAR SPAR BETWEEN RIBS 10 AND 11. : REMOVED PIN HOLE DAMAGE ON UPPER SKIN OF RH HORIZONTAL STABILIZER AT REAR SPAR BETWEEN RIB 10-11 BY DRILLING THROUGH DAMAGE AND INSTALLING RIVET. REF EMB ETD2021-170-0418SDR R61A2021122001026Fitting · wornLH HORIZONTAL STABILIZER BEARING FITTING DAMAGED ON I/B SIDE AROUND ENTIRE CIRCUMFERENCE. : PERFORMED TEMPORARY REPAIR ON LH HORIZONTAL STABILIZER BEARING FITTING ON I/B SIDE AROUND ENTIRE CIRCUMFERENCE BY SPOT FACING. REMAINING THICKNESS 0.517" REF ETD2021-17SDR R61A2021122001025Fitting · wornRH HORIZONTAL STABILIZER BEARING FITTING DAMAGED ON I/B SIDE AROUND ENTIRE CIRCUMFERENCE. PERFORMED A PERMANENT REPAIR ON RH HORIZONTAL STABILIZER BEARING FITTING ON I/B SIDE AROUND ENTIRE CIRCUMFERENCE BY SPOT FACING. REMAINING THICKNESS 0.525" REF ETD2021-17SDR CALA2021121002335Hinge Fitting · wornLH ELEVATOR #6 HINGE FITTING, IB AND OB BUSHINGS ARE WORN ON INN TER DIAMETER (REMOVE AND REPLACE - SDR) REMOVED AND REPLACED #6 HINGE FITTING I/B AND O/B BUSHINGS IAW S RM 51-72-12-911-002 FIG 002 SHEET 01 AND CMM SUBTASK 55-21-15-41 0-012-A01. P/N D559820012SDR MASA20211213617None · erodedTHE VERTICAL STABILIZER BULLET FAIRING UPPER PANEL ASSEMBLY WAS FOUND HAVING EROSION DAMAGE. PERFORMED PERMANENT REPAIR JAW CRJ7/9 SRM 51-74-02-201-001-A01, (REV. DATED 7-9-2021). DEFECT LOCATION: VERTICAL STABILIZER BULLET FAIRING UPPER PANELSDR JR2R20218327384Rib · crackedL/H STAB RIB 12A CRACKEDSDR CALA2021120802277Bushing · wornLH ELEVATOR #6 HINGE FITTING, IB AND OB BUSHINGS ARE WORN ON INN TER DIAMETER (REMOVE AND REPLACE - SDR)SDR CALA2021120102205Lever · chippedA3NB-55-3-6005 RH ELEVATOR HINGE ARM LWR EDGE I/B SIDE CHIPPED D OT 42-070 () REMOVED LINES HYD ACCESS IAW AMM 27-34-51-000-001-A. RECEIVED NE W PART P/N D55981442003002 B/N 0003855407 LOCATED AND DRILLED IA W SRM 51-44-21 INSTALED NEW PART IAW SRM 51-42-21/00SDR CALA2021120102201Skin · crackedHALF INCH CRACK AT LH HORIZONTAL STABILIZER LOWER SKIN AT STATIO N 129.5 APPROX. 1'' FROM LEADING EDGE (REF. AAR NR 99916788). REMOVED DAMAGE CRACK & REPAIRED AREA ON L/H HORZ LOWER SKIN AT S TA 129.5 APPROX. 1'' FORM LEADING EDGE IAW B737-800 SRM 55-10-01- 2RSDR CALA2021111802130Skin · noneREMOVE EXISTING REPAIR DOUBLER FOR HORZ STAB RIB REMOVAL ACCESS STA 92.70, INSTALL NEW DOUBLER WHEN WORK IS DONE. (REF AAR NR 9636811) PER TABLE 204. REMOVED EXISTING REPAIR FOR ACCESS, FABRICATED AND INSTALLED NEW DOUBLER REPAIR AT R/H HORIZ STAB LOWER SKIN ASDR CALA2021111802129Rib · cracked(EA 5510-01843 REV H OP 002) RH HOR. STAB INSPAR RIB AT STAB STA 92.70 STIFFENER #1 I/B SIDE OF RIB AT HORIZONTAL FLANGE CRACKED (REF AAR NR 9636620) REMOVED, REPAIRED AND REINSTALLED R/H HORIZ STAB RIB STA 92.70 AS PER B737-900 RES-WI 2017752-9 AND SRM 55-10-SDR 2021FA0000319Skin · corrodedCORROSION ON HORIZONTAL STAB LH UPPER AND LOWER SKINS JUST FWD OF CLOSE-OUT PANEL 351AC. REFERENCE TEXTRON AVIATION ENGINEERING MEMO DQ32437 DATED 13NOV2021.SDR 2021FA0000318Skin · corrodedCORROSION ON HORIZONTAL STAB RH UPPER AND LOWER SKINS JUST FWD OF CLOSE-OUT PANEL 352AC. REFERENCE TEXTRON AVIATION ENGINEERING MEMO DQ32438 DATED 13NOV2021.SDR 2021FA0000317Skin · corrodedHORIZONTAL STAB LH LOWER SKIN HAS 2 AREAS OF CORROSION AT TRAILING EDGE OF SKIN. REFERENCE TEXTRON AVIATION ENGINEERING MEMO DQ32439 DATED 13NOV2021.SDR CALA2021110402035Skin · crackedRH HORIZ STAB LOWER INSPAR SKIN CRACKED AT STA 138.7 DIRECTLY AC ROSS FROM DRAIN HOLE.CRACK IS APPROX .500 IN LENGTH(ENDS OF CRAC K VERIFIED WITH EDDY CURRENT AND MARKED) REPEAT INSPECTIONS-DVI 9000 FLIGHT CYCLES AND EXTERNAL LFEC 9000 FLIGHT CYCLES REF 737NDTSDR SWAA2021112939406Access Panel · crackedCRACK SEAL - PLATE ACCESS PANEL 333AB AT LT HORIZONTAL STAB ; 2021-496780 / [01] REPLACED SEAL-PLATE ACCESS PANEL 333AB AT LT HORIZONTAL STABILIZER IAW SRM B737-700 51-40-02; [02] VERIFIED TASK COMPLETESDR CALA2021102601977Skin · crackedREF FLEET CYCLE NR #9790736 REF EA 5510-01843 REV H R/H HORIZONT AL STABLOWER SKIN AREA AT STA 147.90 FOUND TWO CRACK INDICATIONS DURING C SCAN INSP REPAIRED LOWER SKIN PER SRM 55-10-01 REPAIR 11. PLACE ON DIP INSPECTION THRESHOLD 56,000 TOTAL FLIGHT CYCLES DESDR MASA20220329130None · crackedCRACK ON RH/LH ANGLES BTW VERTICAL STAB AND EXTERNAL FUSELAGE (TAIL CONE STA 67.5%).
CORRECTIVE ACTION: RH/LH ANGLES BTW VERTICAL STAB AND EXTERNAL FUSELAGE (TAIL CONE STA 67.5%) WERE REPAIRED PER CRJ-900 SRM 55-31-00-201-001-A01SDR UIEA2021101902254Jumper · noneR/WING VARIABLE CAMBER LEADING EDGE # 17 ,18,20 AND 23 WITH BROKEN BONDING WIRES(<P><SPAN>REMOVED AND REPLACED R/W VARIABLE CAMBER JUMPER PER SWPM 20-20-10 .</SPAN></P>)SDR DALA2023081806756Unknown · unknownSHIP 5642 DTE MONITOR INSPECTION LOG REF ERA 594728-14. CORRECTIVE ACTION: REF ERA 594728-14.SDR CALA2021101401858Skin · crackedEA 5510-01843 REV H A-55 DOT 002, 2 CRACKS NOTED ON R/H LOWER HO RIZONTAL STAB SKIN ON RIB 6, STATION 129.5, 3" INBOARD OF PREVIO US REPAIR (REF. AAR NR 99911901). V935579). REMOVED DAMAGE CRACK & REPAINTED ARE ON R/H HORIZONTAL STAB LOWE R SKIN ALONG RIB 6 STSDR CALA2021101401855Skin · noneMRD ISSUED MRD *SAN 01-1305Z* FOR AIRCRAFT 0219 ISSUED ON 04OCT21 06:05:02 BY U308639 (COOPER, LEONARD) ON FLIGHT 2314 FROM SAN TO ORD. NO FURTHER MAINTENANCE ACTION NEEDEDSDR CALA2021101101852Skin · crackedEA 5510-01843 REV H CRACK NOTED ON R/H LOWER HORIZONTAL STAB ON RIB 9, STATION 157.1 AFT OF PREVIOUS REPAIR. (REF AAR RFD NR 99911902). INITIATE DIP FOR REINSPECTION THRESHOLD REF SRM 55-10-01-2R-11 STEP 5 TABLE 204 @ 56000 TOTAL CYC, DVI & LFEC @ 9000 CYC INT
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