JASC 5511
Service difficulty reports · 6,462
Reports filed under 5511 · Horizontal Stabilizer, Spar/Rib, 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 = '5511' 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 = '5511' 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 20000720SH037Stabilizer · crackedBOTH STABILIZER SPARS FOUND CRACKED IN THE UPPER BEND RADIUS FOR THE FLANGE AT THE INBOARD PAD ABOUT 2 INCHES FROM THE PADS. THIS AREA IS CONCEALED UNDER STIFFENER 0432001-15 (ALSO CRACKED). THIS WAS DISCOVERED DURING INSPECTION FOR AD 80-11-04, ALSO SPAR RESDR COMA0060516Rib · misdrilledMOUNT HOLES (AND 2 RIVETS) FOR HYDRAULIC LINE UNIONS IN OLD SPLIT VISOR FITTINGS (P/N 600-23070-9) AND (P/N 600-23070-10), NOT IN SAME LOCATIONS AS NEW VISOR FITTING (P/N 600-23070-13) AND (P/N 600-23070-14). HOLES LOCATED ON A/C INCORRECTLY, LOCATED DURING MSDR AALA20001041Spar · corrodedTUL - FOUND RIGHT HORIZONTAL CORRODED ON TOP REAR SPAR CHORD 20 INCHES FROM INBOARD END. INSTALLED DOUBELR PER ESO 11697, DATED 6-13-2000. (M)SDR UPS00433335Rib · crackedINSPECTION TYPE:C, TAIL CRACK IN LOWER CHORD ON RT HORIZONTAL STABILIZER T/E RIB AT STAB BL 380. NEW RIB FABRICATED IAW E0145283 AND FITTED IAW SRM 51-30-02.SDR UPS00233147Spar · crackedINSPECTION TYPE:C+SI LT HOROZONTAL STAB, FRONT SPAR LOWER CHORD CRACKED @ LE STA 236 - 248. HFEC C/O IAW B727 NDT MANUAL, PT6, 51-00-00, FIG 4. CRACK ENDS MARKED BEFORE REPAIR AND POST DAMAGE REMOVAL. NO DEFECTS FOUND. REPAIR C/O IAW SRM 55-10-5SDR 20000628SH005Rib · bentDURING ANNUAL/100 HOUR INSPECTION, THE SECOND RIB OUTBOARD OF CENTER ON THE RT SIDE OF THE HORIZONTAL STABILIZER WAS FOUND BENT THROUGH THE LIGHTENING HOLES. POSSIBLE CAUSE OF THIS DAMAGE, IMPROPER GROUND HANDLING (SITTING ON STABILIZER TO TURN AIRCRAFT). (XSDR AWXA0000395Spar · damagedLEFT HORIZONTAL STABILIZER LEADING EDGE SPAR HAS PREVIOUS TEMPORARY REPAIR. PERFORM PERMANENT REPAIR. REMOVED LEADING EDGE, CUT OUT DAMAGED AREA FROM UPPER SPAR CHORD IAW SRM 55-10-10. FABRICATED PARTS AND INSTALLED IAW 55-10-10, 51-20-02, 51-40-02.SDR CALA0000758Spar · gougedINSPECTION FOUND HORIZONTAL STABILIZER FRONT SPAR LEFT UPPER AFT AND LOWER AFT BARREL NUT HOLE GOUGED. REPAIRED IAW EA 9-5510-2-A0697 AND ECRA 5511-01020.SDR 20000601SH025Doubler · crackedUPON DISCOVERY OF CRACKS IN SN 5078, INSPECTED BOTH SPAR CAPS ON SN 5062 AND DISCOVERED A CRACK ON THE LEFT SIDE SPAR CAP DOUBLER (JE15-15L). THE CRACK IS ADJACENT TO THE LOWER SIDE OF THE HORIZONTAL STABILIZER LEADING EDGE. EDDY CURRENT INSPECTION DID NOT RSDR 20000601SH024Doubler · crackedWHILE DISASSEMBLING THE TAIL FOR PERMANENT STORAGE, A CRACK WAS DISCOVERED ON THE LEFT AND RIGHT SPAR CAP DOUBLERS (JE15-15L AND JE15-15R) ON THE LOWER SIDE OF THE HORIZONTAL STABILIZER LEADING EDGE. EDDY CURRENT INSPECTION DID NOT REVEAL ANY DAMAGE TO ADJACESDR F3LA00105Rib · crackedDEN - DURING C-7 CHECK, INSPECTION REPORTED LT HORIZONTAL STABILIZER LEADING EDGE RIB CRACKED, FOURTH RIB FROM INBOARD END. MAINTENANCE REPAIRED CRACKED RIB PER SRM 51-40-3 AND SRM 51-10-1. (X)SDR UPS00832888Rib · crackedINSPECTION TYPE:C123, RIGHT HORIZONTAL STAB L/E LOWER RIB IS CRACKED AT XFS 116.25. REPAIRED IAW SRM 55-2-0 FIG 2.SDR UPS00832835Rib · crackedINSPECTION TYPE:C123, LEFT HORIZONTAL STAB L/E RIB IS CRACKED AT XFS141.25. REPAIRED RIB IAW SRM 55-2-0 FIG 2.SDR UPS00832767Rib · crackedINSPECTION TYPE:C123, RIGHT HORIZONTAL STAB L/E UPPER RIB IS CRACKED AT XFS 172.5. REPAIRED IAW SRM 55-2-0 FIG 2.SDR ASAA0080337Spar · crackedPHX - DURING 30K CHECK, FOUND CRACK AND BEND WAS FOUND IN LEFT HORIZONTAL STABILIZER REAR SPAR CAP AT STATION XHS 158. REMOVED AND REPLACED SPAR CAP IAW DC9 SRM 51-30-05. (M)SDR RRXA002697Frame · crackedDURING A MAINTENANCE VISIT FOUND A CRACKED UPPER LEFT I/B HORIZONTAL STAB L/E FR AT STA XFS 53.7, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 51-1-4, 51-1SDR RRXA002696Frame · crackedDURING A MAINTENANCE VISIT FOUND A CRACKED LOWER LEFT I/B HORIZONTAL STAB L/E FRAME AT XFS 53.7, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 55-2-0, 51-1-SDR TWAA0007704Rib · crackedDURING OP 16 MAINT CHECK ON LT HORIZ STAB LEADING EDGE ASSEMBLY, NUMBER 1 LEADING EDGE RIB, I/B END WAS CRACKED ON BOTTOM TRAILING EDGE, NUMBER 1 FROM I/B END. ACCOMP HIGH FREQ EDDY CURRENT ON END OF CRACK FOR CONTAINMENT PER 51-00-03 PART 6 OF NDT MANUAL. SSDR UPS00232837Spar · corrodedINSPECTION TYPE:C, CORROSION, LEFT HORIZONTAL STABILIZER, REAR SPAR, UPPER CAP, BALANCE PANEL BAY 4 STABILIZER STATION 155 - 190. CUT OUT DAMAGED SECTION, CORROSION FOUND OUT OF LIMITS. INSTALLED RE AIR IN ACCORDANCE WITH SRM 55-10-5 FIG 1, MATERIAL USED, 70SDR QXEA0001180Spar Cap · scratchedYYC- HORIZONTAL STAB SPAR CAP ANGLES HAVE LIGHT SCRATCHES. REPAIRED IAW DHC-8 RD 8-55-626.SDR AT0100151Spar Cap · crackedFOUND RIGHT HORIZONTAL STAB SPAR CAP CRACKED. STOP DRILLED CRACK AND INSTALLED DOUBLER IAW TIMCO SERVICE ORDER 151108-21080.SDR DL72S000748Stringer · crackedTPA E-2 LETTER CHECK, VERT STAB STR 10 L CRACKED AT STA 157.2. REPAIRED PER M/M 55-30-0 FIG 803.SDR ABXA000245Rib · crackedDURING D-CHECK, FOUND RIGHT HORIZONTAL STABILIZER OUTBOARD RIB CRACKED. REPLACED RIB IAW DC9 SRM 51-30-1.SDR DL72W000824Stringer · crackedFOUND DURING MV2 CORROSION VISIT NRC 64, 2 INCH CRACK IN STR S-8 AT FIN STA 157.200 INTERIOR VERTICAL STABALIZER LT SIDE. REPAIRED PER M/M 55-30-0.SDR CA000501029Spar · damaged(CAN) NO TEXTSDR GAIA00142Rib · crackedDURING HEAVY C-CHECK AT TIMCO/OSC, FOUND HORIZONTAL STABILIZER RIGHT LOWER FORWARD INBOARD CLOSURE RIB CHORD WAS FOUND CRACKED. REPAIRED IAW SB 727-55-81. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR DL73K000539Spar · corrodedCORROSION WAS FOUND ON THE FRONT AND REAR SPAR OF THE HORIZONTAL STABILIZER CENTER SECTION ATTACH FITTING. CORROSION WAS FOUND ON THE FORWARD AND AFT FACES AND IN THE BORE. THE DAMAGE WAS REMOVED, TREATED AND PAINTED PER ERA 334168-14 AT HMV.SDR AWXA0000131Frame · crackedRIGHT STAB SLIDER FAIRING FWD FRAME CRACKED AT STA 1056 STR 12R. REMOVED DAMAGED AREA IAW 737 SRM 53-10-00, FABRICATED REPAIR PARTS IAW 737 SRM 51-40-3 FROM (.063 2024T3 R732710, .071 2024T3 R700681). INSTALLED REPAIR PARTS IAW 737 SRM 51-40-3. INSTALLED FRSDR AWXA0000129Frame · crackedLT HORIZ STAB SLIDER FAIRING FWD FRAME CRACKED AT STA 1096 STR 12. REMOVED AND REPLACED FWD FRAME (NEW PART) IAW 737 SRM 51-30-2 AND 51-10-1.SDR ASAA0080192Spar Cap · damagedPHX - DURING 30K CHECK, FOUND AN ELONGATED LEADING EDGE CAP ATTACH FASTENER HOLE IN THE LEFT HORIZONTAL STABILIZER FORWARD LOWER SPAR CAP FLANGE AT STATION XHS=90. REPAIRED PER EA 5510-01093 AND EA 10-5510-0319. (M)SDR UPS00831921Rib · crackedINSPECTION TYPE:C123, RIGHT HORIZONTAL L/E RIB IS CRACKED AT XFS 135. REPAIRED IAW SRM 55-2-0 FIG 2.SDR AWXA0000099Rib · crackedRT HORIZ L/E HAS CRACKED RIB, NR 3 RIB O/B. REMOVED RIB IAW 737 SRM 51-30-2, FABRICATED REPAIR PARTS IAW 737 SRM 55-10-4 FIG 1 AND INSTALLED REPAIR DOUBLER IAW 737 SRM 55-10-1 AND 737 SRM 51-30-2.SDR RRXA002215Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE BOTTOM RIB ON THE LEFT I/B HORIZ STAB I/B LEADING EDGE FRAME AT XFS 166, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLERS SDR RRXA002214Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE I/B BOTTOM RIB ON THE LEFT I/B STAB LEADING EDGE FRAME AT XFS 172, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC-SDR AU000391Spar · cracked(AUS) HORIZONTAL STABILIZER SPAR CRACKED THROUGH ATTACHMENT BOLT HOLES (4 OFF). FOUND FOLLOWING TAIL ROTOR STRIKE INSPECTION ALTHOUGH IT IS SUSPECTED THAT THE CRACKS WERE ALREADY PRESENT.SDR RRXA000640Frame · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK AT THE LOWER L/E FORMER ANGLE LT HORIZONTAL STAB AT STA XFS 47, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED IAW DC-8 SRM 51-1-20D AND DAC DWG 5SDR 2000ZZZX307Stringer · misrepairedTWO EXISTING UNAPPROVED REPAIR CHANNELS ON THE LT HORIZONTAL STABILIZER UPPER PANEL AT STR 6 AT XHS 25 AND XHS 37. REPAIRED LT HORIZONTAL STABILIZER UPPER PANEL STRINGER AT XHS 25 AND XHS 37, L6 PER EIA ECRA 941-55-059-2.SDR 2000ZZZX305Rib · crackedDAMAGE TO THE XHS 86.00 RIB IN THE RT HORIZONTAL STABILIZER FORWARD UPPER END WHILE GAINING ACCESS TO AN UNCONFIRMED CRACK. CRACK WAS LATER FOUND TO BE AN ANOMALIE ONLY. REPAIRED RT HORIZONTAL STABILIZER RIB DAMAGE AT XHS 86 PER EIA ECRA 941-55-013-2 REV A.SDR UPS00831543Rib · crackedINSPECTION TYPE:C123, VERTICAL L/E RIB CRACKED AT FS 279.687. REPAIRED IAW SRM 55-2-0 FIG 2.SDR UPS00831542Rib · crackedINSPECTION TYPE:C123, VERTICAL L/E RIB WAS CRACKED AT FS 248.38. REPAIRED IAW SRM 55-2-0 FIG 8.SDR 2000ZZZX659Spar · damagedDURING SCHEDULED MAINTENANCE CHECK, THE RIGHT HORIZONTAL STABILIZER AFT SPAR BEAM WAS FOUND CRACKED. CAUSE OF FAILURE IS UNKNOWN AT THIS TIME. REPLACED AFT BEAM ASSEMBLY. CASA TECHNICAL SUPPORT WAS NOTIFIED. AIRCRAFT TC: 18,394. (X)SDR CA000215016Rib · cracked(CAN) THE LEFT INBOARD NOSE RIB WAS FOUND CRACKED ON THE HORIZONTAL STABLIZER.SDR DHL200071772DSpar · damagedAT D-CK, RT HORIZONTAL STAB REAR SPAR AREA, STAB STA 32.08, INT, RIVET DAMAGED AND SKIN CUT AT TOP INT SURFACE. CUTOUT DAMAGED AREA PER B727 SRM 51-10-1. INSTALLED FILLER AND DOUBLER REPAIR PER B727 SRM 51-40-2. REF: N/R 3406.SDR TSAA0155002Spar · gougedIDENTIFIED .035 INCH GOUGE AT RIGHT HORIZONTAL STABILIZER CENTER SECTION REAR SPAR UPPER CHORD AFT UPPER CLEVIS LUG DURING SSIP INSPECTION. REPAIRED BY 20:1 RATION BLEND OUT, CONFIRMED HFEC INSPECTION NO DEFECTS NOTED, CLEAN AND TREATED AFFECTED AREA. IAW ECSDR 0000601229Rib · crackedDURING M-CHECK, FOUND CRACK ON LOWER SKIN PANEL STRINGER NUMBER 12 OF HORIZONTAL STATION XE407 AT STRINGER RIB CLIP. REPAIRED PER EA 12-173332.SDR CA000120027Rib · cracked(CAN) LT HORIZONTAL STABILIZER TIP RIB WAS FOUND TO BE CRACKED AT AFT TOP CORNER. RIB WAS REPLACED.SDR SWAA992092Spar · crackedDURING SCHEDULED D-CHECK, FOUND RT HORIZONTAL STAB FRONT SPAR CHORD CRACKED, STA 57.93. REPAIRED SPAR CHORD PER ER NR 99-6467.SDR CALA9901646Spar · bentINSPECTION FOUND RT HORIZONTAL STABILIZER REAR SPAR U-CHANNEL BENT BETWEEN HINGE NR 4 AND NR 5. THE CHANNEL WAS REMOVED AND A NEW CHANNEL WAS INSTALLED IAW SRM 51-30-02 AND 51-30-08.SDR USAA991412Spar · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 1.5 INCH CRACK RIGHT HORIZONTAL STAB 1.25 INCH FORWARD OF AFT SPAR BETWEEN STAB STATION 96 AND 97.5. INSTALLED DOUBLER PER SRM 55-10-01. (M)SDR CALA9901600Spar · crackedINSPECTION FOUND A 3 INCH CRACK IN LEFT HORIZONTAL STABILIZER PANEL SIDE UPPER CHORD. THE CHORD WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 51-33-01.
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