JASC 5522
Service difficulty reports · 3,272
Reports filed under 5522 · Elevator, Plate/Skin, 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 = '5522' 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 = '5522' 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 HEEA0013759Skin · corrodedELEV CORRODED THROUGH SKIN.SDR HEEA0013758Elevator · corrodedLT ELEV ASSY CORRODED THROUGH SKIN.SDR CA980421005Skin · damaged(CAN) DURING CRUISE IN STILL AIR, AIRCRAFT STRUCK BY LIGHTNING. IT APPEARS TO HAVE ENTERED VHF COMM ANTENNA ON FORWARD FUSELAGE BELLY. EXIT POINT WAS AT RIGHT ELEVATOR TRAILING EDGE. A SMALL AREA AT EXIT POINT WAS MELTED INTO A BLOB. THE AFT HALF OF THE ELSDR CA980403001Panel · dented(CAN) PILOT SNAGGED A STIFF ELEVATOR TRIM CONTROL. THE ELEVATOR TRIM LINK P/N 82760164-101 WAS CONTACTING THE ACCESS COVER WHEN THE ELEVATOR WAS MOVED TO THE FULL NOSE UP OR NOSE DOWN POSITION AND THE ELEVATOR TRIM WAS SET JUST OUT OF THE TAKE OFF POSITION IN SDR 98ZZZX1873Skin · corrodedPIN HOLE CORROSION WAS FOUND ON UPPER SKIN. FURTHER INVESTIGATION REVEALED SEVERE INTERIOR CORROSION. THE PART WAS REPLACED WTIH AN OVERHAULED ELEVATOR.SDR P5CA9800498Skin · crackedLEFT INBOARD ELEVATOR LOWER SKIN CRACKED. REPAIRED PER BOEING SRM 51-40-09.SDR DHL9872693DRivets · looseAT D CHECK, LT ELEVATOR LOWER SKIN HAS LOOSE RIVETS JUST AFT OF LOWER ACCESS PANEL. REPLACED ANGLE PER SRM 51-40-3, 1.25 BY 1.25 BY 18. N/R 4261.SDR MWEA98183Skin · misrepairedPREVIOUS REPAIR WAS NOTED ON THE LT ELEVATOR BETWEEN NOSE RIBS 8 AND 9 FROM OUTBOARD TIP REPAIR NOT IAW SRM. FABRICATED REPAIR DOUBLER IAW SRM 55-02.SDR P5CA9800391Panel · delaminationLT HORIZ STAB LOWER T/E FIXED PANEL 334GBL FOUND DELAMINATION. HOT BOND REPAIRED PER SRM 51-40-06 PARA 3.SDR P5CA9800292Skin · delaminatedDELAMINATION OF FIVE AREAS ON UPPER SURFACE OF THE RIGHT INBOARD ELEVATOR. FIBERGLASS REPAIR MADE PER BAC SRM 51-40-15.SDR P5CA9800287Skin · delaminatedDELAMINATION ON UPPER SURFACE OF LEFT INBOARD ELEVATOR. FIBERGLASS REPAIR MADE PER BAC SRM 51-40-15.SDR P5CA9800284Skin · delaminatedDELAMINATION ON SEVERAL AREAS OF THE RIGHT OUTBOARD ELEVATOR UPPER SURFACE. FIBERGLASS REPAIR MADE PER BAC SRM 51-40-15.SDR P5CA9800283Skin · crackedCRACK ON UPPER SURFACE OF LEFT INBOARD ELEVATOR. FIBERGLASS REPAIR MADE PER BAC SRM 51-40-15.SDR P5CA9800278Skin · delaminatedDELAMINATION ON SEVERAL AREAS OF LEFT OUTBOARD ELEVATOR UPPER SURFACE. FIBERGLASS REPAIR MADE PER BAC SRM 51-40-15.SDR P5CA9800433Skin · corrosionLEVEL 1 CORROSION ON THE LEFT OUTBOARD ELEVATOR UPPER SURFACE. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02.SDR CKSA98028Skin · damagedDUE TO WEATHER IN MIAMI AIRPORT SUCH AS HIGH WINDS, TORNADO'S AND FLYING DEBRIS, LT ELEVATOR AT STA XE 149.0 WEB SKIN FOR HINGE CUT OUT IS DAMAGED AND CRACKED. REMOVED DAMAGED SECTION OF SKIN AND FABRICATED NEW ONE AS PER SAMPLE USING SAME THICKNESS SAME MATESDR CKSA98027Skin · damagedDUE TO WEATHER IN MIAMI AIRPORT SUCH AS HIGH WINDS, TORNADO'S AND FLYING DEBRIS, LT ELEVATOR AT STA XE 221.0 WEB SKIN FOR HINGE CUTOUT IS DAMAGED AND CRACKED. REMOVED DAMAGED SECTION OF SKIN AND FABRICATED NEW ONE AS PER SAMPLE USING SAME THICKNESS SAME MATERSDR CKSA98026Skin · damagedDUE TO WEATHER IN MIAMI AIRPORT SUCH AS HIGH WINDS, TORNADO'S AND FLYING DEBRIS, LT ELEVATOR AT STA XE 272.0 WEB SKIN FOR HINGE CUTOUT IS DAMAGED AND CRACKED. REMOVED DAMAGED SECTION OF SKIN AND FABRICATED NEW ONE AS PER SAMPLE USING SAME THICKNESS SAME MATERSDR CKSA98025Skin · crackedDUE TO WEATHER IN MIAMI AIRPORT SUCH AS HIGH WINDS, TORNADO'S AND FLYING DEBRIS, LT ELEV HINGE CUT-OUT AT XE 77.000 SKIN EDGES CRACKED. REMOVED DAMAGED SECTION OF SKIN AND FABRICATED NEW ONE AS PER SAMPLE USING SAME THICKNESS SAME MATERIAL IAW SRM 55-4-1. OSDR MWEA98147Skin · corrodedDURING INSPECTION, FOUND LIGHT CORROSION ON EXTERIOR SURFACE OF LOWER SKIN ON RIGHT ELEVATOR XE 157.9. MTC REPAIRED IAW SRM 55-03 FIG 14 SHEET 2 AND SRM 51-30.SDR EISA98017Skin · crackedDURING C-CHECK, FOUND RIGHT ELEVATOR HAS CRACK AND HOLE IN BOTTOM SKIN, OUTBOARD END. FABRICATED DOUBLER PER SRM 55-20-03. (M)SDR DL72L980303Skin · crackedFOUND ON F1 LETTER CK 2.5 INCH CRACK ON, THE RT ELEVATOR LOWER SKIN AT THE FWD INBD END. REPAIRED PER MM 55-20-3.SDR DL72K980295Skin · damagedLOWER SKIN DAMAGED 58 INCHES FROM O/B END. REPAIRED PER SRM 55-20-3. NR 2895.SDR CALA9800167Skin · crackedINSPECTION FOUND A 2 INCH CRACK IN LT ELEVATOR SKIN AT PANEL NR 335FB. THE CRACK WAS STOP DRILLED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 55-10-00 AND 51-21-01.SDR CALA9800166Skin · corrodedINSPECTION FOUND LT INBOARD ELEVATOR UPPER TRAILING EDGE SKIN CORRODED. THE CORRODED AREA WAS CUT OUT, DOUBLERS, SPLICES, AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 55-10-00, 51-21-01, 51-31-01, AND 51-35-02.SDR 98ZZZX609Skin · crackedDURING RAMP INSPECTION, FOUND CRACK IN TOP SKIN JUST OUTBOARD OF OUTBOARD HINGE POINT. CRACK ALIGNED WITH CRACK IN SKIN P/N 96-610006-3. SUB-SURFACE STRUCTURE SHOWED NO DAMAGE, BUT CRACKED PAINT IN BALANCE WEIGHT ATTACH AREA INDICATES PREVIOUS STRESS. AIRCRSDR 98ZZZX608Skin · crackedDURING RAMP INSPECTION, FOUND CRACK IN TOP SKIN JUST OUTBOARD OF OUTBOARD HINGE POINT. CRACK ALIGNED WITH CRACK IN SKIN P/N 96-61006-49. SUB-SURFACE STRUCTURE SHOWED NO DAMAGE, BUT CRACKED PAINT IN BALANCE WEIGHT ATTACH AREA INDICATES PREVIOUS STRESS. AIRCRSDR DLM88980185Skin · damagedLT ELEVATOR UPPER AND LOWER SKIN AND REAR CLOSING CHANNEL WERE DAMAGED WHILE PERFORMING MAINTENANCE. REPAIRED PER ERA 331260-14.SDR ASAA9840015Skin · peelingSEA - DURING C-CHECK, A SMALL SECTION OF THE OUTER CARBON LAYER WAS FOUND PEELING ON THE LEFT ELEVATOR LOWER SURFACE NEXT TO THE 3RD HINGE CUTOUT FROM INBOARD END. REPAIRED PER EA 5520-01051 AND BOEING TELEX ASA-SEA-98-0010RR. (M)SDR P5CA9800190Skin · crackedCRACK ON AFT INBOARD CORNER OF LEFT INBOARD ELEVATOR. FIBERGLASS REPAIR ACCOMPLISHED PER BAC SRM 51-40-15.SDR 99ZZZX546Skin · delaminatedLEFT AND RIGHT DETACHABLE INBOARD ELEVATORS T/E DELAMINATED. APPLIED HOT BEND LAY-UP REPAIRS IAW MD-11 SRM 55-99-00, SHEET 3 FIG 1 AND SHEET 4 FIG 2.SDR MWEA98024Skin · misdrilledLT ELEV OBRD TRAIL EDGE HAS APPROX 1 QUARTER INCH COUNTER SINK HOLE. MTC REPAIRED IAW SRM 55-03 FIG 15.SDR MWEA98019Skin · gougedRT ELEV TRAILING EDGE HAS 3 DEEP GOUGES STA XHS158 AND 204.1. MTC REPAIRED IAW SRM 53-03 FIG 15.SDR DL72L980084Skin · damagedFOUND DURING F-1 LETTER CHECK, RIGHT ELEVATOR LWR SKIN DAMAGED O/B OF TAB CUTOUT. ALSO, RIGHT ELEVATOR REAR SPAR LWR LEG DAMAGED O/B OF TAB CUTOUT. SKIN REPAIRED PER 55-20-3 FIG 4. SPAR REPAIRED PER SRM 51-40-3 FIG 1.SDR DHL9880623CFairing · dentedAT C-CHECK, LEFT ELEVATOR AT ELEVATOR MOUNT FITTING CUTOUTS UPPER AND LOWER FAIRINGS DENTED, CRACKED AND BENT. STRAIGHTENED DEFORMITY, RESTORED TO ORIGINAL CONTOUR. TRIMMED CRACKED AREA, PERFORMED DYE PEN AND NO CRACK NOTED.SDR DL72S972619Skin · crackedFOUND DURING A-2 LETTER CHECK, 1.75 INCH CRACK IN RT ELEVATOR UPPER SKIN AT DOUBLER BETWEEN O/B 2 ELEVATOR HINGES. REPAIRED PER ERA 363435-14.SDR CA971216049Stiffener · cracked(CAN) TRAILING EDGE OF ELEVATOR SKIN FOUND SEPARATED. CLOSER EXAMINATION FOUND STIFFENER CRACKED AT RIVET HOLES AND BROKEN THROUGH IN 3 PLACES. INTERGRANULAR CORROSION FOUND ON STIFFENER. SKIN OK. AIRCRAFT TT: 13,469.SDR P5CA9701842Skin · tornTEAR AND DELAMINATION AT INBOARD AFT CORNER LEFT OUTBOARD ELEVATOR. REPAIRED PER BOEING SRM 51-40-15.SDR MWEA97841Skin · corrodedDURING C CHK, LT ELEV UPPER OUTBRD SKIN CORRODED UNDER OUTBOARD STATIC SWITCH MOUNTING. MAINTENANCE REPAIRED IAW SRM 55-20-1.SDR CALA9701602Skin · dentedINSPECTION FOUND RT ELEVATOR LOWER OUTBOARD SKIN DENTED. A DOUBLER REPAIR WAS INSTALLED IAW SRM 55-20-3. A CALCULATED BALANCE CHECK WAS ACCOMPLISHED IAW MM 51-80-7.SDR ABXA9701919Skin · crackedTHE RT ELEVATOR LWR SKIN AT STA XE 55.012 AND JUST FWD OF THE TRAILING EDGE IS CRACKED. THE CRACK IS APPROX 1.8 LONG. REPAIRED IAW DC8 SRM 53-2-1.SDR AU971548Skin · cracked(AUS) ELEVATOR SKIN OUTBOARD OF THE RH TRIM TAB FOUND WITH SMALL CRACK. WITH FIRM FORCE APPLIED TO THE TRAILING EDGE, THE CRACK OPENED UP TO 127MM (5IN) IN LENGTH. CLOSER INSPECTION REVEALED SEVERAL MORE CRACKS. CRACKING WAS INITIATED BY CORROSION. SUSPECT SKSDR DL72S972160Skin · cracked.5 INCH CRACK IN LOWER SKIN OF LT ELEVATOR 5 INCHES FROM I/B EDGE. REPAIRED PER SRM 55-20-3.SDR DL72S972154Skin · cracked.5 INCH CRACK IN LOWER SKIN OF LEFT ELEVATOR 5 IN FROM I/B EDGE. REPAIR PER SRM 55-20-3.SDR MWEA97804Skin · crackedDURING C-CHECK, FOUND CRACK IN RT ELEVATOR LOWER SKIN FWD OF SPAR AND OUTBOARD RIB AT STA XE101. MTC REPAIRED IAW DAC/BAC SVC ORD 0256/GLP AND SRM 51-10-3.SDR P5CA9701749Panel · delaminationDELAMINATED RT INBD ELEVATOR POWER CONTROL ACCESS PANEL NR 344. REPAIRED PER SRM 51-30-02, 51-24-11.SDR P5CA9701719Access Panel · delaminatedDELAMINATED POWER PAC ACCESS PANEL ON LT ELEVATOR. REPAIRED PER SRM 51-40-06.SDR P5CA9701713Skin · crackedA 4 INCH CRACK IN RT INBD ELEVATOR T/E. REPAIRED PER SRM 51-40-15 AND SRM 51-24-11.SDR DL72S972097Skin · damagedELEVATOR BONDED BEADED SKIN DAMAGED LT ELEVATOR STA 15 LWR SKIN 3RD AND 4TH BEAD. MFG AND SEALED REPAIR DOUBLERS, INSTALLED DOUBLERS REPAIRED PER SRM 55-20-3 PG 4 FIG 3.SDR 97ZZZX5116Elevator · damagedAFTER A HANGAR RASH INCIDENT, THE RIGHT ELEVATOR WAS BEING REPAIRED FOR DAMAGE TO THE FIBERGLASS TIP. AFTER REMOVAL OF THE TIP, THREE HOLES IN THE OUTBOARD TRAILING EDGE AREA OF THE SKIN WERE FOUND FILLED WITH BODY FILLER. THE FILLER WAS REMOVED AND AN ALUMI
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