JASC 7800
Service difficulty reports · 281
Reports filed under 7800 · Engine Exhaust System, 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 = '7800' 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 = '7800' 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 2026FA0000037Channel · crackedDURING MAINTENANCE INSPECTIONS AT IAI FACILITIES SHOP FOUND A CRACK ON CHANNEL. DAMAGED AND ENLARGED FASTENER HOLES ON OUTER SKIN FAIRING. WORK PERFORMED IAW REA MF03036R0216.SDR 2025FA0000514Exhaust Pipe · inflt separationHEATSHIELD IS LOOSE ON THE EXHAUST PIPE TTSN 31.9 HOURSSDR ENHA20250522001Muffler · leakingPILOT REPORTED CO DETECTOR INDICATING. MECHANICS FOUND THE RIGHT HAND MUFFLER COUPLING LEAKING. MECHANICS REPLACED THE ATTACHING HARDWARE.SDR 2025FA0000270Exhaust Pipe · separatedAD2018-10-10 DATED JUNE 12 2018 REQUIRES THE HEAT SHIELD TO BE TIGHT ON THE AND WELDED TO THE EXHAUST PIPE. THE HEAT SHIELD SPOT WELDS FAILED AND VERY LOOSE ON THE EXHAUST PIPE. THE AD IS SUGGESTING THE PIPE SHOULD LAST AT LEAST 1500.0 HOURS BUT FAILED AT 16.9SDR 2025FA0000269Exhaust Pipe · separatedAD2018-10-10 DATED JUNE 12 2018 REQUIRES THE HEAT SHIELD TO BE TIGHT ON THE AND WELDED TO THE EXHAUST PIPE. THE HEAT SHIELD SPOT WELDS FAILED AND VERY LOOSE ON THE EXHAUST PIPE. THE AD IS SUGGESTING THE PIPE SHOULD LAST AT ;LEAST 1500.0 HOURS BUT FAILED AT 145SDR 2025FA0000268Exhaust Pipe · separatedAD2018-10-10 DATED JUNE 12 2018 REQUIRES THE HEAT SHIELD TO BE TIGHT ON THE AND WELDED TO THE EXHAUST PIPE. THE HEAT SHIELD SPOT WELDS FAILED AND VERY LOOSE ON THE EXHAUST PIPE. THE AD IS SUGGESTING THE PIPE SHOULD LAST AT ;LEAST 1500.0 HOURS BUT FAILED AT 23.SDR 2025FA0000134Muffler · crackedCREW REPORTS EXHAUST SMELL IN CABIN. VISUAL INSPECTION FOUND MUFFLER CRACKED.SDR VNAA202408070007Coaming · crackedRH UPPER TRANSCOWL LATCH COAMING IS CRACKED. REMOVED AND REPLACED COAMING IAW MHIRJ REO 670-54-21-1647 REV -A DATED 2024-06-17."SDR SWAA2024071512651Tailpipe · fireTAIL PIPE FIRE ENGINE #1. EXTINGUISHED ON ITS OWN<[01] INSPECTED #1 ENGINE INLET & EXHAUST. FOUND OIL ACCUMULATION IN CENTER EXHAUST PLUG CAVITY. NO OTHER DEFECTS NOTED. OILE CONSUMPTION & PSI ARE WITHIN NORMAL LIMITS. REF FIM 71-05 TASK 811. POWERPLANT ENGINESDR MK1Y20240602008Sleeve · unknownREPAIR - ENG #2, PW4060, PRIMARY EXHAUST SLEEVE.SDR SWAA2024042477722Tube · leakingDECLARED EMERGENCY, SUSPECT LEAK #1 ENGINE<[01] R&R CENTER VENT TUBE EXTENSION AND MIXER IAW AMM 78-11-03 AND REMOVED AND REINSTALLED AFT PLUG IAW AMM 78-11-02.SDR SWAA2024042478765Mixing Unit · leakingDECLARED EMERGENCY, SUSPECT LEAK #1 ENGINE<[01] R&R CENTER VENT TUBE EXTENSION AND MIXER IAW AMM 78-11-03 AND REMOVED AND REINSTALLED AFT PLUG IAW AMM 78-11-02.SDR SWAA2024042478766Plug · leakingDECLARED EMERGENCY, SUSPECT LEAK #1 ENGINE<[01] R&R CENTER VENT TUBE EXTENSION AND MIXER IAW AMM 78-11-03 AND REMOVED AND REINSTALLED AFT PLUG IAW AMM 78-11-02.SDR CALA2024010800052Unknown · unknownAFTER POWER UP ON T/O ROLL-MOMENTARY RT ENG REVERSER LIGHT-RTO COMPLIED WITH DDP DDP COMPLIED WITH DISPATCH DESK: 24 NAME: DS DATE: 04-JAN-24- NOC DESK: 757 NAME: MC DATE: 04-JAN-24- RIGHT REVERSER INOP. CYCLED THRUST REV. 6 TIMES AND COULD NOT DUPLICATE FAULTSDR CALA2023111603401Unknown · unknownDURING T/O ROLL AFTER T/O THRUST APPLIED HAD MOMENTARY RIGHT THRUST REV LIGHT. ACCOMPLISHED #2 ENGINE THRUST REVERSER DEACTIVATION PER MEL CARD AS REQUIRED. REQUESTING MEL. PLACARD APPLIED TO INST PANEL. 78005 AND AMM 78-31-00-201. CB ON P11 AND P6 PULLED ANDSDR CALA2023111603405Unknown · unknownRIGHT REVERSER AMBER LIGHT ILLUMINATED AT 115KTS ON TAKEOFF FOUND NO MESSAGE UNDER STATUS PAGE OR UNDER ECS/MSG ON P61. PERFORMED T/R OPERATIONAL CHECKS IAW 78-30-00-715-037-R04 WITH NO DEFECTS NOTED. PERFORMED TASK MULTIPLE TIMES WITH SAME RESULTS. INSPECTED SDR 2023FA0000677Unknown · unknownFOUND EXISTING DOUBLER REPAIR ON ENGINE #1 PRIMARY EXHAUST SKIN AT LH SIDE.SDR 2023FA0000659Unknown · unknownENG #1 EXHAUST OUTER SLEEVE S/N 0468-A P/N 015T0305-10: NRC M0769 DENT WITH SHARP CREASE IN THE OUTER EXHAUST SKIN LOCATED BT 7-8 O’CLOCK AND BT NAS STA 331.47-337.32. DENT SIZE: 2.42”(A)X0.125(Y) A=2.42” Y=0.125” A/Y RATIO 19.3. SDR 2023FA0000654Unknown · unknownDURING MAINTENANCE INSPECTION SHOP FOUND ON ENG #1, THRUST REVERSER, AT JUNCTION OF TWO (2) PANELS, LOWER REAR PART, MISSING FILLER MATERIAL. DAMAGES DIMENSIONS: LENGTH: 2.6”, WIDTH: 1.2”.SDR 2023FA0000646Unknown · unknownDURING MAINTENANCE INSPECTION SHOP FOUND ON ENG #1, THRUST REVERSER, AT JUCTION OF BOTH SIDE OF C-DUCT, LOWER REAR PARTS, MISSING FILLER MATERIAL. DAMAGES DIMENSIONS: LENGTH: 3”, WIDTH: 1”.SDR CALA2023102503168Actuator · faultyL REV CAUTION ON TAKEOFF .REV CAUTION OUT AFTER THROTTLE RETARDED MEL TO BE APPLIED WITH TOMC APPROVEL REV ISOL VALVE PIN INSTALLED , MECH DEACT PINS INSTALLED , LEFT ENG SYNC LOCK P11 PULLED AND SAFETIED. PLACARD INSTALLED FWD OF THROTTLE THRUST REV INOP PERFSDR YV3R2023082800578Shield · crackedCUSTOMER REPORTED SHIELD ASSEMBLY P/N: D314-1 WAS FOUND CRACKED..SDR JJBA20230823021Unknown · unknownAT LH TR ASSY, AFT OUTBD SIDE, CORROSION SUSPECTED UNDER SKIN. LH TR ASSY REMOVED AND REPLACED. OPS CHECK SAT.SDR ENHA LP233910Seal · leakingLEFT ENGINE BLUBBERED THEN DIED WHILE TURNING AROUND TO TAKEOFF. MECHANICS FOUND #1 CYLINDER SPARK PLUGS FOULED AND WET WITH GAS. MECHANICS REPLACED ALL PARK PLUGS ON LEFT HAND ENGINE. MECHANICS FOUND #1 INTAKE TUBE O-RING PINCHED AND ROLLED, MECHANICS REPLACSDR YV3R2023061400570Shield · crackedCUSTOMER REPORTED SHIELD ASSEMBLY P/N: D314-1 WAS FOUND CRACKED.SDR UIEA2023051000446Duct · unknownNO.1 ENG LH C-DUCT FWD V BLADE UPPER AREA CRACK(<P>C-DUCT REPLACED AS PER AMM 78-31-01 REV 107 DATE : 15 MAR 2023.</P>)SDR YV3R2023051600568Shield · crackedCUSTOMER REPORTED SHIELD ASSEMBLY P/N: D314-2 WAS FOUND CRACKED.SDR ABXA2023042467Unknown · unknownLH REV ISLN VLV MSG DISPLAYED,DURING, LH ENG START. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE DEFERRED THE L/H T/R IAW MEL 78-31-1A. MX PROCEDURES C/W. PLACARD INSTALLED. AIRCRAFT RETURNED TO SERVICE.SDR CALA2023041201105Thrust Reverser · unknownPDA 3 #1 ENGINE THRUST REVERSER O/B AFT UPPER SIDE HAS 9 FASTENERS MISSING. SEE PHOTO. ADDED PHOTO. INSTALLED NEW FASTENERS REF. SRM 51-40-02, NO DAMAGE TO PANEL NOTED, OK FOR SERVICE.SDR UIEA2023040300304Switch · unknownON TAKE-OFF, N1 ON #1 ENGINE ONLY PRODUCED 42% THRUST(<P>FOUND #1 THRUST REVERSER POSITION FEEDBACK SENSOR OUT OF ADJUSTMENT READING 28.0. ADJUSTED IAW B747-700 AMM 78-34-10. READING 0.0 NOW. DIRECTLY RELATED TO DMI 182884 ON LP 1777901 P1 PER MEL 78-31-01A CASDR HALA2023032100009Unknown · unknownREPORTED #1 ENGINE TAILPIPE FIRE. ACCOMPLISHED AMM 72-00-00-210-817-A. VISUAL INSPECTION OF ENG AFTER FIRE NO DEFECTA NOTED.SDR 2023FA0000201Muffler · failedCARBON MONOXIDE INDICATION ON ON MAP DISPLAY ON FOREFLIGHT FROM SENTRY PLUS ADS-B RECEIVER. IMMEDIATELY CAME ON WHEN HEAT WAS PULLED ON. TURNED OFF HEAT, OPENED ALL VENTS AND VERIFIED THE SENTRY RETURNED TO NORMAL. SCHEDULE AN INSPECTION WHICH DISCOVERED A HOSDR UIEA2023022400192None · noneNO.4 ENG LH T/R OPEN ACTUATOR ATT POINT BOLT HOLE FOUND ELONGATED.(<P>NO.4 ENG LH T/R OPEN ACTUATOR ATT POINT REPAIRED IAW CMM 78-32-02 REV.62</P>)SDR UIEA2023022200175Support Ring · noneNO.4 ENG L/H T/R AFT CASCADE SUPPORT RING 11 O'CLOCK FOUND CRACK FORWARD OF BOLT HOLE.(<P>SUPPORT RING REPLACEMENT CARRIED OUT AS PER ATLAS AIR EO: 1978A084 REV.3 PART 1.</P>)SDR UIEA2023022000142None · noneNO.3 ENG L/H T/R IDG SERVICE DOOR AFT 2EA LATCH ATT SKIN FOUND WEAR.(<P>2EA WEAR SKIN AREA REPAIRED AS PER ST ENGINEERING CMM 78-32-02 REPAIR 45.</P>)SDR IXXA2023040303Rib · gouged#2 ENGINE OUTBOARD THRUST REVERSER INSIDE FWD STIFFENER GOUGEDSDR YV3R2023031500553Shield · crackedCUSTOMER REPORTED SHIELD ASSEMBLY P/N: D314-2 CRACKED.SDR SROM110220222None · crackedLH NACELLE EXHAUST SHROUD SPRING CLIPS CRACKED AT 2 LOCATIONS (P/N 8Z9029-103). CRACKS ARE OUTSIDE OF MANUFACTURES LIMITS REQUIRING PART REPLACEMENT.SDR UIEA2022102201169None · noneTHREE DENTS ON ENGINE #2 PRIMARY EXHAUST OUTER SKIN BETWEEN 6/8 O´CLOCK AND BETWEEN NAC STA 323.42/344.67(<P>WELD FILL REPAIR IAW BOEING MSG: CMA-TLS-22-0022-02B</P>)SDR CALA2022102402930None · missingPDA 3 FOUND ON WALK AROUND: #1 ENGINE COMMON EXHAUST NOZZLE APPOX 1 O''CLOCK IS MISSING METAL. SEE PICS ADDED PICS ADD PIC REMOVED NUMBER 1 ENG COMMON NOZZLE ASSEMBLY REF AMM 71-11-11-00-010A. REMOVED AND REPLACED CNA ASSY REF AMM 78-11-11 ALL CHECKS GOOD AT TSDR 2022FA0000618Muffler · crackedNEWLY "OVERHAULED" MUFFLER CRACKED AFTER ONLY 81.3 HOURS OF OPERATION. VISIBLE INDICATION OF FAILURE WAS EXHAUST SOOT ON THE EXTERIOR OF THE MUFFLER SHROUD. MUFFLER WAS SOLD AS OVERHAULED WITH FORM 8130-3 AND WORK ORDER WHILE ALL PARTS APPEARED TO BE MANUFACTUSDR CALA2022091402347None · noneREVERSER UNLOCK INDICATI ON DURING TAKEOFF. REJ ECTED AT AROUND 100KTS. BTS GOT TO 4 AT HIGHEST DEACTIVATED AND SECURED LEFT ENGINE THRUST REVERSER PER MEL DDP IS COMPLIED WITH, PLACED MEL. 7831E. REQUEST MEL. DISPATCH DESK: 3316 NAME: DUY DATE: 08-SEP-22- NOSDR CALA2022091202343Eec · inoperativePILOT REPORTS E1 REV FAULT. DIVERSION INTO BNA. THRUST REVERSER HAS BEEN DEACTIVATED AND SECURED IN THE FWD THRUST (STOWED AND LOCKED) POSITION. REMOVED AND REPLACED #1 ENGINE EEC. ACCP IDT INSPECTION OF EEC INSTALLATION SAFETY AND SECURITY. IDT EEC OP CHK PASSDR CALA2022091202338None · missingPDA 3 #2 ENG PRIMARY EXH NOZZLE OUTBD SIDE FWD FENCE HAS ELONGATED HOLES IN NOZZLE ITSELF AND THE FENCE AND MISSING HI-LICK FASTENER. REMOVED AND REPLACED PRIMARY NOZZLE.SDR SWIA202266633None · chafedL/H UPPER TRANSCOWL COAMING IS CHAFED AT FWD EDGE. (C-CHECK RO 10/24/2022) PERMANENTLY REPAIRED L/H UPPER TRANSCOWL COAMING AT FWD EDGE REF GENERIC REO #670-54-21-1028 REV (NC) 2009-06-15 STEPS 1-9. COMPLIED WITH SKY CARD 51-900-1002-SKY.SDR SWIA202266632None · chafedL/H LOWER TRANSCOWL COAMING IS CHAFED AT FWD EDGE. (C-CHECK RO 10/24/2022) COMPLIED WITH REO REPAIR REF REO 670-54-21-1028 DATED 2009-06-15 REV NC. COMPLIED WITH 51-900-1002-SKY. ALL CHECKS GOODSDR SWIA202266631None · chafedR/H LOWER TRANSCOWL COAMING CHAFED AT FWD EDGE. (C-CHECK RO 10/24/2022) REPAIRED R/H LOWER TRANSCOWL COAMING AT FWD EDGE. REF REO 670-54-21-1028, REV. NC, DATED 2009-06-15. CHECKS GOOD. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.SDR SWIA202266630None · wornR/H LOWER TRANSCOWL FWD AND AFT LATCH BEARING PADS ARE WORN. (C-CHECK RO 10/24/2022) REMOVED AND REPLACED FWD. AND AFT. LATCH BEARING PADS P/N CN624-2130-201. UPON REMOVAL FOUND AFT. C-CHANNEL STIFFENER TO BE WORN. REMOVED AND REPLACED C-CHANNEL STIFFENSDR SWIA202266629None · chafedR/H UPPER TRANSCOWL COAMING CHAFED AT FWD EDGE. (C-CHECK RO 10/24/2022) REPAIRED R/H UPPER TRANSCOWL COAMING AT FWD EDGE. REF REO 670-54-21-1028, REV. NC, DATED 2009-06-15. COMPLIED WITH 51-900-1002-SKY. CHECKS GOOD.SDR SWIA202266628None · wornR/H UPPER TRANSCOWL LATCH DOOR HAS EXCESSIVE PLAY AT HINGE POINT. (C-CHECK RO 10/24/2022) ON R/H UPPER TRANSCOWL LATCH-DOOR, REMOVED WORN PARTS & INSTALLED NEW 1 EA. HINGE HOUSING P/N CN624-2030-205, 4 EA. BUSHING P/N CN624-2027-201, 8 EA. BOLT P/N B02
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