N79748, cancelled May 4, 2011
Service difficulty reports · 107
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. 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 n_number = 'N79748' AND deregistration_id = 'N79748-2011-05-04' 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 n_number = 'N79748' AND deregistration_id = 'N79748-2011-05-04' 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 GAIA04047OPControl Column · bindingDURING CRUISE FLIGHT, A BINDING OF THE CONTROL YOKE WAS NOTED IN A ROLL TO THE RIGHT. SPOILERS WERE CYCLED AND ABOVE PROBLEM WAS CORRECTED BUT LATER DID RETURN. FLT WAS COMPLETED AND AN UNEVENTFUL LANDING WAS MADE. INSPECTED AND CHECK FLIGHT CONTROLS AILEROSDR GAIA04037OPComputer · malfunctionedFLT 578 - SFO-PHX-FWA - AUTOPILOT DIFFICULT TO ENGAGE IN CRUISE. REMOVED AND REPLACED THE PITCH CHANNEL COMPUTER. THE SYSTEM OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR GAIA04024OPFire Loop · looseTHE NR 3 ENGINE GROUND FAULT LIGHT CAME ON DURING TAXI AT SFO. INSPECTED AND CHECKED NR 3 ENGINE FIRE LOOP CLEANED AND RESECURED CONNECTORS. THE SYSTEM OPERATIONALLY CHECKED GOOD NO DEFECTS FOUND. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR GAIA03116OPLight · inoperativeDURING ROUTINE MAINTENANCE AT FWA, IT WAS DISCOVERED THAT THE MAIN ENTRY EMERGENCY EXIT LIGHT DID NOT ILLUMINATE. REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT. OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR GAIA03007OPIndicator · false indicationFLT 879 - RNO-SJC - DURING CRUISE, THE FLIGHT CREW NOTICED THAT THE OIL QUANTITY ON NR 2 ENGINE WAS STEADILY DECREASING. THE CREW DECLARED AN EMERGENCY AND MADE A PRECAUTIONARY SHUT DOWN OF THE NR 2 ENGINE. DURING APPROACH THE OIL QUANTITY RETURNED TO NORMALSDR GAIA02100STHinge · crackedDURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE FORWARD MAIN CARGO DOOR HINGE WAS CRACKED. INSTALLED NEW HINGE SECTION PER AEI SERVICES BULLETIN 01-01. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR GAIA02093STFrame · dentedDURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE FUSELAGE FRAME WAS DENTED JUST ABOVE FLOOR LEVEL RIGHT MAIN CARGO COMPARTMENT BS 600. CUT OUT DAMAGED AREA OF FRAME IAW B727 SRM 51-40-3 FIGURE 1, FABRICATED REPAIR DOUBLER IAW B727 SRM 51-40-3 AND 53-10SDR GAIA02101STHinge · crackedDURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE AFT MAIN CARGO DOOR HINGE WAS CRACKED. INSTALLED NEW HINGE SECTION AEI SERVICE BULLETIN 01-01. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR GAIA02081STDoor Frame · corrodedDURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT AT THE E/E ACCESS, THE AFT DOOR LOCKING FRAME HAD CORROSION AT THE FRAME TO SKIN AT BS 460, STRINGER S29L TO S28L. REMOVED FRAME DAMAGE, AND REPAIRED PER BOEING SRM 51-10-2 FIGURE 3. THE AIRCRAFT WAS RETURNSDR GAIA02083STSkin · dentedDURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE FUSELAGE EXTERIOR NOSE SECTION AT BS 310 THROUGH 330 BETWEEN STRINGERS 21R TO STRINGER 22R SKIN WAS DENTED. CUT OUT DAMAGED AREA. FABRICATED DOUBLER AND FILLER TREATED AND PRIMED AREA IAW SRM 53-30-3 FISDR GAIA02085STStringer · crackedDURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT IN THE MAIN CARGO COMPARTMENT INTERIOR AT BS 720B HAD A CRACK AT STRINGER S15L FORWARD OF WING LIGHT SUPPORT. CUT OUT DAMAGED AREA, FABRICATED NEW PART IAW B727 SRM 53-10-3, FIG 5. THE AIRCRAFT WAS RETURNEDSDR GAIA02086STStringer · crackedDURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE MAIN CARGO COMPARTMENT INTERIOR BS 720B HAD A CRACK AT STRINGER S15R END, FORWARD OF WING LIGHT SUPPORT. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED NEW PART IAW B727 SRM 53-10-3, FIGURE 5. THE AIRCRASDR GAIA02091STFrame · dentedDURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE FUSELAGE FRAME WAS DENTED JUST ABOVE FLOOR LEVEL AT THE RIGHT SIDE MAIN CARGO COMPARTMENT BS 560. CUT OUT DAMAGED AREA OF FRAME IAW B727 SRM 51-40-3, FIGURE 1. FABRICATED DOUBLER IAW B727-SRM 51-40-3, FSDR GAIA02092STFrame · dentedDURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE FUSELAGE FRAME WAS DENTED JUST ABOVE FLOOR LEVEL AT THE RIGHT MAIN CARGO COMPARTMENT BS 580. CUT OUT DAMAGED AREA OF FRAME IAW B727 SRM 51-40-3, FIGURE 1. FABRICATED DOUBLER IAW B727 SRM 51-40-3 AND 53-SDR GAIA02090STFrame · dentedDURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE FUSELAGE FRAME DENTED JUST ABOVE FLOOR LEVEL RIGHT CABIN BS 540. CUT OUT DAMAGED AREA OF FRAME IAW B727 SRM 51-40-3 FIGURE 1. FABRICATED DOUBLER IAW B727 SRM 51-40-3, FIGURE 1 AND 53-10-2 FIGURE 2. THESDR GAIA02089STFrame · crackedDURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE BS 360, FRAME INBOARD FLANGE WAS DENTED AND CRACKED IN THE AREA OF STRINGER 16 LEFT. CUT OUT DAMAGED AREA IAW B727 SRM 51-40-3, FIG 1 FABRICATED DOUBLER IAW B727 SRM 51-20-1 AND 51-40-3 FIG 1. THE AIRCASDR GAIA02088STFrame · dentedDURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE FORWARD CARGO COMPARTMENT, THE FRAME AT BS 680 HAS THREE DENTS INTO THE RADIUS OF STRINGERS S25L TO S23L. COLD WORKED DENTS, NDT FOUND NO CRACKS, FABRICATED DOUBLER REPAIR IAW B727 SRNM 51-40-3, FIGURE 1SDR GAIA02087STPlenum · corrodedDURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE LEFT AFT PLENUM LOWER SKIN HAS CORROSION IN TWO PLACES. FOUND CORROSION OUT OF LIMITS. INSTALLED DOUBLER AND TRIPLER IAW B727 SRM 57-30-3 FIGURE 8. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR GAIA02084STSkin · dentedDURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THERE WAS A DENT IN THE SKIN AT BS 1130, STRINGER 27L. REMOVED OLD REPAIR CUT OUT DAMAGED AREA INSTALLED FILLER, DOUBLER AND TRIPLER PER BOEING SRM 53-30-3, FIGURE 5. THE AIRCRAFT WAS RETURNED TO SERVICE. SDR GAIA02082STSkin · dentedDURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THERE WAS A DENT IN THE SKIN AT BS 1090, STRINGER S15R. CUT OUT DAMAGED AREA FABRICATED DOUBLER IAW B727 SRM 53-30-3, FIGURE 1, SHEET 2, PATE 6. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR GAIA02080STSkin · dentedDURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE FORWARD LOWER CARGO DOOR CUTOUT FRAME AND SKIN WAS DENTED NEAR STRINGER S23R AT THE FORWARD PORTION OF THE DOOR CUTOUT FRAME (FUSELAGE SKIN). C/A: ACCOMPLISHED REPAIR IAW REPAIR ORDER. AIRCRAFT WAS RETSDR GAIA01314OPFrame · chafedFLT - 3850 - MSP-FWA - DURING CRUISE, THE FLIGHT CREW NOTICED THAT THE 'A' SYSTEM HYDRAULIC FLUID QUANTITY WAS DECREASING. AN EMERGENCY WAS DECLARED AND THE HYDRAULIC SYSTEM WAS ISOLATED THE AIRCRAFT CONTINUED TO FWA. THE AIRCRAFT MADE AN UNEVENTFUL LANDING.SDR GAIA01313OPHydraulic Line · crackedFLT 3850 - MSP-FWA - DURING CRUISE, THE FLIGHT CREW NOTICED THAT THE 'A' SYSTEM HYDRAULIC SYSTEM WAS ISOLATED THE AIRCRAFT CONTINUED TO FWA. THE AIRCRAFT MADE AN UNEVENTFUL LANDING. INSPECTION REVEALED A CRACKED HYDRAULIC LINE AT FUSELAGE STATION 1303. THE SDR GAIA01238STLight · not seatedMAINTENANCE FOUND EMERGENCY EXIT LIGHTS INOPERATIVE. FOUND LIGHT ASSEMBLY NOT SEATED IN CONNECTOR. REINSTALLED AND OPERATIONALLY CHECKED SYSTEM. SYSTEM CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M)SDR GAIA01156OPHydraulic Line · leakingFLT 1850 - PDX-SEA - UPON LANDING GEAR EXTENSION, LOST A SYSTEM HYDRAULICS QUANTITY WENT TO ZERO. AIRCRAFT MADE AN UNEVENTFUL LANDING IN SEA. INSPECTION OF AIRCRAFT FOUND LEAKING LEFT GEAR DOOR ACTUATOR RETURN HOSE. REMOVED AND LEFT ACTUATOR RETURN HOSE. REMSDR GAIA01073BOPLine · rupturedFLT 1805 - FWA-LAX - AT FL310, HYDRAULIC SYSTEM ''A'' PRESSURE AND QUANTITY WENT TO ZERO. AIRCRAFT MADE AN UNEVENTFUL LANDING IN DEN. TROUBLESHOOT AND FOUND RUPTURED HYDRAULIC LINE IN RIGHT SIDE OF AFT AIRSTAIR. REMOVED AND REPLACED THE HYDRAULIC LINE PER BSDR GAIA00800Line · leakingFLT 3712 - FWA-ELP - SYSTEM ''A'' HYDRAULIC PRESSURE AND QUANTITY DROPPED TO ZERO ON CLIMB-OUT. AIRCRAFT MADE AN UNEVENTFUL RETURN TO FWA. FOUND NR 2 ENGINE ''A'' SYSTEM RETURN LINE LEAKING. INSTALLED FLEX LINE AND PERFORMED ENGINE RUN. NO LEAKS NOTED AND SDR GAIA00688Light · inoperativeNO FLIGHT. DURING ROUTINE MAINTENANCE, DISCOVERED THE L-1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY. OPERATIONALLY CHECKED GOOD. THE AIRCRAFT RETURNED TO SERVICE. (X)SDR GAIA00491Rod End · shearedDISCREPANCY: TAKE OFF ABORTED AT 70 KTS DUE TO VIOLENT NOSE WHEEL SHIMMY.CORRECTIVE ACTION: FOUND NOSE GEAR TORQUE LINKS TO BE DISCONNECTED CAUSING EXCESSIVE SHIMMY, RE-CONNECTED AS REQUIRED. UPON FURTHER INSPECTION FOUND NOSE WHEEL STEERING BYPASS LINKAGE RODSDR GAIA00125Light · inoperativeFOUND DURING PREFLIGHT, FLIGHT DECK EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED EMEREGNCY EXIT LIGHT ASSEMBLY. OPERATIONALLY CHECKED SYSTEM GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR GAIA0052Light · inoperativeFLT 1849 - MSP-SEA - ENCOUNTERED DURING CRUISE, THE EMERGENCY EXIT LIGHTS REMAINED DIMLY ILLUMINATED. TURNED SWITCH ON AND LIGHTS ALL ILLUMINATED BRIGHTLY, BUT COULD NOT TURN OFF. THE FILGHT CONTINUED TO SEA AND LANDED SAFELY WITHOUT ANY FURTHER DIFFICULTIESSDR GAIA0043Light · unsecureDURING ROUTINE MAINTENANCE AT TYS,THE COCKPIT EMERGENCY EXIT LIGHT ASSEMBLY WAS FOUND UNSECURED. REINSTALLED COCKPIT EMERGENCY LIGHT ASSEMBLY. OPERATIONALLY CHECKED NORMAL. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR GAIA0042Bulb · failedFOUND DURING ROUTINE MAINTENANCE AT MIA, THE LIGHT BULB INOPERATIVE FOR THE MAIN CABIN DOOR EMERGENCY EXIT LIGHT. REMOVED AND REPLACED BULB AT THE MAIN CABIN DOOR EMERGENCY EXIT LIGHT. OPERATIONALLY CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR GAIA0020Stringer · damagedFOUND DURING ZERO B, TRANSITION CHECK AT AVBORNE HEAVY MAINTENANCE FACILITY, PRIOR TO THIS AIRCRAFT BEING ON THE KHA CERTIFICATE, DAMAGE WAS FOUND ON STRINGER 28R FROM BODY STATION 682 TO STATION 694. INSTALLED STRINGER REPAIR FROM STATION 682 TO STATION 694,SDR GAIA0021Skin · damagedFOUND DURING ZERO B, TRANSITION CHECK AT AVBORNE HEAVY MAINTENANCE FACILITY, DAMAGE WAS FOUND ALONG FUSELAGE SKIN FROM STATION 697 TO 708, BETWEEN STRINGER 28L AND STRINGER 28R. INSTALLED EXTERNAL DOUBLER REPAIR FROM STATION 697 TO STATION 708, BETWEEN STRINGSDR GAIA0022Skin · damagedFOUND DURING ZERO B, TRANSITION CHECK AT AVBORNE HEAVY MAINTENANCE FACILITY, DAMAGE WAS FOUND ON EXTERIOR SKIN FROM STATION 575 TO 588 STRINGER 26L TO 27L. INSTALLED EXTERIOR FUSELAGE SKIN REPAIR FROM STATION 575 TO 588, STRINGER 26L TO 27L. MATERIAL USED 20SDR GAIA0023Stringer · damagedFOUND DURING ZERO B, TRANSITION CHECK AT AVBORNE HEAVY MAINTENANCE FACILITY, DAMAGE WAS FOUND ALONG STRINGER AT STRINGER 27L FROM STATION 573 TO 588. INSTALLED STRINGER REPAIR AT STRINGER 27L FROM STATION 573 TO STATION 588. MATERIAL USED, PART NR BAC1498-14SDR GAIA0024Floorbeam · damagedFOUND DURING ZERO B, TRANSITION CHECK AT AVBORNE HEAVY MAINTENANCE FACILITY, DAMAGE WAS FOUND ON FLOORBEAM UPPER T CHORD AT STATION 344 FROM LBL 62.62 TO RBL 62.62. INSTALLED FLOORBEAM UPPER T CHORD REPAIR AT STATION 344 FROM LBL 62.62 TO RBL 62.62. MATERIALSDR CALA9901293Panel · crackedINSPECTION FOUND TWO 3 CRACKS IN VERTICAL STABILIZER SADDLE PANEL. THE SADDLE PANEL WAS REMOVED, REPAIRED IAW SRM 55-30-7, FIGURE3, AND REINSTALLED IAW MM 55-30-1, PAGE 201.SDR CALA9901291Skin · corrodedINSPECTION FOUND NR 5 L/E FLAP BULL NOSE CORRODED. THE FLAP BULL NOSE WAS REMOVED AND REPLACED IAW MM 27-81-1, PAGE 401.SDR CALA9901287Skin · crackedINSPECTION FOUND A 2 INCH CRACK IN LT WING NR 7 SPOILER PANEL SKIN WITH DENTS ON LOWER SURFACE. THE SPOILER PANEL WAS REMOVED, REPAIRED, AND REINSTALLED IAW SRM 57-30-00, PAGE 30 AND MM 27-62-1, PAGE 403.SDR CALA9901290Fitting · crackedINSPECTION FOUND A 1.5 CRACK IN RT MLG BEAM SUPPORT FITTING. THE SUPPORT FITTING AND BUSHING WERE REMOVED AND REPLACED IAW ECRA 5740-01102.SDR CALA9901289Skin · debondedINSPECTION FOUND LT WING NR 2 SPOILER UPPER SKIN DEBONDED WITH SURFACE CORROSION AROUND SCREW HEADS. THE NR 2 SPOILER PANEL WAS REMOVED AND REPLACED IAW MM 27-61-1, PAGE 407.SDR CALA9901288Battery Pack · dischargedINSPECTION FOUND CABIN EMERGENCY AISLE PATH LIGHTING INOPERATIVE. MAINTENANCE FOUND A BLOWN FUSE AND INOPERATIVE BATTERY. THE FUSE AND BATTERY PACK WERE REMOVED AND REPLACED IAW MM 33-50-1.SDR CALA9901270Fitting · corrodedINSPECTION FOUND RT MLG BEAM H FITTING ATTACH HOLE AND UPPER FORWARD LUG CORRODED. THE ATTACH HOLE WAS REPAIRED IAW ECRA 5740-01903, PAGE 2 AND THE FITTING WAS REPLACED.SDR CALA9901269Fitting · crackedINSPECTION FOUND A .75 INCH CRACK IN RT WING REAR SPAR O/B ATTACH FITTING FOR MLG. THE FITTING WAS REMOVED AND REPLACED IAW ECRA 5740-01901.SDR CALA9901268Track · corrodedINSPECTION FOUND RT WING NR 5 FLAP TRACK CORRODED. THE FLAP TRACK WAS REMOVED AND REPLACED IAW MM 27-51-31, PAGE 402-410.SDR CALA9901130Casting · crackedINSPECTION FOUND A 1 INCH CRACK IN RT FORWARD OVERWING DOOR INNER UPPER CASTING. THE CASTING WAS REMOVED AND A NEW CASTING WAS INSTALLED IAW SRM 51-30-2, FIGURE 1.SDR CALA9901103Battery Pack · dischargedINSPECTION FOUND FORWARD OVERHEAD EMERGENCY LIGHT AT ROW NR 2 INOPERATIVE. MAINTENANCE FOUND THE BATTERY PACK AT FAULT. THE BATTERY PACK WAS RECHARGED AND REINSTALLED. OPERATION CHECKED GOOD IAW MM 33-50-81, PAGE 403.SDR CALA9901102Fitting · corrodedINSPECTION FOUND FORWARD END OF LT WING NR 4 FLAP TRACK FITTING CORRODED. THE FITTING WAS REMOVED AND REPLACED. THE FLAP TRACK WAS REINSTALLED IAW MM 27-51-72, PAGE 401.
Back to N79748, cancelled May 4, 2011