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 TSAA9555162Beam · corrodedDURING HEAVY MAINTENANCE VISIT, LEFT HORIZONTAL STABILIZER TRAILING EDGE BEAM UPPER SURFACE FILIFORM CORROSION NOTED AT ES 94.07. REPAIRED PER ECO 1584R3. AIRCRAFT RETURNED TO SERVICE. (M)Aug 16, 1995 · N808AL · Boeing 7372T4SDR TSAA9555161Beam · corrodedDURING HEAVY MAINTENANCE VISIT, LEFT HORIZONTAL STABILIZER TRAILING EDGE BEAM UPPER SURFACE EXFOLIATION CORROSION NOTED AT ES 149.12. REPAIRED PER ECO 1584R3. AIRCRAFT RETURNED TO SERVICE. (M)Aug 16, 1995 · N808AL · Boeing 7372T4SDR TSAA9555160Beam · corrodedDURING HEAVY MAINTENANCE VISIT, LEFT HORIZONTAL STABILIZER TRAILING EDGE BEAM UPPER SURFACE EXFOLIATION CORROSION NOTED AT ES 176.64. REPAIRED PER ECO 1584R3. AIRCRAFT RETURNED TO SERVICE. (M)Aug 16, 1995 · N808AL · Boeing 7372T4SDR TSAA9555159Beam · corrodedDURING HEAVY MAINTENANCE VISIT, LEFT HORIZONTAL STABILIZER TRAILING EDGE BEAM UPPER SURFACE EXFOLIATION CORROSION NOTED AT ES 145. REPAIRED PER ECD 1584R3. AIRCRAFT RETURNED TO SERVICE. (M)Aug 16, 1995 · N808AL · Boeing 7372T4SDR UPS204128Hinge Fitting · corrodedWHILE IN FOR C-CHECK, MAINTENANCE FOUND THE LT NR 5 BALANCE PANEL FITTING TO BE CORRODED. MAINTENANCE REPLACED THE LT BALANCE PANEL HINGE FITTING IAW SRM 51-30-2 AND SRM 51-30-5.Aug 14, 1995 · N908UP · Boeing 72727CSDR 96ZZZM446Fitting · crackedDURING C-CHECK, FOUND HORIZONTAL STABILIZER FRONT SPAR RIGHT UPPER OUTBOARD FITTING INDICATES CRACK AT LUG HOLE. REMOVED BUSHING AT RIGHT UPPER OUTBOARD LUG. ACCOMPLISHED HFEC INSPECTION OF LUG HOLE, CRACK NOTED AT 7 O'CLOCK POSITION. REAMED LUG TO .8125 INAug 8, 1995 · N703DH · Boeing 72730CSDR 95FDEA01189T Angle · crackedLEFT STAB L/E 2ND RIB, REMOVED SECTION O/B WEB UPPER T-CHORD IS CRACKED ON INSIDE. REMOVED T-CHORD, INSTALLED NEW T-CHORD P/N ALC-7502-11, PER SRM 51-00-01.Aug 4, 1995 · N303FE · Doug DC1030FSDR 95FDEA01188T Angle · crackedRT STAB L/E 2ND RIB, O/B SECTION UPPER WEB T-CHORD IS CRACKED, ENTIRE LENGTH INSIDE. REMOVED T-ANGLE, INSTALLED NEW PART ALC7502-12, FEDEX SRM 51-00-01.Aug 4, 1995 · N303FE · Doug DC1030FSDR 95ZZZX4365Panel Assy · corrodedINSPECTION FOUND NR 10 HORIZONTAL STABILIZER BALANCE PANEL AND REAR PANEL HINGE MATING SURFACE HAD LIGHT CORROSION. HINGE, PN 65-26659-1-2. THERE WAS NO CORROSION COMPOUND IN NR 10 BALANCE PANEL BAY.Aug 2, 1995 · N352PA · Boeing 727225SDR 95ZZZX4364Panel Assy · corrodedINSPECITON FOUND NR 1 HORIZONTAL STABILIZER BALANCE PANEL AND REAR PANEL HINGE MATING SURFACE HAD LIGHT CORROSION. HINGE, P/N 65-26659-1-2. THERE WAS NO CORROSION COMPOUND IN NR 1 BALANCE PANEL BAY.Aug 2, 1995 · N352PA · Boeing 727225SDR 95FDEA01190T-Chord · crackedLT/STAB L/E 2ND REMOVED SECTION O/B WEB LWR T-CHORD IS CRACKED ON INSIDE 6. STOP DRILLED CRACK, FABRICATED SHIMS AND REPAIRED ANGLE AS PER EA 8-5510-25132.Jul 30, 1995 · N303FE · Doug DC1030FSDR UPS203914Chord · corrodedWHILE IN NAPLES, ITALY FOR C-CHECK, MAINTENANCE FOUND CHORD CORRODED. REPLACED IAW SRM 51-30-2, B727-5530-4601.Jul 27, 1995 · N935UP · Boeing 7271A7CSDR UPS203912Chord · corrodedWHILE IN NAPLES, ITALY FOR C-CHECK, MAINTENANCE FOUND CHORD IS CORRODED. REPLACED IAW SRM 51-30-2, B727-5530-4601.Jul 27, 1995 · N935UP · Boeing 7271A7CSDR UPS203911Chord · corrodedWHILE IN NAPLES, ITALY FOR C-CHECK, MAINTENANCE FOUND CHORD IS CORRODED. REPLACED IAW SRM 51-30-2, B727-5530-4601.Jul 27, 1995 · N935UP · Boeing 7271A7CSDR UPS203910Chord · corrodedWHILE IN NAPLES, ITALY FOR C-CHECK, MAINTENANCE FOUND CHORD IS CORRODED. REPLACED IAW SRM 51-30-2.Jul 27, 1995 · N935UP · Boeing 7271A7CSDR AALA951275Beam · corrodedTULE - FOUND CORROSION ON RT TRAILING EDGE HORIZONTAL STABILIZER BEAM. REPLACED TRAILING EDGE BEAM TOP OF HORIZONTAL STABILIZER, RT TRAILING EDGE. (M)Jul 18, 1995 · N716AA · Boeing 727227SDR TSAA9555133Beam · corrodedDURING HEAVY MAINTENANCE VISIT, DISCOVERED EXFOLIATION CORROSION ON RT HORIZONTAL STABILIZER LOWER T/E BEAM AT STRINGER 125, ELS 76.45. REPAIRED PER ECO1584R3. AIRCRAFT RETURNED TO SERVICE. (M)Jul 10, 1995 · N802AL · Boeing 7372S5CSDR 96ZZZM577Rib · corrodedDURING D-CHECK, RIB LEFT SIDE STATION 1354 INSIDE TORQUE BOX LOWER SURFACE OF LOWER ANGLE HAS CORROSION ON HORIZ STAB. REMOVED CORROSION AS PER SRM 51-10-6 MATERIAL LOSS .005. INSTALLED ANGLE REPAIR 2024-T3 .063 2 INCH BY 10 INCH AS PER SRM 51-40-3.Jul 9, 1995 · N727DH · Boeing 727228SDR USAA950831Le Web · crackedPIT - DURING Q-4/CX-6 CHECK INSPECTION, FOUND A .25 INCH CRACK RIGHT INBOARD WEB LEADING EDGE TO HORIZONTAL STABILIZER FROM SPAR. INSTALLED DOUBLER REPAIR IAW SRM 55-01 FIG 5. (M)Jun 30, 1995 · N808US · Doug DC981SDR DL72S953048Structure · crackedLIGHTENING HOLE, CRACKED AND BENT ABOVE AND TO THE LEFT OF THE ELEVATOR FEEL COMPUTER. REPAIRED PER SRM 55-10-4 PAGE 3 FIG 2. FOUND AT HMV.Jun 27, 1995 · N489DA · Boeing 727232SDR UPS203376Chord · crackedWHILE IN SI CHECK, MAINTENANCE FOUND CRACKED T-CHORD ON RT HORIZ STAB. UPPER SURFACE SKIN SUPPORT CRACKED AT ATTACH POINT OF NR 1 ELEV HINGE SUPPORT RIB (ACCESS THROUGH PANEL 9213). REMOVED AND REPLACED T-CHORD IAW SRM 51-30-2, 51-30-2, 51-30-5.May 26, 1995 · N919 · Boeing 72730CSDR UPS203289Balance Panel · corrodedWHILE IN C CHECK, MAINTENANCE FOUND CORROSION ON RT HORIZ STAB, NR 5 BALANCE PANEL DOUBLER. INSTALLED REPAIR PER SRM 51-30-2, 51-20-1, 55-20-2, 51-10-2, MM 27-30-21.May 21, 1995 · N946UP · Boeing 72725CSDR UPS203288Balance Panel · corrodedWHILE IN C CHECK, MAINTENANCE FOUND CORROSION ON LEFT HORIZ STAB, NR 5 BALANCE PANEL DOUBLER. INSTALLED REPAIR PER SRM 55-10-1, 51-30-2, MM 51-20-21, 51-20-00, 27-30-21.May 21, 1995 · N946UP · Boeing 72725CSDR DLL10952002Stiffener · crackedINTERNAL STIFFENERS CRACKED RT HORIZ LE PANEL 341C, FOUND DURING HMV. REPAIRED PER SRM 55-12-00 FIG 803.May 9, 1995 · N719DA · Lkheed 10113851SDR DLL10951999Stiffener · crackedINTERNAL STIFFENERS CRACKED LT HORIZ LE PANEL 331F, FOUND DURING HMV. REPAIRED PER SRM 55-12-00 FIG 803.May 9, 1995 · N719DA · Lkheed 10113851SDR DLL10951976Stiffener · crackedINTERNAL STIFFENER CRACKED RT HORIZ LE PANEL 341D, FOUND DURING HMV. REPAIRED PER SRM 55-12-00 FIG 803.May 9, 1995 · N719DA · Lkheed 10113851SDR DLL10951975Stiffener · crackedINTERNAL STIFFENER CRACKED LT HORIZ LE PANEL 331E, FOUND DURING HMV. REPAIRED PER SRM 55-12-00 FIG 803.May 9, 1995 · N719DA · Lkheed 10113851SDR DLL10951974Stiffener · crackedINTERNAL STIFFENER CRACKED RT HORIZ LE PANEL 341E, FOUND DURING HMV. REPAIRED PER SRM 55-12-00 FIG 803.May 9, 1995 · N719DA · Lkheed 10113851SDR DL72E951982Balance Board · crackedFOUND ON CV-2 CHECK, .8125 CRACK AT LT INBD BALANCE BOARD ACCESS PANEL 9114. REPAIRED AS PER 55-10-3 FIG 3.May 9, 1995 · N830WA · Boeing 727247SDR 95ZZZX2448Leading Edge · burnedON INITIAL INSPECTION, FOUND HORIZONTAL STABILIZER DE-ICE TEST WOULD NOT CYCLE FULL AMOUNT OF CYCLES AND WOULD SKIP. UPON FURTHER INVESTIGATION, FOUND LEFT HORIZONTAL STABILIZER BURNED ON UPPER OUTBOARD LEADING EDGE. REPLACED LEADING EDGE WITH NEW. OPERATIOMay 3, 1995 · N8239E · Beech 400BEECHSDR 95ZZZX2684Bracket · brokenOUTBOARD TAB OF BRACKET BROKE OFF AFTER ONLY 434 HOURS. THIS IS THE SECOND BROKEN BRACKET IN 2 YEARS. BROKEN AT RADIUS NEAR NUTPLATE AND RIVETS WHERE IT ATTACHES TO THE HORIZONTAL STAB REAR SPAR.May 1, 1995 · N9419G · Cessna U206ESDR 95ZZZX2438Stabilizer · bird nestDURING PRE-FLIGHT, PILOT NOTICED TWIG STICKING OUT OF TAILCONE. MAINTENANCE PERSONNEL REMOVED TAILCONE AND FOUND ENTIRE HORIZONTAL STABILIZER FILLED WITH BIRD'S NEST. STABILIZER WAS PART OF STABILATOR ASSY AND OUT OF BALANCE. INSPECTED 2 OTHER LIKE AIRCRAFTMay 1, 1995 · N6715D · Beech C23SDR DLL10951821Stiffener · crackedINTERNAL STIFFENERS CRACKED RT HORIZ LE PANEL 341A. FOUND DURING HMV INITIAL. REAIRED PER SRM 55-12-00 FIG 803.Apr 30, 1995 · N719DA · Lkheed 10113851SDR EGRA9535Stabilizer · debondedHORIZONTAL STABILIZER FOUND DEBONDED. STABILIZER SHIPPED TO KEYSTONE FOR REPAIR. REPAIRED DISBONDED STABILIZER IAW CMM SA4047-76-5 REPAIR PROCEDURE #2 FOR BOND SEPERATIONS AND REPAIR PROCEDURE #3 FOR SKIN PATCH REPAIR. REPAIRED STABILIZER RETURNED AFTER REPAIRApr 20, 1995 · N22CP · Skrsky S76BSDR CAL950334Fitting · crackedDHM - FITTING CRACKED ON HORIZONTAL STABILIZER CENTER SECTION, STATION 1121 BL 12R AFT END OF FITTING CRACKED .25 INCH. REMANUFACTURE NEW FITTING PER SRM 55-10-3. (W)Apr 20, 1995 · N16301 · Boeing 7373T0SDR DLL10952010Stiffeners · crackedINTERNAL STIFFENERS CRACKED LT HORIZ LE PANEL 331D. REPAIRED PER SRM 55-12-00 FIG 803.Apr 16, 1995 · N719DA · Lkheed 10113851SDR DLL10952009Stiffeners · crackedINTERNAL STIFFENERS CRACKED RT HORIZ LE PANEL 341F. REPAIRED PER SRM 55-12-00 FIG 803. FOUND AT HMV.Apr 16, 1995 · N719DA · Lkheed 10113851SDR DLL10952005Stiffener · crackedINTERNAL STIFFENER CRACKED IN LEFT HAND HORIZONTAL STABILIZER LEADING EDGE PANEL 331C. FOUND AT HMV, REPAIRED PER SRM 55-12-00 FIG 803.Apr 16, 1995 · N719DA · Lkheed 10113851SDR DLL10951899Stiffener · crackedINTERNAL STIFFENERS, CRACKED RT HORIZ L/E PNL 341B. REPAIRED STIFFENERS PER SRM 55-12-00 FIG 803.Apr 16, 1995 · N719DA · Lkheed 10113851SDR DLL10951898Stiffener · crackedINTERNAL STIFFENERS, CRACKED LT HORIZ L/E PNL 331B. REPAIRED PER SRM 55-12-00 FIG 803.Apr 16, 1995 · N719DA · Lkheed 10113851SDR DLL10951812Stiffeners · crackedINTERNAL STIFFENERS CRACKED LT HORIZ LE PANEL 331G. REPAIRED PER SRM 55-12-00 FIG 803, FOUND AT HMV.Apr 16, 1995 · N719DA · Lkheed 10113851SDR ASAA9510039Attach Lugs · corrodedSEA - DURING D-CHECK, CORROSION WAS FOUND ON THE FACES AND IN THE INTERNAL DIAMETER OF THE HORIZONTAL STABILIZER ATTACHMENT LUGS. REPAIRED PER EA 5510-01029 AND BOEING SB 737-55-1055. (Z)Apr 16, 1995 · N740AS · Boeing 737290CSDR 95ZZZX1908Bracket · crackedDURING ANNUAL INSPECTION, FOUND CRACK IN BEND RADIUS OF ONE FORWARD AND ONE AFT STABILATOR BALANCE ARM SUPPORT BRACKET ON STABILATOR. RECOMMEND REPLACEMENT OF THESE WITH LATER STEEL BRACKETS, PN 1732063-1 AND DASH 2, AND 1732064-1, AND DASH 2 PER CESSNA SEB 8Mar 22, 1995 · N51386 · Cessna 177RGSDR 95ZZZX1907Bracket · crackedDURING ANNUAL INSPECTION, FOUND CRACK IN BEND RADIUS OF ONE FORWARD AND ONE AFT STABILATOR BALANCE ARM SUPPORT BRACKET ON STABILATOR. RECOMMEND REPLACEMENT OF THESE WITH LATER STEEL BRACKETS, PN 1732063-1 AND DASH 2, AND 1732064-1, AND DASH 2 PER CESSNA SEB 8Mar 22, 1995 · N51386 · Cessna 177RGSDR 95ZZZX1412Channel · crackedDURING ANNUAL INSPECTION FOUND BOTH LEFT AND RIGHT CHANNELS CRACKED AND NUMEROUS WORKING RIVETS. REPLACED BOTH CHANNELS WITH NEW PARTS. RECOMMEND CLOSER INSPECTION EVERY 100 HOURS.Mar 6, 1995 · N6487E · Beech 58PSDR TSAA9555046Beam · corrodedDURING HEAVY MAINTENANCE VISIT, FOUND EXFOLIATION ON RT HORIZONTAL STABILIZER T/E BEAM UPPER CAP AT SS70 AND SS166. REPAIRED PER ECO 1584R3. AIRCRAFT RETURNED TO SERVICE. (Z)Mar 3, 1995 · N304AL · Boeing 7373Y0SDR ABXA9500145Barrel Nut · rustedDURING COMPLIANCE OF A.D. 82-06-02, FOUND HORIZONTAL STABILIZER CENTER BOX FRONT SPAR UPPER LEFT NR 2 BARREL NUT RUSTED. CLEANED AND TREATED BARREL NUT IAW DC-9 SRM 51-10-3.Mar 3, 1995 · N927AX · Doug DC915SDR ABXA9500144Retainer · looseDURING COMPLIANCE OF A.D. 82-06-02, FOUND HORIZONTAL STABILIZER CENTER BOX FRONT SPAR UPPER LEFT NR 2 BARREL NUT RETAINER LOOSE. SECURED BARREL NUT RETAINER AS REQUIRED IAW DC-9 SRM 51-10-3.Mar 3, 1995 · N927AX · Doug DC915SDR 95ZZZW353Chord · corrosionDURING D-CHECK, CORROSION AT UPPER T/E CHORD LOWER SIDE OUTBOARD END (LT STABILIZER). REMOVED CORROSION PER SRM 51-10-06, ALODINE AND PRIMED PER SRM 51-10-2, CORROSION OUT OF LIMITS, INSTALLED DOUBLER REPAIR PER SRM 5-10-6, REPAIR 2 INCHES BY 33 INCHES 2024-TFeb 20, 1995 · N741DH · Boeing 7272Q9SDR 95ZZZW516Bolt · corrodedNR 1 'A' FRAME UPPER BOLT RT STABILIZER SCRAPED DUE TO CORROSION AND RIDGE WEAR. REMOVED AND REPLACED BOLT AS REQUIRED IAW MM.Feb 17, 1995 · N246SS · Bag BAE146100A
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