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.

SDR QXEA0001407Fitting · corrodedPDX- HORIZ STAB JUNCTION FITTING HAS A PIT ON THE LEFT HAND UPPER LUG, ON THE INBOARD SURFACE. REPAIRED IAW HORIZON AIR EA 4-55-212.May 5, 2000 · N498US · Fokker F28MK4000SDR ABXA000228Cap · crackedDURING C-CHECK, FOUND LEFT HORIZONTAL STABILIZER CAP CRACKED OUTBOARD OF ELEVATOR CONTROL VALVE. REPLACED CAP IAW DC9 SRM 51-30-5.May 2, 2000 · N909AX · Doug DC932FSDR CALA0000587Bracket · crackedCRACK IN RIGHT ANGLE BRACKET ON RIGHT HAND DETACHABLE SEGMENT OUTER SUPPORT ANGLE OF HORIZONTAL STABILIZER LEADING EDGE (23). CAP REPLACED PER SRM 51-71-00.Apr 29, 2000 · N17087 · Doug DC1030SDR UPS00832581Fitting · crackedINSPECTION TYPE:C-2, LT HORIZ STAB I/B FWD UPPER T-ANGLE FITTING CRACKED STA XFS 60.00. REMOVED, FAB AND INSTALLED FITTING IAW SRM 51-1-20D & 51-1-11.Apr 27, 2000 · N700UP · Doug DC871FSDR DL72K000818Mount · corrodedFACE-CORRODED CENTER AFT MOUNT PAD FOR TENSION TIE PLATE CORRODED ON TOP SURFACE. REMOVED DAMAGE WITHIN LIMITS AS PER SRM 55-30-50 FIG 801D. ROTO PEENED PER PS 900-4- NR 5. OK TO TREAT. REPAIRED PER SRM 55-30-50 FIG 801D.Apr 27, 2000 · N529DA · Boeing 727232SDR USAA000606Fitting · crackedCLT - FOUND FITTING/STABILIZER CRACKED 4.5 INCH, HORIZ STABILIZER CENTER SECTION AFT JACK SCREW. REMOVED AND REPLACED FITTING/STABILIZER PER SRM 51-10-02. (M)Apr 26, 2000 · N351US · Boeing 737301SDR SWAA000772Angle · crackedDURING SCHEDULED 1/4D CHECK, FOUND LT HORIZONTAL STAB VERTICAL T-ANGLE CRACKED, STA 230 AFT SIDE OF AFT SPAR. REMOVED AND REPLACED T-ANGLE PER SRM.Apr 24, 2000 · N667SW · Boeing 7373T5SDR TWAA0006426Plate · corrodedDURING CHECK-C MAINT, THE LT SIDE STABILIZER WRAP AROUND SEAL PLATE HAD SEVERAL SCREW HOLES WITH CORROSION. MADE DOUBLER PER SRM 53-01. REMOVED CORROSION BY SPOT FACING OUT HOLES PER SRM 53-01, PAGE 1B. INSTALLED DOUBLER OVER SPOT FACED AREA PER SRM 55-01, Apr 22, 2000 · N9306T · Doug DC983SDR CALA0000548Channel · bentLEFT HORIZONTAL STAB TRAILING EDGE SECTION HAT SECTION BENT (3 X 1). REMOVED AND REPLACED HAT CHANNEL PER SRM 51-30-2 AND 51-30-08.Apr 21, 2000 · N14831 · Doug DC982SDR AALA2000757Fitting · corrodedTUL - FOUND RIGHT HORIZ STABILIZER SUPPORT LUG PLATES ON VERTICAL STABILIZER CORRODED BEYOND LIMITS. REMOVED AND REPLACED ALL 4 RIGHT STABILIZER HINGE SUPPORT LUG PLATES SRM 51-01. (M)Apr 20, 2000 · N487AA · Doug DC982SDR 20000417SH013Fitting · crackedBOTH AFT INBOARD HORIZONTAL STABILIZER ATTACH POINTS CRACKED ABOVE BOLT HOLE. LEFT HORIZONTAL STABILIZER DOUBLER AT REAR SPAR ATTACH POINT CRACKED, MOST AFT CHANNEL OF REAR SPAR OF HORIZONTAL STABILIZER HAS A 1 INCH CRACK IN RADIUS FORWARD OF MOST OUTBOARD LApr 17, 2000 · N6960N · Cessna T210NSDR ASAA0080246Plate · corrodedOAK - DURING C-CHECK INSPECTION, THE RIGHT HINGE OUTBOARD LUG, INBOARD HINGE PLATE, VERTICAL-TO-HORIZONTAL STABILIZER AFT ATTACH WAS FOUND CORRODED AND PITTED. (M)Apr 12, 2000 · N932AS · Doug DC982SDR ASAA0080245Attach Fitting · corrodedOAK - DURING C-CHECK INSPECTION, THE RIGHT HINGE OUTBOARD LUG, INBOARD HINGE PLATE, VERTICAL-TO-HORIZONTAL STABILIZER AFT ATTACH WAS FOUND CORRODED AND PITTED. (M)Apr 12, 2000 · N932AS · Doug DC982SDR QXEA0001078Switch · chafedPDX - LEADING EDGE 51C TEMP SWITCH IS CHAFING ON PREVIOUS REPAIR. REMOVED AND REPLACED DOUBLER IAW FOKKER SRM 51-31-01 AND HORIZON AIR EA 4-55-204.Apr 6, 2000 · N494US · Fokker F28MK4000SDR AALA2000600Beam · corrodedTUL - FOUND HORIZONTAL STAB TRAILING EDGE BEAM RIGHT CORRODED 3 PLACES. INSTALLED NEW RIGHT HORIZONTAL STAB TRAILING EDGE BEAM SRM 53-10-1. (M)Apr 4, 2000 · N723AA · Boeing 727227SDR CA000516006Support Fitting · cracked(CAN) ON 1000 HOUR INSPECTION, NDT FOUND CRACK IN TAPER PIN ATTACH HOLE. SUSPECT OVERTORQUING OF PIN. NEW TORQUE ASSY. REPLACED.Apr 3, 2000 · Beech 100BEECHSDR AALA2000599Beam · corrodedTUL - FOUND UPPER HORIZON STAB TRAILING EDGE BEAM CORRODED AT ES 165.5. TRIMMED OUT AND REMOVED DAMAGE. FABRICATED 301.5 HD STAINLESS .063 INCH STRAP AND INSTALLED PER ESO11697 DATED 3/28/00. (M)Apr 3, 2000 · N723AA · Boeing 727227SDR 20000425SH042Skin · corrodedSEVERE CORROSION FOUND ON FORWARD INBOARD STABILATOR SPAR AND INBOARD RIB JUNCTION. FOUND AFTER REMOVING TOP SKIN TO REPLACE. (X)Mar 31, 2000 · N5542W · Piper PA28160SDR EIAA2000084Structure · corrodedEAC-MZJ - RIGHT HORIZONTAL STABILIZER UPPER SURFACE FROM FRONT SPAR TO REAR SPAR STA 143.6 TO TIP HAD AREAS OF CORROSION. REPAIRED PER ECRA 479-55-133-2. BLENDED CORROSION, REMOVED AND REPLACED FASTENERS, ROTO-PEENED REWORKED AREAS. ACCOMPLISHED REPAIR AT SMar 30, 2000 · N479EV · Boeing 747132SDR QXEA0000970Structure · corrodedPDX - LEFT-HAND UPPER LUG ON HORIZONTAL STABILIZER DRIVE FITTING HAS AREAS OF FRETTING CORROSION. REPAIRED IAW HORIZON AIR EA 4-55-201 AND FOKKER SRM 51-10-4.Mar 28, 2000 · N487US · Fokker F28MK4000SDR 20000425SH003Stop · damagedBROKEN FLANGE AT .250 INCH - .254 INCH DIAMETER HOLE. REF: SAFF: SAUDI ARABIAN AIRLINES. (X)Mar 24, 2000 · Doug MD9030SDR 20000425SH002Stop · damagedBROKEN FLANGE AT .250 INCH - .254 INCH HOLES. REF: SAFF: SAUDI ARABIAN AIRLINES. (X)Mar 24, 2000 · Doug MD9030SDR 20000425SH001Stop · damagedBROKEN FLANGE AT .250 INCH - .254 INCH DIAMETER HOLE. REF: SAFF: SAUDI ARABIAN AIRLINES. (X)Mar 24, 2000 · Doug MD9030SDR QXEA0000973Fitting · corrodedPDX - RIGHT-HAND LOWER LUG ON HORIZONTAL STABILIZER DRIVE FITTING HAS FRETTING CORROSION DAMAGE. REPAIRED IAW HORIZON AIR EA 4-55-201 AND FOKKER SRM 51-10-4.Mar 23, 2000 · N487US · Fokker F28MK4000SDR QXEA0000972Fitting · corrodedPDX - RIGHT-HAND UPPER LUG ON HORIZONTAL STABILIZER DRIVE FITTING HAS FRETTING CORROSION DAMAGE. REPAIRED IAW HORIZON AIR EA 4-55-201 AND SRM 51-10-4.Mar 23, 2000 · N487US · Fokker F28MK4000SDR QXEA0000971Structure · corrodedPDX - LEFT-HAND LOWER LUG ON HORIZONTAL STABILIZER DRIVE FITTING HAS FRETTING CORROSION DAMAGE. REPAIRED IAW HORIZON AIR EA 4-55-201 AND FOKKER SRM 51-10-4.Mar 23, 2000 · N487US · Fokker F28MK4000SDR QXEA0000969Angle · crackedPDX - CRACK IN VERTICAL CONNECTION ANGLE LEFT SIDE AT SPAR I AT HI-LOKS AND AT ANGLE RADIUS. REPAIRED IAW FOKKER SRM 55-31-00, PAGE 2, FIGURE 1.Mar 23, 2000 · N487US · Fokker F28MK4000SDR QXEA0000967Structure · corrodedPDX - HORIZONTAL STABILIZER JUNCTION FITTING LOWER LEFT-HAND LUG HAS FRETTING CORROSION ON INBOARD AND OUTBOARD SURFACES. REPAIRED IAW HORIZON AIR EA 4-55-202 AND FOKKER SRM 51-10-4.Mar 23, 2000 · N487US · Fokker F28MK4000SDR QXEA0000966Structure · corrodedPDX - HORIZONTAL STABILIZER JUNCTION FITTING UPPER RIGHT-HAND LUG HAS FRETTING CORROSION ON INBOARD AND OUTBOARD SURFACES. REPAIRED IAW HORIZON AIR EA 4-55-202 AND FOKKER SRM 51-10-4.Mar 23, 2000 · N487US · Fokker F28MK4000SDR QXEA0000965Structure · corrodedPDX - HORIZONTAL STABILIZER JUNCTION FITTING LOWER RIGHT-HAND LUG HAS FRETTING CORROSION ON INBOARD AND OUTBOARD SURFACES. REPAIRED IAW HORIZON AIR EA 4-55-202 AND FOKKER SRM 51-10-4.Mar 23, 2000 · N487US · Fokker F28MK4000SDR QXEA0000957Fitting · corrodedPDX - HORIZONTAL STABILIZER JUNCTION FITTING UPPER LEFT-HAND LUG HAS FRETTING CORROSION INBOARD AND OUTBOARD SURFACE. REPAIRED IAW FOKKER SRM 51-10-4 AND HORIZON AIR EA 4-55-202.Mar 23, 2000 · N487US · Fokker F28MK4000SDR FJTA00049261Bolt · crackedMQY - WHILE PERFORMING THE NDT PHASE OF CP/CP TASK 55-10-011 (NDT OF HORIZONTAL STABILIZER ATTACH BOLTS), A CRACK WAS DETECTED IN ONE BOLT (P/N 137367F9). THE CRACK WAS DETECTED JUST BELOW THE BOLT HEAD TO LOAD BEARING SURFACE. ALL FOUR ATTACH BOLTS WERE REPMar 20, 2000 · N926AE · Bag JETSTM3201SDR QXEA0000974Fitting · corrodedPDX - SURFACE CORROSION ON HORIZONTAL STABILIZER DRIVE FITTING SKIN. REPAIRED IAW HORIZON AIR EA 4-55-199.Mar 16, 2000 · N487US · Fokker F28MK4000SDR ASAA0080198Support Bracket · damagedSEA - DURING MAINTENANCE INSPECTION, THE RIGHT SUPPORT FOR THE HORIZONTAL STABILIZER FAIRING WAS FOUND WITH AN OBLONG HOLE AT THE NUTPLATE. REPAIRED PER EA 5510-01094. (M)Mar 14, 2000 · N935AS · Doug DC982SDR DL72W000503Hinge · corrodedTHE I/B LUG OF THE HORIZONTAL STABILIZER PIVOT HINGE AT LBL 10 WAS FOUND WITH CORROSION IN THE HOLE BORE AND ON THE I/B FACE OF THE LUG. THE BORE WAS OVERSIZED AND THE FACE LIGHTLY SPOTFACED TO REMOVE THE CORROSION. THE LUG WAS REPAIRED WITH A REPAIR BUMar 11, 2000 · N291WA · Boeing 727247SDR RRXA002357Structure · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE AT SCREW HOLES ON THE RT O/B HORIZONTAL STAB LEADING EDGE I/B AT STA XFS 185 TO 187, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTAMar 9, 2000 · N995CF · Doug DC862SDR SWAA000431Lug · corrodedDURING SCHEDULED D-CHECK, FOUND LT HORIZONTAL STAB AFT SPAR UPPER LUG FWD FACE CORRODED. REPAIRED LUG PER ERO NR 00-0178PS AND ACO 6513-55.Mar 7, 2000 · N82SW · Boeing 7372H4SDR UPS00832118Fairing · chafedINSPECTION TYPE: C123, RT UPPER HORIZONTAL FILLET PANEL IS CHAFED. REMOVED DAMAGE, FOUND TO EXCEED LIMITS PER DC8 SRM 55-2-0. FABBED DOUBLER PER DC8 SRM 55-2-0. ALODINED & PRIMED PER DC8 SRM 51-1-8. INSTALLED PER DC8 SRM 51-1-21.Mar 6, 2000 · N804UP · Doug DC873FSDR CALA0000259Angle · crackedINSPECTION FOUND A 10 INCH CRACK IN HORIZONTAL STABILIZER RIGHT I/B LEADING EDGE I/B ANGLE AT XHR 9.652. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-02, 51-30-05, 51-10-04, AND 51-30-01.Mar 4, 2000 · N37882 · Doug DC981SDR RRXA002398Finger Doubler · damagedDURING A MAINTENANCE VISIT FOUND A RIVET PULLED THROUGH THE FINGER DOUBLER ON THE LT HORIZ STAB REAR SPAR ACCESS AT STA 221, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED Mar 2, 2000 · N995CF · Doug DC862SDR TSAA0055089Beam · corrodedHORIZONTAL STABILIZER UPPER AND LOWER TRAILING EDGE BEAM FOUND CORRODED. REPAIRED IAW ECO 1979 R4. AIRCRAFT RETURNED TO SERVICE. (M)Feb 28, 2000 · N809AL · Boeing 7372Q9SDR HEEA066552Support · crackedSUPPORT CRACKED IN BEND RADIUS ON FORWARD.Feb 28, 2000 · N437PH · Bell 407SDR QXEA0000736Fitting · corrodedPDX- HORIZONTAL STABILIZER DRIVE FITTING LOWER LEFT HAND LUG HAS PITTING CORROSION ALONG UPPER HALF. REPAIRED IAW HORIZON AIR EA 4-55-191.Feb 25, 2000 · N478US · Fokker F28MK4000SDR QXEA0000735Fitting · corrodedPDX- HORIZONTAL STABILIZER DRIVE FITTING LOWER RIGHT HAND LUG INBOARD FACE HAS PITTING CORROSION 2 PLACES. REPAIRED IAW HORIZON AIR EA 4-55-191.Feb 25, 2000 · N478US · Fokker F28MK4000SDR UPS00832039Angle · crackedINSPECTION TYPE:C123 LEFT H-STAB L/E INBD SIDE ANGLE IS CRACKED AT XFS 47. REMOVED AND REPLACED ANGLE IAW DWG 3701427, AND SRM 51-1-20D, 51-1-21.Feb 24, 2000 · N706UP · Doug DC871FSDR QXEA0000740Fitting · corrodedPDX- HORIZONTAL STABILIZER JUNCTION FITTING LOWER LEFT HAND LUG INBOARD FACE HAS CORROSION PITTING ONE PLACE UPPER. REPAIRED IAW HORIZON AIR EA 4-55-190, REFERENCE 49302 FOR RE-ASSEMBLY.Feb 24, 2000 · N478US · Fokker F28MK4000SDR QXEA0000739Fitting · corrodedPDX- HORIZONTAL STABILIZER JUNCTION FITTING UPPER LEFT HAND LUG INBOARD FACE HAS PITTING CORROSION 1 PLACE AFT. REPAIRED IAW HORIZON AIR EA 4-55-190, REFERENCE 4-302 FOR RE-ASSEMBLY.Feb 24, 2000 · N478US · Fokker F28MK4000SDR QXEA0000738Fitting · corrodedPDX- HORIZONTAL STABILIZER JUNCTION FITTING LOWER RIGHT HAND LUG INBOARD HAS PITTING CORROSION. REPAIRED IAW HORIZON AIR EA 4-55-190.Feb 24, 2000 · N478US · Fokker F28MK4000SDR QXEA0000737Fitting · corrodedPDX- HORIZONTAL STABILIZER JUNCTION FITTING UPPER RIGHT HAND LUG INBOARD FACE HAS PITTING CORROSION. REPAIRED IAW HORIZON AIR EA 4-55-190.Feb 24, 2000 · N478US · Fokker F28MK4000SDR USAA000244Angle · crackedCLT - ANGLE CRACKED AT STATION 1138 ON HORIZ STABILIZER. REPAIRED PER SRM 51-40-3 FIG 1. (M)Feb 22, 2000 · N260AU · Boeing 737201
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