# JASC 1430: Fasteners - Type: JASC system/component code (FAA) - ATA chapter: 14 Hardware - Title in the code table: FASTENERS - Service difficulty reports: 705 - FAA code table: https://www.faa.gov/sites/faa.gov/files/JASC_Code.pdf#page=15 - Page: https://openairdocs.org/jasc/1430 ## What it covers For reports indicating a problem with any aircraft or engine fastener that is not associated a specific aircraft system. Typical parts are generic AN bolts, nuts, rivets, etc. ## Service difficulty reports (705, newest 50) - [SDR 2VKA2024072453552](https://openairdocs.org/sdr/2VKA2024072453552), Jan 24, 2024: Bell 407. WASHER. CRACKED. WHILE CHANGING TRANSMISSION ASSEMBLY, TECHNICIAN NOTICED THREE PYLON RETAINING BOLT WASHERS PN:140-007-25S22E6 CRACKED A (N314SF) - [SDR TSAA20230606107](https://openairdocs.org/sdr/TSAA20230606107), Jun 6, 2023: Boeing 737330. UNKNOWN. UNKNOWN. CA 1464/361 WHILE PERFORM CUSTOMER PROVIDE TASK CARD ECO 3531-R10 WHICH INDICATED IN SB 737-53A1240, FOUND FASTENER HAD (N301KH) - [SDR 8HBR20230415051](https://openairdocs.org/sdr/8HBR20230415051), Apr 15, 2023: Piper PA34220T. BOLT. MISMANUFACTURED. BOLT, PIPER P/N 402-921 QUANTITY OF 8 WERE ORDERED FROM BOEING, 4 OF THE 8 DID NOT HAVE THE HOLE DRILLED THROUGH THE THR (N4324D) - [SDR 2022FA0000485](https://openairdocs.org/sdr/2022FA0000485), Aug 1, 2022: Piper PA34200T. BOLT. USED. LEFT LANDING GEAR SCISSOR LINK CENTER BOLT FAILED DURING TAXI (N8111P) - [SDR 2022FA0000272](https://openairdocs.org/sdr/2022FA0000272), May 22, 2022: Cessna 172M. COWL FASTENER. BROKEN. I DO NOT KNOW IF I OR THE MANUFACTURER NEED TO REPORT THIS. I BOUGHT A FEW COWLING FASTENERS AND THEY ALL FAILED WITHIN (N3JA) - [SDR 2022FA0000011](https://openairdocs.org/sdr/2022FA0000011), Jan 11, 2022: Cessna 750. BRACKET. CRACKED. A RECENT SDR REPORT FOR A BROKEN BRACKET AND SUBSEQUENT LEAK IN A HYDRAULIC LINE ON AIRCRAFT N733FL (12508 HRS), S/N 750 (N750VP) - [SDR R61A2021111700902](https://openairdocs.org/sdr/R61A2021111700902), Nov 7, 2021: Emb ERJ170200LR. SKIN. OUT OF LIMITS. FOUND STUCK FASTENER IN FITTING ON AILERON TORQUE TUBE SUPPORT, PERFORMED TEMPORARY REPAIR BY REAMING HOLE AND FABRICATE (N219YX) - [SDR 2007FA0000392](https://openairdocs.org/sdr/2007FA0000392), Mar 1, 2007: TAB. CRACKED. WHEN TECH WENT TO BEND THE TAB ATTACHED TO THE WASHER AT THE RADIUS OF THE BEND, THEY WOULD CRACK. (K) - [SDR 2006FA0000421](https://openairdocs.org/sdr/2006FA0000421), Apr 10, 2006: Beech 400A. SCREW. WRONG PART. DURING INSPECTION IAW MFG SB, FOUND BRAKE HYDRAULIC LINE DAMAGED BY FLOOR PANEL ATTACHING SCREW. REPAIRED TUBING AND MOD (N907JE) - [SDR ASAA0610173](https://openairdocs.org/sdr/ASAA0610173), Feb 20, 2006: Boeing 737290C. RIVET. CORRODED. CORROSION ON RIVETS. REPAIRED PER SRM 53 10 3 FIG 1. (N742AS) - [SDR CA051208003](https://openairdocs.org/sdr/CA051208003), Nov 12, 2005: Dhav DHC2MKI. BOLT. WRONG PART. WRONG BOLTS INSTALLED AT LOWER FUSELAGE STRUT TO BIRDCAGE STRUCTURE. AN6-A INSTALLED, SHOULD BE AN176-13A CLOSE TOLERANC - [SDR 05FDEA02608](https://openairdocs.org/sdr/05FDEA02608), Aug 24, 2005: Doug DC1010. FASTENER. WRONG PART. AIR COND COMPT LT SIDE FOUND EXISTING REPAIR WITH WRONG FASTENERS (CHERRY AND BOLT) ON NLG BLKHD. REMOVED EXISTING REPAI (N556FE) - [SDR CA050818004](https://openairdocs.org/sdr/CA050818004), Aug 18, 2005: Cessna U206G. BOLT. BROKEN. (CAN) PILOT REPORT: NO BRAKE ON RT SIDE OF AIRCRAFT. BRAKE PEDDLE WAS SOLID, NO TRAVEL. INSPECTION REVEALED THAT THE OB - [SDR CA050906003](https://openairdocs.org/sdr/CA050906003), Aug 4, 2005: BOLT. FAILED. (CAN) ENG TAY 16916 AFTER TEST, HAD ABNORMAL NOISE DURING ROTATION OF LP SYS. ENG WAS REJECTED AT DISPATCH AND MODULE 5 - [SDR SWAA052308](https://openairdocs.org/sdr/SWAA052308), Aug 2, 2005: Boeing 7373H4. BOLT. WORN. DURING SCHEDULED C1 CHECK, LT ELEVATOR TAB FAILED THE FREE PLAY CHECK. REMOVED AND REPLACED LT ELEVATOR TAB CONTROL PUSH (N396SW) - [SDR 2005FA0001089](https://openairdocs.org/sdr/2005FA0001089), Aug 2, 2005: Piper PA34200T. NUT. CRACKED. REPAIR STATION WAS REPAIRING AIRCRAFT HYD LEAK. WHEN REMOVING LOWER FORWARD WING ATTACH BOLT COVERS FOUND 10 OF THE 16 M (N36049) - [SDR DL76S050419](https://openairdocs.org/sdr/DL76S050419), Jul 30, 2005: Boeing 767332. BOLT. LOOSE. RT ENG FIRE IND INTERMIT DURING CLM. S/D ENG AND ATB TO ATL.C/A FOUND 4 BOLTS LOOSE ON HPT NOZZLE COOLING DUCTS AT HPC C (N130DL) - [SDR 05FDEA02138](https://openairdocs.org/sdr/05FDEA02138), Jul 29, 2005: Airbus A300F4605R. FASTENER. MISSING. PASSING 5500FT MSL AND LEVELING AT 6000 FT, HAND FLYING USING AUTO THROTTLES, ATTEMPTED TO TRIM AIRCRAFT MANUALLY WITH T (N651FE) - [SDR CA050708003](https://openairdocs.org/sdr/CA050708003), Jul 8, 2005: Dhav DHC8301. COLLAR. FAILED. DURING HEAVY MAINTENANCE IT WAS DISCOVERED ON THE LHS WING FWD SPAR AT WS 490.0 SPLICE JOINT. 4 CRACKED LOCKBOLT COLLARS - [SDR MWEA050047](https://openairdocs.org/sdr/MWEA050047), Jun 7, 2005: Boeing 717200. RIVET. LIGHTNING STRIKE. ONE EACH RIVET AT STATION 64-83 ABOVE LONGERON 18 LEFT HAS EVIDENCE OF A LIGHTNING STRIKE. HEAT DAMAGE HAS BEEN REMOVED (N903ME) - [SDR 2005FA0000835](https://openairdocs.org/sdr/2005FA0000835), Jun 2, 2005: Raythn 390. BOLT. CHAFED. UPON REMOVAL OF FLAP ACTUTORS FOUND NR 3 LT AND RT FLAP ACTUATORS WERE DEEPLY GOUGED, DUE TO FLAP TRACK BOLTS INSTALLED (N128JL) - [SDR ASOA05455](https://openairdocs.org/sdr/ASOA05455), May 22, 2005: Aerosp ATR72. FASTENER. MISSING. DURING A GROUND INSPECTION, THE PASSENGER DOOR WAS FOUND DIFFICULT TO OPEN. MAINTENANCE REINSTALLED 2 FASTENERS (SCREWS) (N643AS) - [SDR QXEA200500994](https://openairdocs.org/sdr/QXEA200500994), May 17, 2005: Cndair CL6002C10. FASTENER. LOOSE. RT WING UPPER SKIN TRAILING EDGE HAS LOOSE FASTENERS AT INBOARD OF MULTI-FUNCTION SPOILERS. REPAIRED IAW CRJ 700 SRM 51- (N616QX) - [SDR QXEA200501003](https://openairdocs.org/sdr/QXEA200501003), May 17, 2005: Cndair CL6002C10. FASTENER. LOOSE. LT WING OUTBOARD FLIGHT SPOILERS HAVE LOOSE FASTENERS, OUTBOARD AND INBOARD SIDES. REPAIRED IAW CRJ 700 SRM 51-42-07-001 (N616QX) - [SDR ASOA05417](https://openairdocs.org/sdr/ASOA05417), May 6, 2005: Cndair CL6002B19. FASTENER. CORRODED. DURING A C-CHECK IN MCN, THE FASTENERS UNDER THE CABIN FLOORBOARD AT FS 333 APPROXMATELY RBL 7-9 WERE FOUND TO BE CORROD (N849AS) - [SDR 2005FA0000789](https://openairdocs.org/sdr/2005FA0000789), May 5, 2005: Beech B200. RIVET. MISSING. DURING VISUAL INSPECTION OF AFT FUSELAGE STRINGERS AT AFT PRESSURE BULKHEAD FOR COMPLIANCE WITH AD, NOTED (1) RIVET MISS (N200ZT) - [SDR AWXA200500617](https://openairdocs.org/sdr/AWXA200500617), May 4, 2005: Boeing 7373G7. BOLT. CORRODED. MCN - FLIGHT CONTROL - DURING C-14 CHECK, CORROSION WAS FOUND ON RT HORIZONTAL STABILIZER, FWD UPPER SPAR TO CENTER ATTA (N322AW) - [SDR QXEA200500931](https://openairdocs.org/sdr/QXEA200500931), Apr 29, 2005: Cndair CL6002C10. RIVET. LOOSE. YYC - RIGHT WING INBOARD MFS AREA, TWO LOOSE RIVETS INBOARD NEAR PIE SHAPE AREA. REPAIRED IAW CRJ700 SRM 51-42-06-001-00 (N611QX) - [SDR QXEA200500899](https://openairdocs.org/sdr/QXEA200500899), Apr 29, 2005: Cndair CL6002C10. RIVET. LOOSE. YYC - FUSELAGE EXTERIOR HAS SMOKING RIVET AT STATION 830 AND STRINGER 7R. REPAIRED IAW CRJ700 SRM 51-42-06-001-001-A01. (N611QX) - [SDR QXEA200500898](https://openairdocs.org/sdr/QXEA200500898), Apr 29, 2005: Cndair CL6002C10. RIVET. LOOSE. YYC - FUSELAGE EXTERIOR HAS SMOKING RIVETS AT STATION 693 AND STRINGER 7R. REPAIRED IAW CRJ-700 SRM 51-42-06-001-001-A01 (N611QX) - [SDR QXEA200500900](https://openairdocs.org/sdr/QXEA200500900), Apr 28, 2005: Cndair CL6002C10. RIVET. LOOSE. YYC - FUSELAGE EXTERIOR HAS SMOKING RIVET AT STATION 850 AND STRINGER 10L. REPLACED IAW CRJ700 SRM 51-42-06-001-001-A01. (N611QX) - [SDR IXXA05SMN01S](https://openairdocs.org/sdr/IXXA05SMN01S), Apr 27, 2005: Doug DC871F. SCREW. CORRODED. DURING ROUTINE C CHECK INSPECTION, RT WING, L/E INBD STUB WING UPPER SURFACE SCREWS OXIDIZED, XW 257.000. REMOVED OXIDIZ (N828BX) - [SDR DAT2005F00004](https://openairdocs.org/sdr/DAT2005F00004), Apr 27, 2005: Stbros SD330. ATTACH BOLT. LOOSE. DURING SCHEDULED MAINTENANCE OF COMPLYING WITH AD (PROP TORQUE) ON THE RT PROPELLER IN ACC`S HANGAR, (3) PROP ATTACH BOL (N938MA) - [SDR 2005FA0000653](https://openairdocs.org/sdr/2005FA0000653), Apr 22, 2005: Beech B300. SCREW. WRONG PART. DURING SCHEDULED INSPECTION FOUND SCREWS ATTACHING AFT LOWER EDGES OF FORWARD WING ROOT FAIRINGS TO UNDERSIDE WING ROOT (N768WT) - [SDR 05FDEA01040](https://openairdocs.org/sdr/05FDEA01040), Apr 18, 2005: Doug MD11. FASTENER. WRONG PART. RT WING, DURING ACCOMPLISHMENT OF EO 1-5750-7-5004 PART 2, SEVEN (7) EACH COUNTERSUNK LOCK FASTENERS COMMON TO TENSION S (N583FE) - [SDR 05FDEA01039](https://openairdocs.org/sdr/05FDEA01039), Apr 18, 2005: Doug MD11. FASTENER. WRONG PART. LT WING, DURING ACCOMPLISHMENT OF EO 1-5750-7-5004 PART 1, SEVEN (7) EACH COUNTERSUNK LOCK FASTENERS COMMON TO TENSION S (N583FE) - [SDR QXEA200500687](https://openairdocs.org/sdr/QXEA200500687), Apr 13, 2005: Dhav DHC8202. RIVET. LOOSE. PDX - FOUR RIVETS SMOKING/PULLING THROUGH SKIN UNDER WING FAIRING, APPROXIMATELY X424, LEFT SIDE WHERE LOWER END OF FAIR (N346PH) - [SDR QXEA200500747](https://openairdocs.org/sdr/QXEA200500747), Apr 12, 2005: Cndair CL6002C10. RIVET. LOOSE. YYC - LOWER FUSELAGE STATION 1098 TO 1108 STRINGER 18 TO 19 RT SKIN HAS FOUR LOOSE RIVETS SMOKING. REPAIRED IAW CRJ700 S (N614QX) - [SDR QXEA200500812](https://openairdocs.org/sdr/QXEA200500812), Apr 11, 2005: Cndair CL6002C10. RIVET. LOOSE. YYC - VERTICAL STABILIZER, RIGHT SIDE, BOTTOM AFT SKIN HAS NINE SMOKING RIVETS. REPLACED IAW CRJ7000 SRM 51-42-13-001-00 (N614QX) - [SDR SIMA200510103](https://openairdocs.org/sdr/SIMA200510103), Apr 1, 2005: Emb EMB145LR. RIVET. DAMAGED. SAW - LIGHTNING STRIKE DAMAGE ON SEVERAL RIVETS ON LEFT WING FUEL CELL. MAINTENANCE REPLACED RIVETS IAW SRM 51-40-02 AND (N689EC) - [SDR QXEA200500638](https://openairdocs.org/sdr/QXEA200500638), Mar 29, 2005: Cndair CL6002C10. FASTENER. LOOSE. YYC - HORIZONTAL STABILIZER CENTERING TRACK ALL ATTACHED FASTENERS LOOSE. REPAIRED IAW HORIZON AIR EA R-55-32A AND REO 6 (N612QX) - [SDR 2005FA0000493](https://openairdocs.org/sdr/2005FA0000493), Mar 29, 2005: Boeing B17G. SCREW. FRACTURED. (7) OF THE (10) FRONT COVER RETAINING SCREWS WERE FRACTURED, ALL AT THE SAME LOCATION- (3) THREADS FROM SHANK. ALL (7) H (N9563Z) - [SDR QXEA200500628](https://openairdocs.org/sdr/QXEA200500628), Mar 24, 2005: Cndair CL6002C10. FASTENER. CORRODED. YYC - RIGHTHAND WING LOWER SURFACE INBOARD MAIN LANDING GEAR DOUBLER PLATE ATTACHMENT FASTENERS ARE RUSTY. REPAIRED IAW (N612QX) - [SDR QXEA200500615](https://openairdocs.org/sdr/QXEA200500615), Mar 23, 2005: Cndair CL6002C10. RIVET. SMOKE. YYC - FUSELAGE EXTERIOR HAS FOUR SMOKING RIVETS AT STATION 745 AND STRINGER 16R. REPLACED RIVETS IAW CRJ7800 SRM 51-42-0 (N612QX) - [SDR QXEA200500623](https://openairdocs.org/sdr/QXEA200500623), Mar 22, 2005: Cndair CL6002C10. SCREW. LOOSE. YYC - RIGHTHAND WINGLET INBOARD AND OUTBOARD SURFACES HAVE MANY LOOSE SCREWS. RETORQUED IAW CRJ700 MM 57-30-84, PAGE 422 (N612QX) - [SDR QXEA200500621](https://openairdocs.org/sdr/QXEA200500621), Mar 20, 2005: Cndair CL6002C10. RIVET. LOOSE. YYC - FUSELAGE UPPER EXTERIOR HAS SEVERAL SMOKING RIVETS AT STRINGER 3L AND BETWEEN FUSELAGE STATION 345 TO 379. REPAIRE (N612QX) - [SDR QXEA200500620](https://openairdocs.org/sdr/QXEA200500620), Mar 20, 2005: Cndair CL6002C10. RIVET. LOOSE. YYC - FUSELAGE UPPER EXTERIOR HAS SEVERAL SMOKING RIVETS AT STRINGER 7L, BETWEEN FUSELAGE STATION 893 TO 939. REPAIRED I (N612QX) - [SDR QXEA200500622](https://openairdocs.org/sdr/QXEA200500622), Mar 20, 2005: Cndair CL6002C10. RIVET. SMOKE. YYC - FUSELAGE EXTERIOR HAS SEVERAL SMOKING RIVETS AT FUSELAGE STATION 677, STRINGER 3L TO STRINGER 6L. REPAIRED IAW CRJ (N612QX) - [SDR QXEA200500543](https://openairdocs.org/sdr/QXEA200500543), Mar 20, 2005: Cndair CL6002C10. RIVET. SMOKE. YYC - FUSELAGE EXTERIOR HAS SMOKING RIVET AT FUSELAGE STATION 485. REPAIRED IAW CRJ700 SRM 51-25-001-001-A01. (N612QX) - [SDR QXEA200500560](https://openairdocs.org/sdr/QXEA200500560), Mar 19, 2005: Cndair CL6002C10. RIVET. PULLED. YYC - CENTER FUSELAGE AT STATION 770.0, WL 725, RBL 9.0-17.0 HAS RIVETS PULLED ON FLAT STRAP. REPAIRED IAW CRJ700 SRM 51 (N612QX) All 705: https://openairdocs.org/jasc/1430/reports.md ## Other codes in chapter 14 - [JASC 1400](https://openairdocs.org/jasc/1400): Miscellaneous Hardware (42 reports) - [JASC 1410](https://openairdocs.org/jasc/1410): Hoses and Tubes (23 reports) - [JASC 1420](https://openairdocs.org/jasc/1420): Electrical Connectors (215 reports) - [JASC 1497](https://openairdocs.org/jasc/1497): Miscellaneous Wiring (9 reports) --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.