JASC 7830
Service difficulty reports · 5,917
Reports filed under 7830 · Engine Thrust Reverser, 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 = '7830' 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 = '7830' 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 A6WA201643812Plate · crackedRIGHT THRUST REVERSER PDU CONNECTOR PLUG MOUNTING PLATE IS CRACKED. REPLACED RT THRUST REVERSER PDU MOUNT PLATE IAW SRM 51-42-06.SDR IPXA2016051503365Skin · crackedINSPECTION TYPE: 2C, NR 1 ENGINE THRUST REVERSER INNER BARREL UPPER SKIN CRACKED. REPAIRED SKIN CRACK IAW EA 011-7830-01-A6232, REV IR AND EO MD11-7830-60767-A.SDR RAIA201604220001Switch · inoperativeENGINE 2 REVERSER FAIL ON EICAS. R & R THRUST REVERSER TRANSIT SWITCHES. OPS CHECK GOOD.SDR A6WA201643787Torque Box · crackedRIGHT THRUST REVERSER TORQUE BOX CRACKED AT THE 5 O`CLOCK POSITION. REPAIRED RT ENG THRUST REVERSER TORQUE BOX IAW REO 601R-78-34-2527 REV B.SDR A6WA201643770Torque Box · crackedLEFT ENG TORQUE BOX CRACKED AT 7 O'CLOCK POSITION. REPAIRED LT ENG TORQUE BOX IAW REO601R-78-34-2527 REV B.SDR HALA2016040900106Warning Light · false activationENGINE 1 REVERSER FAULT, ENGINE 1 LP SHAFT PROT LOSS. PERFORMED ENGINE RUN IAW AMM 71-00-501. NO MESSAGES NOTED, NO FAULTS NOTED. ACFT OK FOR SERVICE.SDR Z6WR20160405007Panel · burnedUPON REMOVAL OF THE 315A2130 BLANKET INSTALLATION, VISUAL & ULTRASONIC INSPECTION OF THE 315A2101-174 BONDED PANEL ASSEMBLY, CMM 78-31-26 FIGURE 6 ITEM 40B, REVEALED EIGHT AREAS OF THERMAL DEGRADATION RESULTING IN DISBOND & DELAMINATION C/T THE 174 BONDED PANSDR ASAA2016040316232Switch · failedON LANDING THE TAKEOFF CONFIGURATION LIGHT AND HORN ACTIVATED WHEN ACTIVATING THE REVERSE THRUST. HORN AND LIGHT EXTINGUISHED WHEN STOWING THE REVERSERS. REF LOG PAGES 11451962 AND 11451963. ACFT GROUNDED. REF PSEU BITE FIM 32-09, TASK 801, NO EXISTING FSDR FDEA201603311128Relay · inoperativeDURING PUSHBACK, REV ISLN, LIGHT ON THROTTLE QUADRANT ILLUMINATED. ADVISED MX THEY SAID IT WOULD EXTINGUISH AFTER TAKEOFF. AFTER TAKEOFF, REV ISLN, REMAINED ILLUMINATED. FOR SAFETY DID AN AIR TURN BACK. R & R K2157. OPENED CB AIR & GND SYS 1 & REV ISLN LSDR DALA2017112708298Cowling · nickedFOUND A NICK IN THE NR 1 ENGINE OTBD THRUST REVERSER COWL FROM REAR 9 INCH, 9 O CLOCK. REPAIRED IAW SRM.SDR A6WA201643733Switch · out of rigWHILE EN-ROUTE RECEIVED LT REVERSER UNLOCKED CAUTION. COMPLIED WITH QRH & DIVERTED. REVERSER APPEARS STOWED ON WALK AROUND. DEACTIVATED LT THRUST REVERSER IAW SUPP 15-046. COMPLIED WITH M ACTION. TROUBLE SHOT & FOUND LT THRUST REVERSER STOW SWITCH TO BE ESDR CALA2016032800190Warning System · false activationRIGHT ENG REVERSER LIGHT ILLUMINATED ON THE TAKEOFF R LL. INITIATED & COMPLETED A LOW SPEED REJECTED TAKEOFF AT 70 KNTS, OFF TIME WAS 1122 Z. COOLED BRAKES FOR 10 MINS BEFORE TAXIING. PLACARDED NR 2 ENG THRUST REVERSER INOPERATIVE. MX PLACED REVERSER ON MESDR DALA2016032502294Door · crackedSEVERAL CRACK ON HOLES OF OUTER SKIN AT LT ENGINE THRUST REVERSE UPPER DOOR. SKIN AT LT ENGINE TRUST REVERSE UPPER DOOR WERE REPAIRED IAW AMM 78-30-07-801.SDR DXTA2016031906206Pin · wornRIGHT REVERSER UNLOCK CAS MSG CLIMBING THRU 28000 FT AT 300 KT. COMPLIED WITH QRH CHECKLIST & LANDED. ACTIVATED RT THRUST REVERSER IAW CMP 780012. PERFORMED T/R UNLOCK OPERATIONAL TEST IAW MM 78-00-00, ALL SWITCHES CHECKED GOOD. DURING OPERATIONS CHECK FOUSDR YGJR20160321ABracket · crackedWHILE PERFORMING A GENERAL VISUAL INSPECTION OF THE RT ENGINE THRUST REVERSER STOW SWITCH BRACKET AREA, IT WAS DISCOVERED THAT THE ATTACHMENT BRACKET FOR THE CONNECTOR PLUGS OF THE STOW SWITCH AND THE THROTTLE LOCK OUT WAS CRACKED. REPLACED CRACKED BRACKET.SDR VNAA2016031400018Switch · failedCREW REPORTED LT THRUST REVERSER UNLOCK AMBER CAUTION MESSAGE AND THAT EMERGENCY STOW DID NOT WORK. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R LT STOW MICROSWITCH AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.SDR VNAA2016031400017Drive Unit · failedCREW REPORTED LT THRUST REVERSER UNLOCK AMBER CAUTION MESSAGE AND THAT EMERGENCY STOW DID NOT WORK. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R LT POWER DRIVE UNIT AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.SDR V0XD20160314058Latch · brokenRIGHT AFT THRUST REVERSER LATCH PIN BROKEN. R & R RT AFT THRUST REVERSER LATCH IAW AMM 78-33-03 & 20-21-00.SDR CA160322007Relay · stuck(CAN) LEFT HAND TRUST REVERSER FAIL CAS MESSAGE WAS DISPLACED ON MFD. DURING TROUBLE SHOOTING FOUND STOW AND DEPLOY HARNESS SWITCH WAS FOUND TO BE AT FAULT. REPLACED HARNESS WITH A REPAIRED UNIT. AS A PRECAUTIONARY MEASURE WE REPLACED LEFT HAND INBOARD STOW RESDR IPXA2016033101450Barrel · gougedINSPECTION TYPE:3C, NR 3 ENGINE OTBD T/R INNER ACOUSTIC BARREL GOUGED. ACCOMPLISHED REPAIR ON NR 3 ENG OTBD T/R INNER ACOUSTIC BARREL IAW EA 011-7830-01-A6169, REV I/R AND EO MD11-7830-60351-A.SDR A6WA201643677Pdu · defectiveRECEIVED RT REV UNLOCK CAUTION MSG, PASSING THROUGH 23,700 FT. COMPLIED WITH QRH, MSG REMAINS, AMBER REV ICON. REVERSERS WERE NOT ARMED. RT REV APPEARS TO BE STOWED AT THE GATE. DEACTIVATED RT TR IAW SUP 15-046. COMPLIED WITH M ACTION. R & R PDU FOR RT TSDR SRXR20160307001Fireseal · crackedNR 4 ENGINE OTBD T/R FIRESEAL RETAINER IS CRACKED, REPAIR WAS ACCOMPLISHED ON NRC A024766 IAW EA 747-5445-39-A6121 I/R AND FAA APPROVED 8110-3, DATED FEB 23 2016.SDR A6WA201643663Thrust Reverser · lack of lubeIN FLIGHT RECEIVED RT REV UNLOCK MSG. COMPLIED WITH QRH. DIVERTED & LANDED BELOW 47000 LBS & MAX BTMS WAS 4454. DEACTIVATED RT TR IAW SUP 15-046, M ACTION COMPLIED WITH. PERFORMED TR LUBE IAW SUPP 14-118A. OPERATIONS CHECKED GOOD AT THIS TIME. REMOVED PLSDR YGJR201603240001Attach Bracket · crackedWHILE PERFORMING A GENERAL VISUAL INSPECTION OF THE RT ENGINE THRUST REVERSER STOW SWITCH BRACKET AREA, IT WAS DISCOVERED THAT THE ATTACHMENT BRACKET FOR THE CONNECTOR PLUGS OF THE STOW SWITCH AND THE THROTTLE LOCK OUT WAS CRACKED. REPLACED CRACKED BRACKET.SDR A6WA201643641Torque Box · crackedNUMBER 1 ENG TR TORQUE BOX AFT FLANGE AT 7O CLOCK CRACKED, REPAIRED.SDR A6WA201643621Rod · disconnectedDURING REMOVAL OF NR 1 ENG OIL TRANSDUCER, FOUND BLOCKER DOOR ROD, THRUST REVERSER AT 1:30 POSITION DISCONNECTED. INSTALLED SERVICEABLE BLOCKER DOOR LINK PIN AT THE 1:30 POSITION IAW AMM 78+33+21. OPERATIONS CHECKED GOOD.SDR Z6WR20160219006Panel · degradedUPON REMOVAL OF THE 315A2130 BLANKET INSTALLATION, VISUAL & ULTRASONIC INSPECTION OF THE 315A2102-174 BONDED PANEL ASSEMBLY, CMM 78-31-26 FIGURE 6 ITEM 45B REVEALED 3 AREAS OF THERMAL DEGRADATION RESULTING IN DISBOND & DELAMINATION. CT THE 174 BONDED PANEL ASSDR Z6WR20160219005Panel · degradedUPON REMOVAL OF THE 315A2130 BLANKET INSTALLATION, VISUAL & ULTRASONIC INSPECTION OF THE 315A2102-174 BONDED PANEL ASSEMBLY, CMM 78-31-26 FIGURE 6 ITEM 45B, REVEALED 3 AREAS OF THERMAL DEGRADATION RESULTING IN DISBOND & DELAMINATION. CT THE 174 BONDED PANEL ASDR Z6WR20160219004Panel · degradedUPON REMOVAL OF THE 315A2130 BLANKET INSTALLATION, VISUAL & ULTRASONIC INSPECTION OF THE 315A2101-174 BONDED PANEL ASSEMBLY, CMM 78-31-26 FIGURE 6 ITEM 40B, REVEALED 3 AREAS OF THERMAL DEGRADATION RESULTING IN DISBOND & DELAMINATION CT THE 174 BONDED PANEL ASSSDR SWIA201641881Relay · failedRT THRUST REVERSER UNLOCK IN FLIGHT, DIVERTED. INSTALLED NEW THROTTLE LOCKOUT/STOW RELAY 2K7K3 INTO JB4. OPS CHECKED GOOD.SDR REXA2016021000193Seal · crackedLOWER EDGE OF LOWER FWD OTBD SEAL ON NR 1 ENG THRUST REVERSER TORQUE BOX IS CRACKED. R & R LOWER EDGE SEAL IAW CMM 78-30-00.SDR DALA2016021100982Band · chafedMAINTENANCE TASK NR 2 ENGINE OTBD THRUST REVERSER V-BAND GROOVE LOWER AREA FOUND CHAFED. PERFORMED BLEND OUT REPAIR IAW PRI 543523-14, REV 0, DATED 01FEB16, 1015 HRS & PRI 543523-14AD, REV 0.SDR VNAA2016020400007Thrust Reverser · warning lightCREW REPORTED INTERMITTENT LT REVERSER UNLOCKED CAUTION MESSAGE IN FLIGHT. MESSAGE WENT FROM INTERMITTENT TO STEADY. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE DEFERRED LT THRUST REVERSER IAW MEL. ACFT RELEASED FOR SERVICE.SDR ASAA2016020415283Switch · failedHISTORY OF NR 2 ENGINE THRUST REVERSER LIGHT ON WHEN STOWED. ACFT GROUNDED. R & R NR 2 AUTO THROTTLE SWITCH PACK ASSY REF AMM 76-11-07-400-802-F00. ACCOMPLISHED ALL TESTS IAW AMM 76-11-07-400-802-F00. ALL TESTS PASS.SDR REXA2016020200144Support Angle · brokenRIGHT UPPER THRUST REVERSER TRACK STAND FAIRING, SUPPORT Z ANGLE BROKEN. R & R SUPPORT Z ANGLE IAW MM 20-42-06.SDR Z6WR20160121003Panel · damagedUPON REMOVAL OF THE 315A2130 BLANKET INSTALLATION, VISUAL AND ULTRASONIC INSPECTION OF THE 315A2102-174 BONDED PANEL ASSY, CMM 78-31-26, FIG 6, ITEM 45B, REVEALS, 2 AREAS OF THERMAL DEGRADATION RESULTING IN DISBOND, DELAMINATION C/T THE -174. BONDED PANEL ASSYSDR Z6WR20160121002Panel · damagedUPON REMOVAL OF THE 315A2130 BLANKET INSTALLATION, VISUAL AND ULTRASONIC INSPECTION OF THE 315A2101-174 BONDED PANEL ASSY, CMM 78-31-26, FIGURE 6, ITEM 40B REVEALS 1 AREA OF THERMAL DEGRADATION RESULTING IN DISBOND, DELAMINATION C/T THE -174 BONDED PANEL ASSY.SDR Z6WR0012016Panel · damagedUPON REMOVAL OF THE 315A2130 BLANKET INSTALLATION, VISUAL AND ULTRASONIC INSPECTION OF THE 315A2101-174 BONDED PANEL ASSY, CMM 78-31-26, FIGURE 6, ITEM 40B, REVEALS 2 AREAS OF THERMAL DEGRADATION RESULTING IN DISBOND, DELAMINATION C/T THE -174 BONDED PANEL ASSSDR SWIA201641768Thrust Reverser · failedLEFT REVERSER UNLOCKED CAUTION MESSAGE IN FLIGHT. RAN QRH, MESSAGE PERSISTED. DIVERTED. R & R LT ENGINE THRUST REVERSER PDU IAW AMM. OPS CHECK GOOD.SDR IPXA2016012698485Skin · chafedINSPECTION TYPE:2C, NR 2 RT T/R CORE COWL AFT UPPER SKIN CHAFE DAMAGE. REPAIRED CHAFE DAMAGE IAW EO MD11-7830- 59559-A AND EA 011-7830-01-A6047, REV IR.SDR FDEA201601050045Bolt · looseNUMBER 3 ENG LT THRUST REVERSER, MOUNTING RING LATCH ASSEMBLY HAS 16 LOOSE BOLTS. QUALITY CONTROL REQUESTS, TORQUE CHECK, ON ALL MOUNTING RING ATTACHMENT FASTENERS. TIGHTENED AND TORQUE CHECKED ALL BOLTS ON MOUNTING RING LATCH ASSY IAW AMM 78-32-11-2.SDR FDEA201601050044Attach Bolt · looseNUMBER 3 ENG LT THRUST REVERSER, UPPER LATCH ATTACH BOLTS LOOSE, 5 EACH. TORQUED UPPER LATCH ATTACH BOLTS IAW AMM 78-32-11-2.SDR CA160105003Thrust Reverser · malfunctioned(CAN) CREW CALLED DX 1HR AFTER ARRIVAL. PATCHED TO MOC TO DISCUSS ISSUE FLT HAD REVERSER 2 PRESSURIZE BROUGHT ENGINE 2 BACK TO IDLE AND RETURNED TO DEPARTURE AIRPORT DECLARED AN EMERGENCY.SDR VNAA2016010300004Warning Message · illuminatedCREW REPORTED LT REVERSER UNLOCKED CAUTION MESSAGE APPEARED INTERMITTENTLY SEVERAL TIMES DURING FLIGHT. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE DEFERRED LT THRUST REVERSER IAW MEL. ACFT RELEASED FOR SERVICE.SDR ZH4R20151230001Beam · corrodedON 12/23/15 OPERATOR REQUESTED THAT A SDR BE SUBMITTED FOR THIS COMPONENT ON EA 542480-14. THE THRUST REVERSER IN QUESTION WAS SENT FOR MAINTENANCE. THE THRUST REVERSER PN 715-0021-505, SN 0131001 WAS A SPARE, REMOVED FROM AIRCRAFT. UPON INSPECTION, THE RT SSDR Z6WR201512220001Panel · burnedUPON REMOVAL OF THE 315A2130 BLANKET INSTALLATION, VISUAL AND ULTRASONIC INSPECTION OF THE 315A2102-177 BONDED PANEL ASSEMBLY, CMM 78-31-26, FIG 6, ITEM 45A, REVEALS, 8 AREAS OF THERMAL DEGRADATION RESULTING IN DISBOND, DELAMINATION C/T THE-177 BONDED PANEL ASSDR Z6WR20151222013Panel · burnedUPON REMOVAL OF THE 315A2130 BLANKET INSTALLATION, VISUAL & ULTRASONIC INSPECTION OF THE 315A2101-177 BONDED PANEL ASSEMBLY, CMM 78-31-26 FIGURE 6 ITEM 45B, REVEALS 7 AREAS OF THERMAL DEGRADATION RESULTING IN DISBOND & DELAMINATION CT -177 BONDED PANEL ASSEMBLSDR Z6WR20151222012Panel · burnedUPON REMOVAL OF THE 315A2130 BLANKET INSTALLATION, VISUAL & ULTRASONIC INSPECTION OF THE 315A2101-174 BONDED PANEL ASSEMBLY, CMM 78-31-26 FIGURE 6 ITEM 40B, REVEALS 9 AREAS OF THERMAL DEGRADATION RESULTING IN DISBOND & DELAMINATION CT -174 BONDED PANEL ASSEMBLSDR Z6WR20151222011Panel · burnedUPON REMOVAL OF THE 315A2130 BLANKET INSTALLATION, VISUAL & ULTRASONIC INSPECTION OF THE 315A2102-174 BONDED PANEL ASSEMBLY, CMM 78-31-26 FIGURE 6 ITEM 45B, REVEALS 8 AREAS OF THERMAL DEGRADATION RESULTING IN DISBOND & DELAMINATION CT-174 BONDED PANEL ASSEMBLYSDR Z6WR20151222010Panel · burnedUPON REMOVAL OF THE 315A2130 BLANKET INSTALLATION, VISUAL & ULTRASONIC INSPECTION OF THE 315A2101-174 BONDED PANEL ASSEMBLY, CMM 78-31-26 FIGURE 6 ITEM 40B, REVEALS 13 AREAS OF THERMAL DEGRADATION RESULTING IN DISBOND & DELAMINATION CT -174 BONDED PANEL ASSEMB
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