JASC 5510
Service difficulty reports · 5,966
Reports filed under 5510 · Horizontal Stabilizer 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 = '5510' 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 = '5510' 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 04FDEA03155Structure · corrodedBARREL NUT BORE NR 28L. EXCEEDED LIMITS AFTER CORROSION REMOVAL. REPAIRED PER FEDEX EA 1-5510-79789.SDR 04FDEA03154Structure · corrodedBARREL NUT BORE NR 34R. EXCEEDED LIMITS AFTER CORROSION REMOVAL. REPAIRED PER FEDEX EA 1-5510-79789.SDR 04FDEA03153Structure · corrodedCORROSION REMOVED ON BARREL NUT BORE NR 7R EXCEEDED LIMITS. REPAIRED PER FEDEX EA 1-5510-79789.SDR 04FDEA03151Structure · corrodedCORROSION REMOVED ON BARREL NUT BORE NR 17R EXCEEDED LIMITS. REPAIRED PER FEDEX EA 1-5510-79789.SDR 04FDEA03149Structure · corrodedCORROSION REMOVED ON BARREL NUT BORE NR 1R EXCEEDED LIMITS. REPAIRED PER FEDEX EA 1-5510-79789.SDR 04FDEA03148Structure · corrodedCORROSION REMOVED ON BARREL NUT BORE NR 32L EXCEEDED LIMITS. REPAIRED PER FEDEX EA 1-5510-79789.SDR 04FDEA03147Structure · corrodedCORROSION REMOVED ON BARREL NUT BORE NR 24L EXCEEDED LIMITS. REPAIRED PER FEDEX EA 1-5510-79789.SDR 04FDEA03146Structure · corrodedCORROSION REMOVED ON BARREL NUT BORE NR 20L EXCEEDED LIMITS. REPAIRED PER FEDEX EA 1-5510-79789.SDR 04FDEA03145Structure · corrodedCORROSION REMOVED ON BARREL NUT BORE NR 16L EXCEEDED LIMITS. REPAIRED PER FEDEX EA 1-5510-79789, HORIZONTAL STABILIZERS BARREL NUT BORE REWORK/ REPAIR - 1-5510-7-5000SDR 04FDEA03144Structure · corrodedCORROSION REMOVED ON BARREL NUT BORE NR 2L EXCEEDED LIMITS. REPAIRED PER FEDEX EA 1-5510-79789.SDR ABXA040399Bearing · crackedRIGHT HORIZONTAL STAB PIVOT BEARING FOUND CRACKED IN HALF. REPLACED BEARING ON NR 0131 IAW DC-9 SRM.SDR 04FDEA03120Structure · corrodedBARREL NUT BORE NR 36R AFTER CORROSION REMOVAL FOUND EXCEEDED LIMITS. REPAIRED PER FEDEX EA 1-5510-79789.SDR 04FDEA03119Structure · corrodedBARREL NUT BORE NR 24R AFTER CORROSION REMOVAL FOUND EXCEEDED LIMITS. REPAIRED PER FEDEX EA 1-5510-79789.SDR 04FDEA03118Structure · corrodedBARREL NUT BORE NR 20 RT, AFTER CORROSION REMOVAL FOUND EXCEEDED LIMITS. REPAIR PER FEDEX EA 1-5510-79789.SDR 04FDEA03117Structure · corrodedBARREL NUT BORE NR 16R, AFTER CORROSION REMOVAL FOUND EXCEEDED LIMITS. REPAIRED PER FEDEX EA 1-5510-79789.SDR 04FDEA03116Structure · corrodedBARREL NUT BORE NR 27L. AFTER CORROSION REMOVAL FOUND EXCEEDED LIMITS. REPAIRED PER FEDEX EA 1-5510-79789.SDR 04FDEA03115Structure · corrodedBARREL NUT BORE NR 25L, AFTER CORROSION REMOVAL FOUND EXCEEDED LIMITS. REPAIRED PER FEDEX EA 1-5510-79789.SDR 04FDEA03114Structure · corrodedBARREL NUT BORE NR 23L, AFTER CORROSION REMOVAL FOUND EXCEEDED LIMITS. REPAIRED PER FEDEX EA 1-5510-79789.SDR 04FDEA03113Structure · corrodedBARREL NUT BORE NR 19L, AFTER CORROSION REMOVAL FOUND EXCEEDED LIMITS. REPAIR PER FEDEX EA 1-5510-79789.SDR 04FDEA03093Structure · corrodedCORROSION REMOVED ON NR 14 RT BARREL NUT BORE FOUND EXCEEDED LIMITS. FITTING REMOVED AND REPLACED (P/N ALC8106Y2) PER SRM 51-33-01 VOLUME II.SDR 04FDEA03092Structure · corrodedCORROSION REMOVED ON NR 26 RT BARREL NUT BORE FOUND EXCEEDED LIMITS. REMOVED AND REPLACED (P/N ALC8107Y2) PER SRM 51-33-01 VOLUME II.SDR SWAA043220Clevis · corrodedDURING SCHEDULED D-CHECK, FOUND RT AND LT HORIZONTAL STABILIZER FITTINGS FWD AND AFT SPAR CLEVIS LUGS CORRODED. REPAIRED HORIZONTAL STAB PER SRM.SDR USAA040905Attach Angle · crackedPIT - Q5 - ANGLE, 6 INCH LONG CRACK, HORIZ STAB CTR SECTION THRUST BEAM ATTACH ANGLE LT SIDE. REMOVED AND REPLACED ANGLE, REPLACED IAW TYP REP SRM 51-00-30. REMOVED AND REPLACED IAW TYP REP SRM 51-00-30.SDR CA041110015Reinforcement · cracked(CAN) HORIZONTAL STABILIZER WAS REMOVED TO ACCESS RT FUSELAGE SIDE SKIN REPLACEMENT (COSMETIC) WITH STABILIZER REMOVED VISIBLE ACCESS TO AFT FUSELAGE STRUCTURE REVEALED A CRACK AT THE LT AFT STABILIZER ATTACH LONGERON PN 0712207-1 - REF. CESSNA 180-C I.P.C. FISDR USAA040775Pin · corrodedPIT - C3, PIN ASSEMBLIES, 1 INCH BY 1 INCH AREA, CORROSION; NO LEVEL OR TASK. RT HORIZ HINGE PINS (INNER AND OUTER) HORIZ STAB. REMOVED AND REPLACED INNER AND OUTER HINGE PIN ASSY IAW EA 79359/ DRAFT EO 5502V025.SDR USAA040776Pin · corrodedPIT, C3, PIN ASSEMBLIES- 1INCH X 1INCH AREA, CORROSION; NO LEVEL OR TASK LT HORIZ HINGE PINS (INNER AND OUTER) HORIZ STAB. REMOVED AND REPLACED INNER AND OUTER HINGE PIN ASSY IWA WA 79359/ DRAFT EO 5502V025.SDR CA041027002Brake · contaminated(CAN) DURING DECENT, WHEN LEVELING AT 6000FT CREW EXPERIENCED DIFFICULTY IN CAPTURING ALTITUDE. PROBLEM WAS QUICKLY DETERMINED TO BE HORIZ STABILIZER TRIM. TRIM WHEEL WAS VERY STIFF TO MOVE BOTH MANUALLY AND ELECTRICALLY WHEN TRIMMING NOSE UP. AC LANDED WITHOSDR SWAA043039Fitting · corrodedDURING SCHEDULED D-CHECK, FOUND LEFT AND RIGHT HORIZONTAL STABILIZER FITTING FWD AND AFT SPARS CLEVIS LUGS CORRODED. REPAIRED HORIZONTAL STAB FITTING PER SRM.SDR QXEA200400722Pin · wornPDX - HORIZONTAL STAB HINGE BOLT PIVOT PINS HAVE STEPWEAR DAMAGE TO THE ANTI ROTATION LUGS. REPAIRED IAW HORIZON AIR EA R-53-23.SDR 04FDEA02895Fitting · crackedNR 26 RIGHT HAND BARREL NUT BORE FOUND CRACKED AT BOTTOM INBOARD SIDE AREA. NR 26 RIGHT HAND BARREL NUT BORE SPLICE FITTING REMOVED AND REPLACED AS PER SRM 51-33-01 VOL II.SDR 04FDEA02892Structure · corrodedTO COMPLY WITH FEDEX EA 1-5510-80350, TITLE: STABILIZERS - HORIZONTAL STABILIZER - MASTER EA - REWORK TO BARREL NUT BORES IN EXCESS OF FEDEX EO 1-5510- 7-5000 (BOEING SB MD11-55-023 REV 2.) FAA AD 2003-22-08 (AMENDMENT 39-13356). COMPLIED WITH FEDEX EA 1-55SDR 04FDEA02884Fitting · migratedLEFT HORIZONTAL STABILIZER INBOARD TRAILING EDGE, STABILIZER TO STABILIZER BOX SAFETY LINK, OUTBOARD ATTACH CLEVIS BUSHING WORN AND MIGRATED THROUGH STABILIZER LOWER INBOARD ACCESS PANEL 334MB. REMOVED FITTING FOR INSTALLATION OF REPAIR BUSHING IAW FEDEX DC10SDR 04FDEA02836Fitting · corrodedCORROSION REMOVED ON NR 14 LEFT HAND BARREL NUT BORE FOUND EXCEEDED LIMITS. FITTING REPLACED AS PER SRM 51-33-01 VOL 2.SDR CA041116004Hinge Bracket · loose(CAN) DURING COMPLETION OF SGB 55-02R1 STABILIZER ATTACHMENT HINGE BRACKET BOLTS FOUND LOOSE (TURN BY FINGERS).SDR CA040927009Attach Bracket · cracked(CAN) CRACK LOCATED ON THE REAR FACE OF THE LT STAB ATTACH BRACKET, THE CRACK PARALLELS THE OB ATTACH FLANGE (ANCHOR NUT ATTACH SIDE) FOR 1.3750. THE CRACK HAD STARTED AT THE TOP OF THE STAB ATTACH BRACKET AND HAD WORKED ITS WAY DOWN. THE CRACK ON THE BRACKET SDR 04FDEA02709Structure · corrodedCORROSION REMOVED ON NR 20 LT BARREL NUT BORE FOUND EXCEEDED LIMITS PER FEDEX EO 1-5510-7-5000-C3-PT1 FIG 03. EXCEEDED LIMIT BARREL NUT BORE NR 20L, REPAIRED AS PER EA 1-5510-81552.SDR 04FDEA02708Structure · corrodedCORROSION REMOVED ON NR 24 LT BARREL NUT BORE FOUND EXCEEDED LIMITS PER FEDEX EO 1-5510-7-5000-C3-PT1 FIG 03. CORROSION REPAIRED AS PER EA 1-5510-81561.SDR 04FDEA02707Structure · corrodedCORROSION REMOVED ON NR 28 LT BARREL NUT BORE FOUND EXCEEDED LIMITS PER FEDEX EO 1-5510-7-5000-C3-PT1 FIG 03. EXCEEDED LIMIT BARREL NUT BORE NR 28L, REPAIRED AS PER EA 1-5510-81548SDR 04FDEA02706Structure · corrodedCORROSION REMOVED ON NR 30 LT BARREL NUT BORE FOUND EXCEEDED LIMITS PER FEDEX EO 1-5510-7-5000-C3-PT1 FIG 03. EXCEEDED LIMIT BARREL NUT BORE NR 30L, REPAIRED AS PER EA 1-5510-81554.SDR 04FDEA02705Structure · corrodedCORROSION REMOVED ON NR 32 LT BARREL NUT BORE FOUND EXCEEDED LIMITS PER FEDEX EO 1-5510-7-5000-C3-PT1 FIG 03. EXCEEDED LIMIT BARREL NUT BORE NR 32L, REPAIRED AS PER EA#1-5510-81549.SDR 04FDEA02704Structure · corrodedCORROSION REMOVED ON NR 33 LT BARREL NUT BORE FOUND EXCEEDED LIMITS PER FEDEX EO 1-5510-7-5000-C3-PT1 FIG 03. EXCEEDED LIMIT BARREL NUT BORE NR 33L, REPAIRED AS PER EA 1-5510-81550.SDR 04FDEA02703Structure · corrodedCORROSION REMOVED ON NR 35 LT BARREL NUT BORE FOUND EXCEEDED LIMITS PER FEDEX EO 1-5510-7-5000-C3-PT1 FIG 03. EXCEEDED LIMIT BARREL NUT BORE NR 35L, REPAIRED AS PER EA 1-5510-81556.SDR 04FDEA02702Structure · corrodedCORROSION REMOVED ON NR 36 LT BARREL NUT BORE FOUND EXCEEDED LIMITS PER FEDEX EO 1-5510-7-5000-C3-PT1 FIG 03. REPAIRED AS PER EA 1-5510-81553, HORIZONTAL STABILIZER-BARREL NUT BORE 36L - REWORKED BEYOND S/B MD11-55-023 REV. 2 LIMITS.SDR 04FDEA02701Structure · corrodedCORROSION REMOVED ON NR 33 RT BARREL NUT BORE FOUND EXCEEDED LIMITS PER FEDEX EO 1-5510-7-5000-C3-PT1 FIG 03. EXCEEDED LIMIT BARREL NUT BORE NR 33R, REPAIRED AS PER EA 1-5510-81547.SDR 04FDEA02700Structure · corrodedCORROSION REMOVED ON 31R BARREL NUT BORE FOUND EXCEEDED LIMIT IAW EO 1-5510-7-5000 C3 PT1 FIG 03. RT HORIZONTAL STABILIZER, EXCEEDED LIMIT BARREL NUT BORE NR 31R, REPAIRED AS PER EA 1-5510-81555.SDR DHL2004801534Fitting · crackedEMPENNAGE, LT HORIZONTAL STABILIZER LWR FITTING CRACKED 1.000 AT XFS 60.000. REMOVED CRACKED FITTING IAW SRM 51-1-21 PG 1. PERFORMED ANTI-CORROSIVE TREATMENT AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING ON LT HORIZONTAL STABILIZER, XFS 60.000 WITHSDR DHL2004801533Fitting · crackedEMPENNAGE, RT HORIZONTAL STABILIZER LWR FITTING CRACKED 1.000, XFS 60.000. REMOVED CRACKED LWR FITTING IAW SRM 51-1-21 PG 1. PERFORMED ANTI-CORROSIVE TREATMENT AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING ON RT HORIZONTAL STABILIZER, XFS 60.000 IASDR 04FDEA02671Structure · corrodedCORROSION REMOVED ON NR 29 LEFT BARREL NUT BORE FOUND EXCEEDED LIMIT. SNRM N1061: CORROSION REPAIRED AS PER EA 1-5510-80355 HORIZONTAL STABILIZER. BARREL NUT BORE 29L. REWORKED BEYOND SB MD11-55-023 REV2 LIMIT.SDR 04FDEA02672Structure · corrodedCORROSION REMOVED ON NR 13 LEFT HAND BARREL NUT BORE FOUND EXCEEDED LIMIT.SDR CA040913004Hinge · crackedDURING A ROUTINE MX INSPECTION, CRACK WAS DISCOVERED ON THE STABILIZER TRIM HINGE ASSY, (PORT SIDE) P/N: F513-1. TOTAL TIME ON AIRFRAME (AND PART) WAS 802 HOURS. THE CRACK WAS LOCATED BETWEEN THE RADIUS OF THE HINGE ARM AND LIGHTENING HOLE OF HINGE BODY. RE
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