JASC 5531
Service difficulty reports · 1,234
Reports filed under 5531 · Vertical 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 = '5531' 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 = '5531' 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 2002F00169Rib · crackedFOUND VERTICAL STAB LEADING EDGE PANEL NR 9545 HAS CRACKED RIB AT 85 INCH FROM LOWER END 9TH RIB. (M)SDR 2002F00165Rib · crackedFOUND VERTICAL STABILIZER LEADING EDGE PANEL NR 9545 HAS A CRACKED RIB AT 94 INCHES FROM LOWER END OF 10TH RIB. (M)SDR SWAA013264Spar · crackedDURING SCHEDULED D CHECK, FOUND VERTICAL FIN FRONT SPAR CRACKED AT SLING ATTACH POINT FASTENER HOLE. REPAIRED SPAR PER ER 01-5587.SDR LR7A01124Web · crackedDURING SCHEDULED C2 INSPECTION PER JOB CARD HSP5539 FOUND VERTICAL STAB REAR BEAM WEB CRACKED AT FS 1095, LBL 6, VSS 20.REPAIRED IAW SRM SMP 583-51-140-17. NR 2040.SDR 01FDEA00976Spar · chafedLEFT HAND VERTICAL STABILIZER MID SPAR CHORD CHAFED AT FIN STA 229. REMOVED AND REPLACED PER SRM 55-30-6 FIG 3.SDR 01FDEA00920Stringer · crackedVERTICAL STAB MAIN BOX INTERIOR STRINGER IS CRACKED AT FIN STA 110.4, STR 9 LT. REMOVED AND REPLACED STRINGER PER SRM 55-30-4 FIG 1 & EA 7-5530-59892.SDR 01FDEA00918Stringer · crackedVERTICAL STABILIZER MAIN BOX INTERIOR STRINGER IS CRACKED AT FIN BS 157.2, STR 8 RT. REMOVED AND REPLACED STRINGER PER SRM 55-30-4 & EA 7-5530-59891.SDR AUS20010934Spar · cracked(AUS) VERTICAL STABILISER REAR SPAR ASSEMBLY CRACKED IN TWO AREAS ADJACENT TO THE FUSELAGE BULKHEAD ATTACHMENT POINT.SDR 01FDEA01119Spar · chafedCHAFE AT VERT STAB L/E RIGHT FRONT SPAR FIN BS 55.8 TO 47.0 O/B SIDE. REMOVED AND REPLACED STAB PER IAW EA 7-5530-58486.SDR 0102622709Rib · corrodedDuring M check, found corrosion in the vertical stabilizer tension tie rib mount hole. Repaired per EA27-182234.SDR CALA0100500Spar · crackedINSPECTION FOUND A .5 INCH CRACK IN VERTICAL STABILIZER LT FRONT SPAR AT CANTED FRAME STA 1388. THE CRACK WAS LOCATED NINE INCHES UP FROM BOTTOM END. THE SPAR WAS REPAIRED IAW ECRA 5510-01581.SDR 01FDEA00374Spar · chafedVERTICAL STAB LT STR 7, MID SPAR CHORD IS CHAFED 3 inches IN FRONT OF SLIDING SEAL. *S/D* Removed and replaced PER FEDEX SRM 55-30-6 FIG 3, FEDEX EA 7-5530-54061.SDR 01FDEA00373Spar · chafedVERTICAL STAB, RT STR 7 MID SPAR CHORD IS CHAFED 3 inches IN FRONT OF SLIDING SEAL. *S/D* Removed and replaced PER FEDEX SRM 55-30-3 FIG 3, FEDEX EA 7-5530-54061.SDR IXXA0100061SSpar Cap · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED AT THE VERTICAL STABILIZER REAR SPAR LEFT HAND CAP AT STATION ZR 265. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED CAP. FABRICATION AND INSTALLATION OF NEW CAP IN ACCORDANCE WITH DOUGLAS STRUCTURAL REPAIR MANUASDR AU010369Spar Cap · cracked(AUS) VERTICAL STABILISER FORWARD RH SPAR CAP ANGLE LOCATED AT VS117.25 CRACKED IN THE AREA WHERE THE RIVETS ATTACH THE TOP RIB TO THEANGLE.SDR HEEA072582Spar · chafedSPAR INSIDE CHAFED FROM CONDUIT. REPLACED WITH SERVICEABLE PART.SDR QXEA0100616Rib · crackedYYC- VERTICAL STAB RIB 8 IS CRACKED ON THE RIGHT HAND SIDE. REPAIRED IAW HORIZON AIR EA 4-55-284.SDR 20010613CW024Spar · crackedFATIGUE CRACK OCCURRED ON RIGHT HAND VERTICAL FIN SPAR MEMBER APPROXIMATELY .5 INCH FORWARD OF THE 90 DEGREE GEARBOX ATTACH FITTING. THIS CRACK WAS DETECTED DURING COMPLIANCE OF AD. PROBABLE CAUSE: FATIGUE. REMOVED AND REPLACED VERTICAL FIN SPAR ASSEMBLY IASDR MWEA010487Spar Cap · misdrilledMISDRILLED HOLE GOING THROUGH SPAR CAP LEFT SIDE OF VERTICAL STABILIZER, BELOW HORIZONTAL STABILIZER LEADING EDGE. DRILLED HOLE, FABRICATED AND INSTALLED BUSHINGS.SDR 01FDEA00235Spar · chafedVERTICAL STAB MIDSPAR CHORD (STR 7) IS CHAFED, LT SIDE 3 INCHES FROM FRONT OF SLIDE SEAL FRONT TRACK. *S/D* REPAIRED AREA PER FEDEX SR 27-55-008.SDR 01FDEA00229Support Fitting · crackedN 650 DUR ROUTINE INSP, UPR AND LWR LUGS OF THE UPR RUDDER ROD SUPPORT FITTING LOCATED ON THE VERTICAL STABILIZER REAR SPAR FND CRACKED. ** S/D ** HFEC IND NO CRACKS PER IAW 727 NDT MANUAL PART 6.SDR 01FDEA00228Rib · crackedDURING ROUTINE INSP HFEC IND THE LWR RUDDER, THRUST HINGE RIB FITTING WAS CRACKED AT FWD RIGHT SIDE. *S/D* REMOVED AND REPLACED RUDDER THRUST HINGE RIB PER IAW FEDEX EO 7-5550-7-2303C PART 2.SDR EIA2001122Spar · corrodedMZJ-EAC - FOUND WEB AT FINS STATION 570, 39 INCHES FROM LE, AND WEB FORWARD SPAR AT FIN STATION 570 CORRODED. INSTALLED FRONT SPAR WEB REPAIR AT STATION 570 PER B747 SRM 55-30-05 FIG 1. REPLACED INBOARD L-CHORD AND WEB ON LE RIB AT STATION 570 PER B747 SRM 5SDR CALA0100207Rib · crackedINSPECTION FOUND RIG PIN HOLE BOSS CRACKED ON RIB WEB AT STA 56.48. THE CRACK WAS 2 INCHES LONG. AN INTERIM REPAIR WAS PERFORMED IAW ECRA 5530-01092. A PERMANENT REPAIR IS TO BE ACCOMPLISHED AT THE EARLIER OF 500 HOURS OR THE NEXT MX CHECK WHERE USE OF RIG SDR CALA0100193Rib · gougedINSPECTION FOUND L/E RIB OF VERTICAL STABILIZER GOUGED AT STA 10-40. THE DORSAL FIN RIB WAS REMOVED AND REPLACED IAW SRM 51-10-02.SDR 01FDEA00158Rib · crackedVERTICAL STAB, RT RIB CHORD IS CRACKED IN 3 PLACES AT FIN STA 133.8, STR 7 - 10R. *S/D* REMOVED, REPLACED AND FAB PER FEDEX SRM 55-30-5.SDR TWAA0102902Rib · crackedDURING CHECK-C MAINT NUMBER 3 AND 4 DORSAL FIN RIBS, FROM UPPER EDGE ON LT SIDE, WERE CRACKED. ROUTED AND RADIUSED END OF RIB. INSTALLED REPLACEMENT FILLER ON NUMBER 3 AND 4. INSTALLED 2024-T3 0.050 DOUBLER PICKING UP MINIMUM 3 ROWS OF FASTENERS BEYOND CRACKSDR AWXA0001305Rib · chafedAREA OF DEEP CHAFING ON VERT STAB FWD LWR END CAP RIB. REMOVED FWD LWR END CAP AND REPLACED WITH A NEW PART IAW SRM 53-10-11 AND 51-30-2.SDR DL72E010113Skin · crackedFOUND ON B2 LETTER CK, .25 INCH CRACK AND SHEARED RIVET AT BASE OF VERTICAL STAB AT STR 7 LT SIDE. REPLACED FASTENER AND REPAIRED PER B727DRD 55-30-3D.SDR 20010205CW016Rib · crackedDURNING ANNUAL INSPECTION , TAIL FIN FABRIC WAS FOUND BUCKLING APPROX 1 INCH AFT OF TOP LEADING EDGE. UPON FABRIC REMOVAL FOR HIDDEN DAMAGE INSPECTION THE FIN RIB WAS FOUND TO BE CRACKED AND BUCKLED AT FWD ATTACHING WELD. FURTHER INSPECTION REVEALED AFT ATTASDR ERKR200000004Spar · gougedEXISTING GOUGES ON THE AFT SURFACE OF THE LEFT HAND VERTICAL STABILIZER FRONT SPAR FITTING LUG. REPAIRED PER S/B 737-55-1028, ECRA N703S-55-B737-003-EAC. (X)SDR ERKR200000003Fitting · corrodedCORROSION VERTICAL REAR SPAR FITTING, LEFT SIDE OUTBOARD LUG AFT FACE OF FITTING. (X)SDR 20010209CW006Spar · corrodedUPON ANNUAL INSPECTION, FLAKING WAS NOTICED ON AFT SPAR AREA. FURTHER INSPECTION REVEALED THE SPAR WAS CORRODED .2500 THROUGH MAIN SURFACE. UNIT WAS REPLACED WITH AN AIRWORTHY ITEM.SDR L1GA200000381Skin · chafedCHAFING ON SKIN LT VERTICAL STAB WHERE VERT L/E MEETS HORTIZONTAL L/E. BLENDED, TREATED AND PRIMED.SDR 0004302296Chord · corrodedDuring "H" check fretting corrosion was found on the vertical flange of the vertical stablizer LH mid spar chord at STA FIN 228. Repaired per EA 22-178752.SDR 20001214SH006Spar Cap · crackedDURING ANNUAL INSPECTION, ''CREAKING'' WAS HEARD WHEN FORCE WAS APPLIED TO STABILATOR TIP TO CHECK FOR BEARING PLAY. SOURCE OF SOUND WAS FOUND TO BE WORKING RIVETS AND CRACKED SPAR CAP INSIDE CENTER SPAR BOX ASSY IN THE LOOSE RIVETS OR CRACK COULD BE SEEN BY SDR AT0000475Frame · corrodedFOUND VERTICAL STABILIZER LEADING EDGE UPPER KNEE CUP HAS CORROSION. REMOVED AND REPLACED VERTICAL STABILIZER LEADING EDGE HORSESHOE FORMER IAW DC9 SRM 51-10-02, 51-10-3, 51-10-4, 55-31-0 FIGURE 4.SDR QXEA0003019Spar · crackedPDX- CRACK IN CASTELLATION AT LEFT EDGE OF VERTICAL STABILIZER SPAR AND FRAME 32-2 HAS PROGRESSED PAST STOP DRILL. REPAIRED IAW FOKKER SRM 53-10-5.SDR C2XA00IA383Skin · crackedDURING C-CHECK INSPECTION THE LEFT HAND SKIN ON THE VERTICLE STABILIZER WAS FOUND TO BE CRACKED. THIS SDR FILED OPEN AWAITING FINAL CORRECTIVE ACTION.(CLOSED BY C2XA00IA394)SDR QXEA0002397Skin · damagedPDX- ROW OF RIVETS PULLED THROUGH SKIN AT TOP END OF LEFT HAND NUMBER 2 INTERMEDIATE SPAR OF VERTICAL STABILIZER. REPAIRED IAW FOKKER SRM 51-31-01 AND HORIZON AIR EA 4-55-253.SDR QXEA0002396Skin · damagedPDX- ROW OF RIVETS PULLED THROUGH SKIN AT TOP END OF RIGHT HAND NUMBER 2 INTERMEDIATE SPAR OF VERTICAL STABILIZER. REPAIRED IAW FOKKER SRM 51-31-01 AND HORIZON AIR EA 4-55-253.SDR 00FDEA00592Rib · corrodedDURING ROUTINE INSP, VERTICAL FIN TENSION TIE RIB BUSHING FOUND CORRODED AT LEFT AFT HORIZONTAL BOLT. REMOVED AND REPLACED VERTICAL FIN TENSION TIE RIB BUSHING PER IAW BOEING OHM 20-50-03.SDR DL72W001673Stringer · crackedA 1 INCH CRACK IN VERT STAB Z ANGLE STR S-8 LT SIDE IN TUNNEL, STA 157.2. REPAIRED PER 727 M/M 55-30-0 FIG 802.SDR QXEA0002245Skin · gougedPDX- RIGHT HAND VERTICAL STABILIZER SKIN HAS A GOUGE BETWEEN SPARS 2 AND AFT ON RIB 304. REPAIRED IAW FOKKER SRM 51-10-4 AND SRM 55-01-01.SDR TWAA0013410Rib · crackedDURING OP 15 MAINT CHECK ON THE VERTICAL STABILIZER LOWER LEADING EDGE SECTION HAD 3 CRACKED RIBS ON INTERIOR. INSTALLED REPAIR ANGLE DOUBLERS PER SSRM 55-30-102, PAGE 202.SDR DL72S001419Stringer · crackedAT MIDVISIT STRINGER 9L AT RIB NR 2 WAS FOUND TO BE CRACKED. STOP DRILLED CRACK PER MM 55-30-0 PG 803. BEGAN FAB DOUBLER PER MM 55-30-0, CHEM TREATED PER PS 900-2-4-1 NR 2 INSTALLED DOUBLER PER MM 55-30-0 FIG 803.SDR P2EA00218Rib · dentedYYC - DURING C-CHECK, WHILE REMOVING THE VERTICAL STAB, THE VERTICAL STAB WAS DAMAGED AT THE FORWARD RIB WEB BS 1007 UPPER END RESULTING IN A DENT 3 INCHES LONG, 4 INCHES WIDE, .250 INCHES DEEP. REPAIRED THE VERTICAL STAB FORWARD RIB WEB BS 1007 UPPER END IAWSDR 0002352292Rib · crackedDURING H CHECK FOUND CRACK IN THE VERTICAL STABILIZER ON THE NR 2 RIB AT THE NR 3 STRINGER RT. REPAIRED PER EA 22-175178.SDR QXEA0001633Rib · crackedYYC- CRACK ON VERTICAL STAB, RIB 3.2 LEFT HAND SIDE AFT END OF LOWER SIDE. REPAIRED IAW FOKKER SRM 55-02-05 PAGE 8 FIGURE 4.SDR 20000530SH004Spar Cap · crackedDURING ROUTINE INSPECTION OF THE JE24 PIVOT FITTING, IT WAS RECOMMENDED BY THIS REPAIR STATION TO INSPECT THE LOWER VERTICAL STABILIZER FRONT SPAR CAP DOUBLERS FOR POSSIBLE CRACKS. CRACKS WERE FOUND ON BOTH LEFT AND RIGHT OUTER DOUBLERS. SUBMITTER STATED THI
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