JASC 5512
Service difficulty reports · 7,887
Reports filed under 5512 · Horizontal Stabilizer, 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 = '5512' 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 = '5512' 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 06FDEA1799Skin · corrodedFOUND LOWER SKIN OF RIGHT HORIZONTAL STAB HAS NUMEROUS AREAS OF CORROSION FROM STAB TIP TO IB END, FWD SPAR TO AFT SPAR. REPAIRED PER FED EX EA 7-5510-102242.SDR MALA060313Skin · dentedHAIL CONTACT DAMAGE ON LEFT HORIZONTAL STABILIZER CAUSED DENT IN UPPER ALUMINUM SKIN AT HS113, .025 INCH DEEP AND .703 INCH DIAMETER. LOCATED 6.5 INCHES AFT OF FWD EDGE OF SKIN PANEL. DAMAGE REPAIRED WITH BONDED DOUBLER IAW SAAB SRM SECTION 55-10-10 AND MESASDR MALA060290Skin · dentedHAIL CONTACT DAMAGE ON RIGHT AND LEFT HORIZONTAL STABILIZER CAUSED DENTS IN UPPER ALUMINUM SKIN. LEFT SIDE STA 95, .026 DEEP AND 1" DIA STA 76, .026 DEEP AND .5" DIA RIGHT SIDE STA 55, .029 DEEP AND 2" DIA STA 94, .013 DEEP AND 7/8" DIA STA 140, .019 DEEP ANDSDR 2006UALA00825Skin · crackedFOUND RT HORIZ STAB TE LWR SKIN CRACKED 1.5 INCHES LONG PARALLEL TO REAR SPAR APPROX 2.5 INCHES FWD OF CENTERLINE OF NR 1 BALANCE BAY.SDR MALA060288Skin · dentedHAIL CONTACT DAMAGE ON RIGHT HORIZONTAL STABILIZER CAUSED DENT IN UPPER ALUMINUM SKIN AT HS 38.58, .022 INCH DEEP AND 1.0 INCH DIAMETER. LOCATED 6.5 INCHES FORWARD OF ELEVATOR LEADING EDGE. DAMAGE REPAIRED WITH BONDED DOUBLER IAW SAAB SRM SECTION SRM SECTIONSDR MALA060287Skin · dentedHAIL CONTACT DAMAGE ON RIGHT HORIZONTAL STABILIZER CAUSED DENT IN UPPER ALUMINUM SKIN AT HS99.92, .025 INCH DEEP AND 0.640 INCH DIAMETER. LOCATED 11.5 INCHES FROM LEADING EDGE AND 36 INCHES FROM OB ELEVATOR HINGE POINT. DAMAGED REPAIRED WITH BONDED DOUBLER IASDR QXEA200601656Panel · damagedYYC C3 HORIZONTAL STAB, REBATE FOR PANEL OPENING 342BB, HAS KNIFE MARKS AROUND CIRCUMFERENCE. REPAIRED IAW DHC-8-400 SRM 51-14-00-350-803, 51-21-10-380-801, 51-25-100-370-801, RD 8/4-55-257 AND EA 6/55/137.SDR QXEA200601660Panel · damagedYYC C3 HORIZONTAL STAB, REBATE FOR PANEL OPENING 332BD, HAS KNIFE MARKS AROUND CIRCUMFERENCE AND SEALING PAD FALLING OFF. REPAIRED IAW DHC-8-400 SRM 51-14-00-350-803, 51-21-10-380-801, 51-25-10-370-801, RD 8/4-55-258, ISSUE 1 AND EA 6-55-138.SDR 2006UALA00831Panel · dentedLT HORIZ STAB LE PANEL DENTED ON BULLNOSE AT SEVERAL LOCATIONS INCLUDING STAB LE STA120 AND 134.SDR 2006UALA00829Skin · dentedFOUND RT HORIZ STAB DENTED APPROX 8 FT FROM I-B EDGE ON LEADING EDGE.SDR MALA060283Skin · damagedHAIL CONTACT ON RIGHT HORIZONTAL STABILIZER CAUSED DENT IN UPPER SPAR ALUMINUM SKIN AT HS59.92, .013 INCH DEEP AND 7/8 INCH DIAMETER. LOCATED 21.5 INCHES FROM THE LEADING EDGE. DAMAGE REPAIRED IAW SAAB SRM SECTION 55-10-10 AND MESABA EO#S55017.SDR MALA060282Skin · damagedHAIL CONTACT DAMAGE ON RIGHT HORIZONTAL STABILIZER CAUSED DENT IN UPPER INBOARD SPAR ALUMINUM SKIN AT HS91.92, .022 INCH DEEP AND 1 INCH DIAMETER. LOCATED 31.5 INCHES FROM THE LEADING EDGE. DAMAGE REPAIRED WITH BONDED DOUBLER IN ACCORDANCE WITH SAAB SRM SECTSDR MALA060281Skin · damagedHAIL CONTACT DAMAGE ON RIGHT HORIZONTAL STABILIZER CAUSED DENT IN UPPER INBOARD SPAR ALUMINUM SKIN AT HS115.92, .005 INCH DEEP AND 1 INCH DIAMETER. LOCATED 17.5 INCHES FROM LEADING EDGE. DAMAGE REPAIRED WITH BONDED DOUBLER IN ACCORDANCE WITH SAAB SRM SECTIONSDR MALA060280Skin · dentedHAIL CONTACT DAMAGE ON RIGHT HORIZONTAL STABILIZER CAUSED DENT IN UPPER INBOARD SPAR ALUMINUM SKIN AT HS147.92, .026 INCH DEEP AND 1 INCH DIAMETER. LOCATED 19 INCHES FROM THE LEADING EDGE. DAMAGE REPAIRED WITH BONDED DOUBLER IAW SAAB SRM SECTION 55-10-10 ANDSDR 06FDEA1600Skin · damagedRIGHT HORIZONTAL STAB LEADING EDGE SECTION FOUND DAMAGED AT STA XFS91.2.SDR 06FDEA1575Panel · puncturedPANEL 9117 HAS PUNCTURE ON LOWER SURFACE, I/B END. *S/D* REPAIRED PANEL 9117 PER FED EX EA 7-5510-96628.SDR ABXA060219Skin · corrodedLEFT INBOARD HORIZONTAL STABILIZER LEADING EDGE SECTION OUTBOARD UPPER SURFACE AT XSTA 177, HAD INTERGRANULAR CORROSION AT SCREW HOLE AREA. INSTALLED REPAIR AT LEFT INBOARD STABILIZER LEADING EDGE SECTION OUTBOARD UPPER SURFACE IAW REA D855-53575-MR, REV. B.SDR 06FDEA1550Panel · crackedDURING NDT INSPECTION, FOUND 4 PANEL CRACKED, HORIZ STAB ZONE. REPLACED PANELS ON CENTER BOX STABILIZER AND LT STABILIZER IAW EA #8-5510-93812. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F164297/N01297 AND IAW SB 55-16 FIG 5.SDR 06FDEA1517Panel · crackedDURING INSPECTION OF HORIZ STAB, INSP CONSTANT SECTION FOUND CRACK ON PANEL P/N 7207-1 POSITION 15. ACCOMPLISHED EA NR 8-5510-93811, REINSTALLED FAIRING IAW SB 55-16 AND IAW SRM 51-31-01 PAR 6 VOL 2.SDR S2G2006F00000Skin · corrodedFOUND PART TO SEVERLY CORRODED AND HAD SEPARATED, TO 2 RIBS. PROBABLE CAUSE: PAINT STRIPPER, RECOMMEND THROUGH CLEANING AFTER STRIPPING AN AIRCRAFT FOR PAINT. (K)SDR DU4R2006372Skin · tornNR 24794 FOUND RT HORIZ STAB. T/E UPPER SKIN TORN BOTH IB AND OB SIDE OF NR3 BALANCE BAY STAB. STA. 157 AND 195 AFT OF AFT SPAR. CUT OUT TORN SKIN OF RT HORIZ. STAB. T/E BOTH IB AND OB END OF NR3 BALANCE BAY. FABRICATED AND INSTALLED DOUBLERS 10.8 X 5.3 INCSDR ASAA0640448Doubler · crackedFOUND RT HORIZONTAL STAB LE BONDED DOUBLER IS CRACKED AT LE. REMOVED DAMAGE FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW ASA EA 5510 01236.SDR QXEA200601068Skin · dentedYYC - C4 LEFT HAND HORIZONTAL STABILIZER LOWER SKIN HAS TWO DENTS AT YH102 AND YH104.5, BETWEEN STRINGER 1 AND 2. REPAIRED IAW RD 8-55-1685, ISSUE 1.SDR QXEA200601659Panel · damagedYYC C3 HORIZONTAL STAB, REBATE FOR PANEL OPENING 335BB, HAS KNIFE MARKS AROUND CIRCUMFERENCE. REPAIRED IAW DHC-8-400 SRM 51-14-00-350-803 AND 51-25-10-370-801.SDR QXEA200601658Panel · damagedYYC C3 HORIZONTAL STAB, REBATE FOR PANEL OPENING 342EB, HAS KNIFE MARKS AROUND CIRCUMFERENCE AND SEALING PAD IS FALLING OFF. REPAIRED IAW DHC-8-400 SRM 51-14-00-350-803 AND 51-25-10-320-801.SDR QXEA200601661Panel · damagedYYC C3 HORIZONTAL STAB, REBATE FOR PANEL OPENING 332EB, HAS KNIFE MARKS AROUND CIRCUMFERENCE AND SEALING PAD FALLING OFF. REPAIRED IAW DHC-8-400 SRM 51-14-00-350-803, 51-21-10-380-801, 51-25-10-370-801, RD 8/4-55-258, ISSUE 1 AND EA 6-55-138.SDR QXEA200601657Panel · damagedYYC C3 HORIZONTAL STAB, REBATE FOR PANEL OPENING 342BD, HAS KNIFE MARKS AROUND CIRCUMFERENCE AND SEALING PAD IS FALLING OFF. REPAIRED IAW DHC-8-400 SRM 51-14-00-350-803 AND 51-25-10-370-801.SDR 06FDEA1334Skin · corrodedRT HORIZONTAL STABILIZER CORROSION REMOVAL DAMAGE IS OUT OF LIMITS AT RT STAB STA 120, .5 INCHES AFT OF THE LE SPAR AND FWD EDGE OF THE SKIN NECESSITATING A REPAIR FROM FEDEX NR N00382 (TAIL 5008). REPAIRED RT HORIZ STAB AT RT STAB STA 120, .5" AFT OF THE LSDR 06FDEA1333Skin · corrodedFOUND RT HORIZONTAL STABILIZER CORROSION REMOVAL DAMAGE IS OUT OF LIMITS AT RT STAB STA 116.5, 9.5 INCHES AFT OF THE LE SPAR AND FWD EDGE OF THE SKIN NECESSITATING A REPAIR FROM FEDEX NR N00382 (TAIL 5008). REPAIRED PER SRM 55-10-3.SDR 2006UALA00656Skin · crackedFOUND HORIZONTAL STAB LOWER SURFACE AFT SPAR SKIN CRACKED AT THIRD BAY FROM I-B END. REMOVED DAMAGE AND ACP NDT FOR CRACKS. FABRICATED AND INSTALLED REPAIR DOUBLER WITH TWO EACH CUT-OUT ACCESS HOLES REF SRM 55-10-01.SDR 2006UALA00651Skin · dentedRT HORIZ STAB LEADING EDGE DENTED APPROX 5 FT FROM FUSELAGE. DAMAGE REMOVED AND A FLUSH REPAIR WAS INSTALLED PER SRM 55-10-01 REPAIR NR 2.SDR ASAA0640387Skin · dentedLT VERTICAL STABILIZER LE HAS GROUP OF DENTS AT STAB STA 90. CUT OUT DAMAGE FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 55 10 01 FIG 201 REPAIR 2.SDR IXXA06RNG026SSkin · corrodedDURING ROUTINE C CHECK, FOUND CORROSION ON HORIZONTAL STABILIZER LOWER SKIN AT STATION XAR 0.00 TO REAR SPAR LEFT HAND. REMOVED CORROSION IAW DC8 SRM 51-1-8 PAGE 20. THICKNESS MEASUREMENT PERFORMED AND IT WAS FOUND OUT OF LIMITS IAW DC8 SRM 55-2-0 PAGE 12. SDR IXXA06RNG027SSkin · crackedDURING ROUTINE C CHECK, FOUND A CRACK ON THE RUDDER FAIRING SKIN DRAIN HOLE AT STATION ZR 81.625 LEFT HAND. DAMAGED SKIN SECTION WAS REPAIRED IAW EWO ATI 55-017 AND DOUGLAS DRAWING 5655074. THIS REPAIR CONSTITUTES A MINOR REPAIR.SDR SWAA061124Skin · crackedDURING SCHEDULED C3 CHECK, FOUND LT HORIZONTAL STAB LOWER SKIN CRACKED AT AFT SPAR, STAB STA 125. REPAIRED STAB PER SRM.SDR ABXA060215Skin · corrodedLEFT HORIZONTAL STABILIZER OUTBOARD LEADING EDGE UPPER STRUCTURE HAD INTERGRANULAR CORROSION ON AFT TRAILING EDGE FROM XFS 178 - 341. ACCOMPLISHED REPAIR OF LEFT HORIZONTAL STABILIZER LEADING EDGE IAW REA D855-53574-MR, REV. A.SDR ABXA060213Panel · corrodedRIGHT HORIZONATL STABILIZER LEADING EDGE OUTBOARD SECTION UPPER TRAILING EDGE INTERGRANULAR CORROSION AT 3 LOCATIONS: XFS260, 316 & 332. CUT OUT DAMAGED AREA AND INSTALLED REPAIR IAW REA D855-53089-MR, REV. B.SDR ABXA060211Skin · corrodedRIGHT HORIZONTAL STABILIZER INBOARD LEADING EDGE SECTION AT UPPER TRAILING EDGE MID AREA AT XSTA 140, HAD INTERGRANULAR CORROSION AROUND SCREW HOLES. INSTALLED REPAIR IAW REA D855-53086-MR, REV. A, ON RIGHT HORIZONTAL STABILIZER INBOARD LEADING EDGE SECTION ATSDR ABXA060212Panel · corrodedRIGHT HORIZONTAL STABILIZER OUTBOARD LEADING EDGE SECTION AT INBOARD UPPER LEADING EDGE HAD INTERGRANULAR CORROSION AT HILOC HOLE. INSTALLED REPAIR IAW REA D855-53090-MR, REV. IR AT RIGHT STABILIZER LEADING EDGE AT XSTA 178.75.SDR ABXA060192Skin · corrodedRIGHT HORIZONTAL STABILIZER LEADING EDGE OUTBOARD SECTION UPPER TRAILING EDGE HAD INTERGRANULAR CORROSION AT 3 LOCATIONS: XFS 260, 316 AND 332. CUT OUT DAMAGED AREA AND INSTALLED REPAIR IAW REA D855-53089-MR, REV B.SDR ABXA060191Skin · corrodedRIGHT HORIZONTAL STABILIZER LEADING EDGE OUTBOARD UPPER SKIN HAD INTERGRANULAR CORROSION AT XFS 178.750. CUT OUT DAMAGED AREA AND INSTALLED REPAIR IAW REA D855-53088-MR, REV A.SDR SWAA061073Skin · crackedDURING SCHEDULED C1 CHECK, FOUND LT HORIZONTAL STAB LOWER SKIN CRACKED AT AFT SPAR, STAB STA 125. REPAIRED HORIZONTAL STAB PER SRM.SDR SWAA061072Skin · crackedDURING SCHEDULED C1 CHECK, FOUND RT HORIZONTAL STAB LOWER SKIN CRACKED AT AFT SPAR BETWEEN STAB STA 96 & STAB STA 118. REPAIRED HORIZONTAL STAB PER SRM.SDR UPS06M46963Panel · corrodedINSPECTION TYPE:C HORIZ STAB POSITION NR R16 BARREL NUT BORE SIDEWALL AND BOTTOM FACE FOUND CORRODED. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 38, BORE REAMED TO 1.067" OD REMAINING BLEND OUT 0.025" DEEP AND EXCEED LIMIT. MAGNIFY DVI C/OUT FOUND NO CORROSDR ABXA060210Skin · corrodedRIGHT HORIZONTAL STABILIZER LEADING EDGE OUTBOARD UPPER SKIN HAD INTERGRANULAR CORROSION AT XFS 178.750. CUT OUT DAMAGED AREA AND INSTALLED REPAIR IAW REA D855-53088-MR, REV. A.SDR AWXA200600615Skin Panel · delaminatedGYR - DURING C08 CHECK DISCOVERED LOWER SKIN PANEL HORIZONTAL RIGHT HAND STABILIZER FORWARD FROM STAB STA 68.290 TO STA 224.249 LOWER SKIN OF PANEL APPROX 40 PERCENT DELAMINATED. MAINTENANCE REMOVED LOWER HORIZONTAL SKIN PANELS RIGHT SIDE. REPAIRED REF SRM 5SDR 06FDEA1151Skin · damagedLEFT HAND HORIZONTAL STABILIZER, CENTER PLANK UPPER SKIN AT STA XE=51.000 STRINGER 6, FOUND HOLE ELONGATED. COMPLIED WITH STEP 47 OF FEDEX EA 1-5510-94597.SDR 2006UALA00514Skin · gougedLT HORIZ STAB LEADING EDGE 70" FROM THE I/B END IS DENTED WITH A GOUGE. DAMAGE WAS REMOVED AND LEADING EDGE REPAIRED PER MM 27-41-21, SRM 55-10-01, GNMM 5-0-4-011, SRM 51-70-01, 55-70-01 AND MM 51-31-00.SDR 2006UALA00451Skin · dentedLH HORIZONTAL STAB UPPER SKIN DENTED 6 FEET FROM INBD. NEW REPAIR SKIN SPLICED IN PER AAR EA 1060102.SDR TAMF20060013SSkin · erodedDURING C-CHECK INSPECTION WAS FOUND A EROSION ON NOSE SKIN AT HORIZONTAL STABILIZER TIP - RT. DAMAGE WAS REPAIRED IAW EWO 767 55-002 AND BOEING SERVICE REQUEST ID: 1-171213467. ERODED AREA WAS CLEANED UP IAW SRM 55-10-30 PAGE 1 TO 3, THICKNESS MEASUREMENT PE
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