JASC 5530

Service difficulty reports · 2,534

Reports filed under 5530 · Vertical Stabilizer, 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 = '5530'
  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 SWAA2015050739403Tail Cone · delaminatedLEFT VERTICAL STABILIZER DELAMINATED ON THE TAIL CONE. REPAIRED STABILIZER IAW EA.Apr 28, 2015 · N942AT · Boeing 717200SDR DALA2015041502785Fastener · looseVERTICAL FIN L/E MID SPLICE HAS MANY FASTENERS LOOSE. R & R IAW SG0955004. LP 1905434.Apr 15, 2015 · N943DN · Doug MD9030SDR VNAA2015040300010Drag Angle · crackedLEFT AND RIGHT VERTICAL STABILIZER LOWER FUSELAGE ATTACHMENT DRAG ANGLES AT 67.5 PERCENT REAR SPAR DATUM, ARE CRACKED. C/W REO 670-55-31-018, REV DATED 4/16/07.Apr 3, 2015 · N709PS · Cndair CL6002C10SDR DXTR2015041401Pivot · crackedVERTICAL SPAR PIVOT FITTING LOWER LT SIDE BOTTOM STRINGER CLIP CRACKED. R & R VERTICAL STABILIZER PIVOT CLIP REF SRM 55-30-01 AND REPAIR DEFINITION S-560XL-5240/05RD DATED 04/10/15.Mar 28, 2015 · N640QS · Cessna 560XLSDR K11A2015052725002Beam · crackedVERTICAL STAB KICKLOAD BEAM LT WEB POST CRACKED WERE IT ATTACHES TO STRINGER 11 IAW SB 727-55-0093, FIG 3, SHEET 4 FOR LOCATION.Mar 25, 2015 · N725CK · Boeing 727224SDR DALA2015040202562Attach Angle · crackedVERTICAL STABILIZER LT SIDE INTERNAL ATTACH ANGLE IS CRACKED AT STA 1475. REPLACED ANGLE IAW SRM 51-30-00.Mar 25, 2015 · N940DN · Doug MD9030SDR DALA2015032502397Angle · crackedCRACK ON LT/RT INTERNAL VERTIACL STABILIZER ATTACH DORSAL ANGLES BETWEEN STA Y=1458 TO 1486. DORSAL ANGLES WERE REMOVED, FABRICATED AND INSTALLED IAW SRM 51-30-02 AND 51-30-05.Mar 24, 2015 · N934DN · Doug MD9030SDR DALA2015031502150Former · crackedCRACKED FORMER ON TIP FAIRING STA YV 172. REPAIR WERE FABRICATED IAW SRM 55-01 IG 4. DOUBLERS AND FILLERS WERE TREATED AND PAINTED IAW SRM 51-10-3 PAR 14-21. REPAIR INSTALLED IAW SRM 51-302.Mar 14, 2015 · N966DL · Doug MD88SDR DALA2015031702209Doubler · crackedCRACKED INTERNAL DOUBLER ON VERTICAL STABILIZER ACCESS PLATE 370 BL CUTOUT. REPAIRED CRACK IAW SRM 5330-05, FIG 3.Mar 13, 2015 · N918DH · Doug MD9030SDR SWIA201540928Panel · crackedDORSAL STRAKE PANEL 321 CT IS CRACKED AT AFT SIDE. REPAIRED THE PANEL IAW EA. Mar 10, 2015 · N701SK · Cndair CL6002C10SDR SWIA201540927Panel · delaminatedDORSAL STRAKE PANEL 321 BT IS DELAMINATED ON BOTTOM SIDE, C-CHECK, RO 3/24/15, REPAIRED DELAMINATION ON PANEL 321BT, REF STS EA.Mar 10, 2015 · N701SK · Cndair CL6002C10SDR VNAA201503100017Drag Angle · crackedLEFT FWD VERT STAB DRAG ANGLE IS CRACKED APPROXIMATELY .25 ON AFT END. PERFORMED A MAJOR REPAIR TO THE LT VERTICAL STABILIZER FUSELAGE ATTACHMENT DRAG ANGLE AT 67.5 PERCENT REAR SPAR DATUM IAW REO 670-55-31-018, REV-DATED 16-APR-07.Mar 10, 2015 · N708PS · Cndair CL6002C10SDR DALA2015031002028Fairing · damagedFWD TOP END OF UPPER RT BANANA FAIRING DAMAGED. REMOVED PREVIOUSLY INSTALLED DOUBLER, REMOVED DAMAGE MATERIAL FROM FAIRING REF ERA 464895-14MA. ACCOMPLISHED HFEC NDT SPM 06-10-01-001. DAMAGED CONTAINED. TRIMED AND PILOT DRILLED DOUBLER FROM PN 55-0018-003.Mar 9, 2015 · N941DL · Doug MD88SDR DALA2015030401943Attach Angle · crackedLEFT VERTICAL FIN ATTACH ANGLE HAS LONG CRACK IN RADIUS, NEAR FIN AFT SPAR. REMOVED DAMAGE AND INSTALLED DOUBLER IAW PRI/ERA 533587-14, REV O.Mar 2, 2015 · N930DN · Doug MD9030SDR DALA2015022601668Angle · crackedCRACKED 2 ANGLES BETWEEN UPPER FUSELAGE SKIN AND DORSAL FIN BASE AT L/E RAM AIR SCOOP AREA STA Y= 1407 TO Y= 1427.Feb 22, 2015 · N980DL · Doug MD88SDR DALA2015022301580Access Panel · crackedCRACKED SETTLEMENT AREA, BOTH SIDES OF ACCESS PANEL 6301B AT DORSAL FIN L/E. DORSAL ANGLES WERE REPLACED IAW SRM 51-30-2, 51-30-5, 51-10-4, 51-10-3 PARA 14 & 21, AND DWG 5912188 REV BD.Feb 22, 2015 · N977DL · Doug MD88SDR CA150223008Fitting · cracked(CAN) DURING ANNUAL INSPECTION, FOUND CORROSION ON THE FITTING HOLDING VERTICAL STAB TO HORIZONTAL STAB. WHEN CORROSION WAS REMOVED, FAINT LINES WERE NOTICED. UNDER 10X MAGNIFICATION A CRACK WAS DETECT ON FORWARD VERTICAL SECTION OF FITTING APPROX 1/2" LONG. FFeb 20, 2015 · Cessna 150JSDR DALA2015022301577Structure · damagedLOOSE FASTENERS ON LOWER EDGE RT SIDE ABOVE LOWER SPLICE OF VERTICAL STABILIZER REMOVABLE L/E. HOLES, 17E/AS WERE REWORKED AND BUSHINGS WERE FABRICATED, PROTECTED ALSO INSTALLED IAW SRM 55-03D.Feb 18, 2015 · N980DL · Doug MD88SDR WVER0217201500003Drag Angle · crackedVERTICAL STABILIZER FORWARD DRAG ANGLE LT SIDE IS CRACKED APPROXIMATELY .5" IN LENGTH.Feb 17, 2015 · N923FJ · Cndair CL6002D24SDR WVER0217201500002Drag Angle · crackedVERTICAL STABILIZER FORWARD DRAG ANGLE RT SIDE IS CRACKED APPROXIMATELY .5" IN LENGTH.Feb 17, 2015 · N923FJ · Cndair CL6002D24SDR DALA2015021001109Channel · crackedCRACKED Z CHANNEL ON VERTICAL STABILIZER T/E BETWEEN ZRS 38.2 AND ZRS 57.7. Z-CHANNEL REPAIRED IAW SRM 55-01, FIG 2.Feb 7, 2015 · N971DL · Doug MD88SDR DALA2015012000417Attach Angle · crackedLEFT INTERNAL VERTICAL STABILIZER ATTACH ANGLE IS CRACKED IN RADIUS. R & R IAW DWG 5912188.Jan 19, 2015 · N944DN · Doug MD9030SDR WVER2015011700002Drag Angle · crackedLEFT AND RT VERTICAL STABILIZER FORWARD DRAG ANGLES ARE CRACKED.Jan 17, 2015 · N247LR · Cndair CL6002D24SDR DALA2015012000511Plate · corrodedCORROSION ON BORE OF PLATES, ZRS=173 AND XH=5 LT SIDE LOCATED ON VERTICAL STAB REAR. BORE OF PLATES WAS REMOVED. HOLD WAS REWORKED WITH MEASURED HOLE LT OTBD: O 1.435 AND HOLE. LT INBD: O 1.435, THEREFORE WITHIN LIMIT. REPAIR AND BUSHING WAS FABRICATED, AREA Jan 15, 2015 · N979DL · Doug MD88SDR IPXA2015013085497Intercostal · crackedINSPECTION TYPE: 4C, LOWER VERTICAL REAR CENTER SPAR TO REAR SPAR, RT AFT INTERCOSTAL CRACKED STA Y=2164 AT X =-8.5. ACCOMPLISHED PERMANENT REPAIR ON LOWER VERTICAL REAR CENTER SPAR TO REAR SPAR RT INTERCOSTAL STA Y=2164 AT X = -8.5 IAW SRM 55-30-02, REPAIR 7Jan 8, 2015 · N256UP · Doug MD11FSDR DXTR2015020401Bracket · crackedLOWER CLIP ON VERTICAL STABILIZER HAS 2 SMOKED HI-LOCKS ON OTBD EDGES ON FWD SIDE. FOUND A CRACK PROTRUDING FROM THE LT OTBD LOWER PIVOT FITTING FLANGE TRAVELING UP & OTBD APPROX .5" FOUND 2 CRACKS TRAVELING FROM THE RT OTBD HOLE, ONE TRAVELING UP & OTBD APPRJan 7, 2015 · N695QS · Cessna 560XLSDR SCNA20141223254Stiffener · crackedRIGHT STABILIZER NR 1 SPAR RIB STAB STA 92.7 FWD VERTICAL STIFFNER CRACKED AT LOWER FLANGE, REPAIRED.Dec 12, 2014 · N817SY · Boeing 7378K2SDR SCNA20141223255Stiffener · crackedRIGHT STABILIZER NR 1 INSPAR RIB AT STA 92.7 AFT VERTICAL STIFFNER CRACKED AT LOWER FLANGE, REPAIRED.Dec 11, 2014 · N817SY · Boeing 7378K2SDR CA141201002Adapter · cracked(CAN) WHILE COMPLETING SB 6/454, THE RT REAR STABILIZER ATTACHMENT ADAPTER FOUND CRACKED.(P/N C6FSM 1820-33). THE ATTACHMENT ADAPTOR WAS REPLACED WITH NO ADDITIONAL DEFECTS NOTED.Nov 25, 2014 · Dhav DHC6*SDR DALA2014112206313Structure · damagedELONGATED HOLES ON REMOVABLE L/E STA ZFS=52.267 AT VERTICAL STABILIZER. REMOVABLE L/E WAS REPAIR IAW CARD 5530- 01045-08 AND SRM FIG 30.Nov 21, 2014 · N974DL · Doug MD88SDR WVER2014111700004Drag Angle · crackedFWD DRAG ANGLE ON RT SIDE OF VERTICAL STABILIZER HAS A CRACK.Nov 17, 2014 · N920FJ · Cndair CL6002D24SDR ASOA2014120511817Drag Angle · crackedLT VERTICAL AFT DRAG ANGLE CRACKED. REMOVED THE DRAG ANGLE AND INSTALLED A NEW DRAG ANGLE IAW SRM 51-42-10-001-01-A01, 51-42-21-001-001-A01, 51-40-11-001-001-A01, 51-42-22-001-001-A01 AND DWG BA670-35002.Nov 15, 2014 · N146PQ · Cndair CL6002D24SDR ASOA20141114338Drag Angle · crackedDURING C-CHECK DRAG ANGLE AT LT FWD CORNER OF VERTICAL STAB IS CRACKED. MAINTENANCE R & R DRAG ANGLE AT LT FWD CORNER OF VERTICAL STAB IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Nov 15, 2014 · N15910 · Emb EMB145LRSDR ASOA20141114337Drag Angle · crackedDURING C-CHECK DRAG ANGLE AT FWD RT CORNER OF VERTICAL STAB IS CRACKED. MAINTENANCE R & R RT FWD DRAG ANGLE ON VERTICAL STAB IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Nov 15, 2014 · N15910 · Emb EMB145LRSDR SWAA2014120234604Structure · delaminatedVERTICAL STABILIZER LE DELAMINATED APPROX 4 INCHES FROM LOWER EDGE. REPAIRED STABILIZER IAW EA.Nov 14, 2014 · N429WN · Boeing 7377H4SDR ASOA20141110328Drag Angle · crackedDURING C-CHECK, DRAG ANGLE AT FWD RT CORNER OF VERTICAL STAB IS CRACKED. MAINTENANCE R & R DRAG ANGLE AT FWD RT CORNER OF VERTICAL STAB IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Nov 10, 2014 · N15910 · Emb EMB145LRSDR DALA2014102905824Skate Angle · crackedFORWARD RT INNER VERTICAL STABILIZER ATTACH ANGLE HAS A FOUR INCH CRACK. R & R INNER SKATE ANGLE IAW DWG 5912188.Oct 28, 2014 · N942DN · Doug MD9030SDR CA141120011Bolt · broken(CAN) FIN SPAR RT MAIN ATTACH BOLT WAS FOUND TO BE BROKEN OFF. HEAD OF BOLT WAS STILL IN ATTACH FITTING NUT AND LOWER PORTION OF BOLT WERE MISSING, BOTH BOLTS REPLACED.Oct 27, 2014 · Dhav DHC2MKISDR WVER102220140001Drag Angle · crackedLEFT AND RT VERTICAL STABILIZER FORWARD DRAG ANGLES ARE CRACKED.Oct 22, 2014 · N914FJ · Cndair CL6002D24SDR DXTR2014102101Fitting · crackedHORIZONTAL STABILIZER FITTING ASSY CRACKED ABOVE CLIP ATTACH POINT.Oct 21, 2014 · N694QS · Cessna 560XLSDR A6WA201442107Hinge Bracket · deformedON VERTICAL STAB AFT SPAR, UPPER CTR RUDDER HINGE BRACKET LOWER HALF BORE MALFORMED.Oct 17, 2014 · N455AW · Cndair CL6002B19SDR SWIA201439679Fairing · damagedLIGHTNING STRIKE DAMAGE TO VERTICAL STABILIZER BULLET FAIRING AND AFT FAIRING ASSY. REPAIRED IAW EA.Oct 9, 2014 · N744SK · Cndair CL6002C10SDR DALA2014100805480Angle · damagedDURING C-CHECK, ELONGATED HOLES WERE FOUND COMMON TO THE LT ANGLE OF THE VERTICAL STABILIZER FRONT SPAR. FOUR OF THE HOLES ARE THE FIRST, FOURTH, FIFTH, AND SIXTH ABOVE ZFS=52. ONE OF THE HOLES IS THE FOURTH HOLE BELOW ZFS=52. ER/A 529591-14AD SECT I WAOct 7, 2014 · N945DL · Doug MD88SDR WVER1006201493802Drag Angle · crackedLEFT VERTICAL STABLIZER FORWARD DRAG ANGLE IS CRACKED APPROXIMATELY 2" LONG.Oct 6, 2014 · N938LR · Cndair CL6002D24SDR WVER1006201493801Drag Angle · crackedLEFT VERTICAL STABLIZER AFT DRAG ANGLE IS CRACKED APPROXIMATELY 2 " LONG.Oct 6, 2014 · N938LR · Cndair CL6002D24SDR WVER201409240003Drag Angle · crackedVERTICAL STABILIZER RT AFT DRAG ANGLE IS CRACKED.Sep 24, 2014 · N507MJ · Cndair CL6002C10SDR DALA2014092405233Angle · crackedCRACKED LT/RT ANGLES FWD UPPER SECTION STA YV=170 AT VERTICAL STABILIZER TIP FAIRING. CLIPS 2EA WERE REMOVED FABRICATED, TREATED, PAINTED, AND INSTALLED IAW SRM 51-10-3, DWG 9911962.Sep 23, 2014 · N975DL · Doug MD88SDR WVER0923201450702Drag Angle · crackedRIGHT FORWARD VERTICAL STABILIZER DRAG ANGLE IS CRACKED APPROXIMATELY TWO INCHES IN LENGTH ON AFT END.Sep 23, 2014 · N507MJ · Cndair CL6002C10SDR WVER0923201450701Drag Angle · crackedLEFT FWD VERTICLE STABALIZER DRAG ANGLE IS CRACKED APPROXIMATELY 2" IN LENGTH ON AFT END.Sep 23, 2014 · N507MJ · Cndair CL6002C10SDR 7AHR2014092300002Structure · gougedGOUGED AREAS WERE FOUND ON FWD LT SIDE OF VERTICAL STABILIZER UNDER UPPER AND LOWER BANANA FAIRING. GOUGED AREAS WERE FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR TO TIP PLATING IAW FLIGHT VEHICLE CONSULTING DWG NR 55-14233-1, REV-NEW, DATED SESep 22, 2014 · N935CE · Doug DC933F
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