N708AA
Service difficulty reports · 80
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 = 'N708AA' AND registry_match = 'registration' 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 = 'N708AA' AND registry_match = 'registration' 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 C8GA2011000028Proximity Switch · faultedDURING CLIMB, ON GEAR RETRACTION THE RED NOSE GEAR LIGHT REMAINED ILLUMINATED. THE GEAR LEVER WAS CYCLED TO THE OFF POSITION, RED NOSE LIGHT REMAINED ILLUMINATED WITH THE GREEN NOSE GEAR DOWN LOCK LIGHT ILLUMINATED. THE ACFT RETURNED TO DEPARTURE AND LANDED WISDR C8GA201111150025Transceiver · failedDURING CRUISE, THE WEATHER RADAR SCREEN WENT BLANK. THE ACFT RETURNED TO DEPARTURE, LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION WAS PERFORMED NOTING THAT THE RADAR TRANSCEIVER TO BE AT FAULT. R & R THE RADAR TRANSCEIVER AND PERFORMED OPS CHECKS WITHOUT DESDR FOTR2021700540Skin · corrodedCORROSION ON RT HORIZ STAB UPPER T/E SKIN AT NR 3 ELEVATOR HINGE CUTOUT. REMOVED CORROSION ON RT HORIZ STAB T/E BEAM WITH 100 PERCENT MATERIAL LOSS, FOUND TO BE OUT OF LIMITS IAW SRM 51-10-1 AND 55-10-1. FITTED NEW BEAM PN 65-24571-2, SN BN574 AND LOCATED HOLSDR FOTR2021700137Hinge · crackedUPPER HINGE AFT MOST SEGMENT HAS AFT LOBE CRACKED. REMOVED AFT HINGE SEGMENT IAW SRM 51-30-2 AND 200F MM CH 52, FIG 5210B. FABRICATED NEW HINGE SEGMENT FROM MS20001-16-7200 PO 2021728 DIM 18" LONG. INSTALLED NEW HINGE SEGMENT IAW SRM 51-30-2 AND 51-10-2 AND SDR FOTR2021700257Angle · crackedRT WHEELWELL VERTICAL ANGLE IS CRACKED AT BS 870, RBL 8 BELOW LOAD CONTROL VALVE. REMOVED SUPPORT STRUCTURE AND VERTICAL ANGLE AT BS 870, RBL 8 FOR REPAIR IAW SRM 51-30-2. REPAIRED BS 870 WEB IAW SRM 53-10-9, FIG 5. FABRICATED 4 EA REPAIR FILLERS FROM 202SDR FOTR2021700544Skin · corrodedCORROSION ON LT HORIZ STAB UPPER SKIN AT NR 4 ELEVATOR HINGE CUTOUT. REMOVED CORROSION ON LT HOR STAB T/E SKIN BEAM AT NR 4 HINGE CUTOUT. MEASURED .040" MATERIAL LOSS FOUND TO BE OUT OF LIMITS IAW SRM 51-10-1, 51-10-6 AND 55-10-1. REMOVED LT HORIZ STAB T/E SDR FOTR2021700623Stringer · damagedSTA 540 AT STR 18R HAS HOLE DRILLED THRU RADIUS OF STRINGER. CUT OUT DAMAGED STRINGER DIM 19.5" LONG FROM STR 18R. FABRICATED NEW STRINGER SECTION FROM BAC1498-141 FROM 7075T6, PO 20041102, DIM 19.5", FABRICATED NEW TOP HAT FROM BAC1498-131, PO 90010803, DIMSDR FOTR2021700212Attach Bracket · crackedLT WING NR 2 SLAT ACTUATOR, INBD ATTACH BRACKET IS CRACKED. SLAT STA 291.0 REMOVED SLAT ACTUATOR SUPPORT STRUCTURE IAW SRM 51-30-2. FABRICATED NEW STIFFENER FROM BAC1503-100145 PO NR 20217147 DIM 9" X 4.5" AND SHIM FROM 7075T6 .032" PO NR 9006027 DIM 5" X SDR FOTR2021700805Structure · damagedNR 3 PYLON DAMAGED. REMOVED TITANIUM DOUBLER FROM NR 3 PYLON IAW SRM 51-30-2 AND EA 2708-5401 REV 1, LOCATED AND DRILLED NEW TITANIUM DOUBLER PN 69-18227-2, PO 20217102 IAW SRM 51-30-5 AND 51-30-6. FABRICATED 2 EA, FREEZE PLUGS FROM 15-5PH .375 PO 20217121 DISDR FOTR20217842Fitting · corrodedFUSELAGE EXTERIOR BS 740 PRESSURE FITTING IS CORRODED BETWEEN STR 27L-28L. REMOVED FITTING FROM STA 740 IAW SRM 51-30-2, FORMED FITTING FROM 7075-0, 7.2" X 10.7" .190" PO 2905745 IAW SRM 51-20-1, FIG 7. HEATED TREATED FITTING TO 7075T6 IAW ENG REPORT 2-37153-SDR FOTR/2021700365Fairing · gougedRT WING, OTBD FLAP, MID FLAP OTBD FAIRING HAS 2 EA GOUGES AND 1 EA LOOSE FASTENER. CUTOUT DAMAGED AREA DIM 1.5" X .6" IAW SRM 57-20-4, FIG 1. FABRICATED 2 EA REPAIR DOUBLERS FROM 2024-T3 .050" PO 90010715 DIM 5.6250" X 2.7500" AND 4.7" X 2". FABBED REPAIR SDR FOTR2021700828Frame · damaged(FOTR) MAIN CABIN FRAME AT BS 720A BETWEEN STR 16L-17L HAS DOUBLE DRILLED HOLE. CUTOUT DAMAGED AREA, DIMENSION 1" X .75" IAW SRM 51-10-1. FABRICATED DOUBLER FROM 7075-T6 PO 90010361, .063" DIMENSION 5.8750" X 3.8750" IAW SRM 51-40-3, FIG 1. INSTALLED REPAIR PSDR FOTR/20217/00827Frame · damaged(FOTR) MAIN CABIN FRAME AT BS 700 BETWEEN STR 16L-17L HAS DOUBLE DRILLED HOLES. CUTOUT DAMAGED AREA AT BS 700 DIMENSION 1" X .8" IAW SRM 51-10-1. FABRICATED DOUBLER FROM 7075-T6 .063 PO 90010361, DIMENSION 6.8750" X 3.5" IAW SRM 51-40-3, FIG 1. INSTALLED REPAISDR FOTR/20217/00826Frame · damaged(FOTR) CABIN FRAME AT BS 680 BETWEEN STR 16L-17L HAS DOUBLE DRILLED HOLES. CUTOUT DAMAGED AREA DIMENSION 1.4" X .6" ON BS 680 BETWEEN STRINGER 16L-17L IAW SRM 51-40-3 FIGURE 1. FABRICATED REPAIR ANGLE FROM 7075-T6 .050" PO 9009353 DIMENSION 7" X 3.6" IAW SRM SDR FOTR2021700821Frame · dented(FOTR) CABIN FRAME AT BS 560 BETWEEN STR 15R-16R DENTED. CUTOUT DAMAGED AREA ON BS 560 BETWEEN STR 15R-16R, DIMENSION 1.1" X 1.1" IAW SRM 51-40-3, FIG 1. FABRICATED REPAIR ANGLE FROM 7075-T6 .071' PO 9009519, DIMENSION 6.5" X 3.5" AND REPAIR FILLER FROM 7075-SDR FOTR2021700725Seat Track · corroded(FOTR) MAIN CABIN CARGO DECK, AT BS 560-580 LBL 45 INBD SIDE OF SEAT TRACK FLANGE HAS CORROSION. REMOVED CORROSION ON CABIN SEAT TRACK LBL 45, BS 560-580 IAW SRM 51-10-1, FOUND OUT OF LIMITS. REMOVED SEAT TRACK FROM BS 480-689 IAW SRM 51-30-2. FABRICATED SEASDR FOTR2021700682Seat Track · corroded(FOTR) LT FUSELAGE CABIN INTERIOR, HAS SURFACE CORROSION ON SEAT TRACK FLANGE BETWEEN BS 720A-720D, LBL 24. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1, FABRICATED NEW SEAT TRACK FROM BAC1520-792 7178-T6511 PO 90010776 DIMENSION 17'1.7500"SDR FOTR202170064Frame · dented(FOTR) LT FUSELAGE CABIN INTERIOR HAS FRAME DENTED AT BS 720, STR 16L. CUTOUT DAMAGED AREA ON FRAME DIMENSION 9" X .9" AT BS 720, STR 16L IAW SRM 51-10-1. FABRICATED FRAME REPAIR FROM 7075-T6 .063" PO 90010361, DIMENSION 5.5" X 17.3" IAW SRM 51-40-3, FIG 1. TSDR FOTR2021700661Frame · cracked(FOTR) REMOVED DAMAGED AREA FROM FRAME AT STR 17L DIMENSION 2.2500" X 1.5" IAW SRM 51-10-1, AND 51-30-2. FABRICATED REPAIR IAW SRM 51-40-3 FROM 7075-0 DIMENSION 9.1" X 4.1" PO 20198132. HEAT TREATED TO 7075T6 IAW FASI REPORT 2-37153-801A. FABRICATED CLIP FROSDR FOTR2021700658Stringer · gouged(FOTR) FUSELAGE CABIN INTERIOR HAS GOUGE AT FRAME BS 360 STR 6L. CUTOUT DAMAGED AREA AT STR 6L BS 360, DIMENSION 9.8750" FABRICATED STR FILLER FROM BAC 1498-143-7075T6 DIMENSION 9.8750". FABRICATED STRAP PLATES NR1 (1 EA) FROM 2024T3 .250" DIMENSION .8" X 1SDR FOTR2021700656Intercostal · cracked(FOTR)FUSELAGE CABIN INTERIOR, INTERCOSTAL IS CRACKED AT STR 16L BETWEEN BS 348-360. REMOVED FASTENERS FOR ACCESS IAW SRM 51-30-2. FABRICATED NEW DOUBLER REPAIR FROM 2024-T3 .063 PO 90010689, DIMENSION 5" X 3" IAW SRM 51-40-2. TREATED AND PRIMED IAW SRM 51-10SDR FOTR2021700653Shear Tie · cracked(FOTR) FUSELAGE CABIN INTERIOR, HAS CRACK INDICATION ON SHEARTIE, STR 8R BS 1130. REMOVED FASTENERS AT FUSELAGE FRAME IN MAIN CABIN BS 1130 STR 8R IAW SRM 51-30-2. C/W HFEC INSP IAW NDTM 51-00-00, FIG 23, PART 6. NO CRACKS NOTED. CUT SHEARTIE DIMENSION 6.2' X SDR FOTR2021700651Web · cracked(FOTR) CABIN INNER WEB DENTED AT BS 640, STR 6L. (AFT MAIN CARGO DOOR). C/W HFEC ON WEB IAW NDTM 51-00-00 FIGURE 23, PART 6. CRACK FOUND. REMOVED TRIM PANEL FROM BS 520-600, REMOVED AFT UPPER INNER SKIN FROM BS 600-560. FABRICATED NEW INNER SKIN FROM 2024-T3 .SDR FOTR2021700631Skin · dented(FOTR) AFT LOWER FUSELAGE EXTERIOR SKIN LT SIDE AT STATION 1148-1160 AND BETWEEN STR 25L-26L, SKIN IS DENTED. CUT DAMAGED AREA OUT OF UPPER LAP SKIN DIMENSION 4.5" X 5.5". FABRICATED REPAIR FILLER FROM 2024-T3 .063 PO 90010580 DIMENSION 12" X 14". FABRICATED SDR FOTR2021700626Stringer · corroded(FOTR) STR 27L BETWEEN BS 720F-740 IS CORRODED. CUT DAMAGED STR DIMENSION 12" LONG IAW SRM 53-10-3, FIG 1. FABRICATED REPAIR STR FROM BAC1498-147 7075T62 PO 2014059 DIMENSION 11.4375" LONG AND FABRICATED REPAIR STR SPLICE FROM BAC1498-131 7075-T6 PO90010803 DISDR FOTR/20217/00507Intercostal · dented(FOTR) C1 DOOR CUTOUT INTERCOSTAL IS DENTED AT UPPER FLANGE BS 627 BETWEEN STR 24R-25R. REMOVED DAMAGED INTERCOSTAL IAW SRM 51-30-2. LOCATED AND DRILLED NEW INTERCOSTAL PN 65-56101-36, PO 2021752. AND INSTALLED AT BS 627 BETWEEN STR 24R-25R IAW SRM 51-30-2,5SDR FOTR/20217/00381Frame · dented(FOTR) CABIN FRAME DENTED AT BS 400 BETWEEN STRINGER 5R-6R. REMOVED DAMAGED AREA OF BS 400 FRAME AT STR 5R-6R DIMENSION 2.25" X 4" IAW SRM 53-10-4 FIG 1, FABRICATED REPAIR FILLER AND 2 EACH SPLICES FROM 7075-0, .050, PO 90010501 AND HEAT TREATED TO T-6 IAW SSDR FOTR/20217/00378Frame · dented(FOTR) CABIN FRAME AT BS 380 DENTED BETWEEN STR 5R-6R, REMOVED DAMAGE AREA OF BS 380 FRAME AT STR 5R-6R, DIMENSION 15" X 4" IAW SRM 53-10-4, FIG 1. FABBRICATED REPAIR FRAME AND 2 EACH SPLICES FROM 7075-0 .050 PO 90010501 AND HEAT TREATED TO T-6 IAW SRM 53-10-0SDR ABXR201006050003Attach Angle · corrodedDURING THE ACCOMPLISHMENT OF A ROUTINE CPCP INSP CARD, A FAIRING ATTACH ANGLE WAS FOUND CORRODED BEYOND LIMITS. THE CORROSION DAMAGE WAS R & R WITH AN ANGLE FABRICATED FROM 0.050" 7075 T6 IAW THE SRM. THE ITEM WAS RETURNED TO SERVICE.SDR C8GA201000004Duct · separatedFLT 2739 FROM ATL TO TOL. DURING CLIMB OPERATION AN AIRFRAME VIBRATION WAS NOTED AND ISOLATED TO THE NR 2 ENGINE. AIRCRAFT RETURNED TO ATL WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION WAS PERFORMED. IT WAS NOTED THAT THE 8TH STAGE DUCT SEPARATESDR C8GA20090182Indicator · erraticDURING TAKEOFF ROLL THE CAPTAINS AIRSPEED INDICATOR BEGAN TO CYCLE FROM 0-300 KNOTS. THE TAKEOFF WAS ABORTED WHERE THE CREW RETURNED TO BLOCKS WITHOUT INCIDENT. POST FLIGHT INSP WAS PERFORMED AND THE CAPTAINS AIRSPEED INDICATOR WAS REMOVED AND REPLACED. OPS CSDR C8GA20090004Linkage · damagedFLT 1716 FROM TOL TO STL. DURING CLIMB OPERATION WHEN RETRACTING THE FLAP FROM 5 DEGREES TO 2 DEGREES THE NR 4 L/E FLAP AMBER LIGHT REMAINED ILLUMINATED. THE AIRCRAFT RETURNED TO TOL WHERE IT LANDED WITH OUT INCIDENT. POST FLIGHT INSPECTION WAS PERFORMED. SDR C8GA20090003Position Switch · inoperativeFLT 2715 FROM IAH TO TOL. DURING CLIMB OPERATION WHEN RETRACTING THE FLAP FROM 5 DEGREES TO 2 DEGREES THE NR 4 L/E FLAP AMBER LIGHT REMAINED ILLUMINATED. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITH OUT INCIDENT. POST FLIGHT INSPECTION WAS PERFORMED. SDR C8GA20080065Fire Loop · shortedFLT 716. ON DECENT THE APU FIRE LIGHT ILLUMINATED AND THE MASTER FIRE BELL SOUNDED. THE APPROPRIATE CHECKLIST ACCOMPLISHED. THE APU FIRE BOTTLE WAS DISCHARGED. EMERGENCY WAS DECLARED. THE AIRCRAFT LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION REVEALED THAT TSDR C8GA20080031Slat · malfunctionedFLT 715 FROM MEM TO TOL. DURING CLIMB OPERATION ON FLAP RETRACTION THE NR 7 LEADING EDGE DEVICE WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO MEM WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION OF THE NR 7 LEADING EDGE POSITION SWITCH WAS PERFORMED ASDR G8G2008F00001Fitting · faultyDURING CLIMB, THE NR 2 ENGINE LOW OIL PSI LIGHT ILLUMINATED AND OIL QUANTITY WENT TO EMPTY. THE NR 2 ENGINE WAS SHUT DOWN, AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION FOUND OIL FILTER BYPASS SWITCH GEARBOX FITTINGSDR C8GA200800Fitting · damagedFLT 720 FROM TOL TO MCO. DURING CLIMB OPERATION OUT OF TOL THE NR 2 ENG LOW OIL PSI LIGHT ILLUMINATED AND OIL QUANTITY WENT TO EMPTY. THE NR 2 ENGINE WAS SHUT DOWN, AN EMERGENCY WAS DECLARED AND THE ACFT LANDED IN TOL WITHOUT INCIDENT. POST FLIGHT INSPECTIOSDR C8G2008F00003Fitting · looseDURING CLIMB OPERATION, THE NR 2 ENGINE LOW OIL PSI LIGHT ILLUMINATED AND OIL QUANTITY WENT TO EMPTY. THE NR 2 ENG WAS SHUTDOWN, AN EMERGENCY WAS DECLARED AND THE AC LANDED WITHOUT INCIDENT. POST FLIGHT INSP REVEALED THAT THE NR 2 ENGINE OIL FILTER BYPASS SWSDR C8GA20080013Overheat Loop · faultedCLT TO BNA - DURING CLIMB OPERATION, THE NR 3 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED. THE AIRCRAFT DIVERTED TO TOL WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION REVEALED THAT THE NR 3 STRUT OVERHEAT DETECTOR LOOP AT FAULT. REMOVED AND REPLACED NSDR C8GA20070004Gearbox · leakingFLT 715 FROM HRL TO MEM. DURING CRUISE OPERATION NR 2 LOW OIL PSI LIGHT ILLUMINATED FOLLOWED BY A DECREASE IN OIL PSI AND OIL QUANTITY. PERFORMED APPROPRIATE CHECKLIST AND SHUT DOWN NR 2 ENGINE. AIRCRAFT DIVERTED TO IAH WHERE IT LANDED WITHOUT INCIDENT. POSSDR C8GA20060015Door · jammedON CLIMB, AIRCRAFT WOULD NOT PRESSURIZE NORMALLY. CREW NOTED SQUEAL AT L1 DOOR. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. FOUND L1 DOOR JAMMED. OPENED AND INSPECTED L1 DOOR. CYCLED DOOR SEVERAL TIMES. OPS CHECK GOOD. AIRCRAFT PRESSURIZES NORMALLY. SDR C8GA20060012Door Seal · out of adjustFLT 1712 FROM TOL TO DEN. DURING CLIMB PASSING THROUGH APPROXIMATELY 4000 FT CREW HEARD A LOUD SQUEAL ACCOMPANIED BY FLUCTUATING PRESSURIZATION. AIRCRAFT RETURNED TO TOL WERE IT LANDED WITHOUT INCIDENT. FOUND L1 DOOR UPPER HINGE COVER TO BE AT FAULT, REPOSISDR C8GA20060010Window · failedFLT 705 FROM YYC TO MSP. ON CLIMB, AT APPROXIMATELY FL30.0, AIRCRAFT EXPERIENCED SEVERE TURBULENCE AND HAIL DAMAGE. CREW DECLARED AN EMERGENCY AND RETURNED TO YYC. AIRCRAFT LANDED WITHOUT INCIDENT. FOUND NOSE RADOME WITH APPROXIMATELY 24 INCH DIAMETER HOLESDR C8GA20060008Warning Light · false activationFLT 711 FROM DEN TO TOL. DURING CLIMB THE LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED WHICH WAS EXTINGUISHED ONLY BY REDUCING THE NR 2 ENGINE THROTTLE TO IDLE. AIRCRAFT RETURNED TO DEN AND LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION WAS PERFORMED, TROUBLESDR C8GA20060007Oil Cooler · inoperativeFLT 1711 FROM LAX TO TOL. DURING CLIMB PASSING THROUGH 10,000FT THE NR 3 ENGINE CSD TRIPPED INDICATING 140 DEGREE'S CELSIUS IN TEMP. THE NR 2 ENGINE CSD WENT TO 140 DEGREE'S AND NR 1 CSD WAS OPERATING HOT AT 125 DEGREE'S. AIRCRAFT DIVERTED TO SAN AND LANDESDR C8GA20060003Connector · contaminatedFLT 1059 FROM TOL TO MCI, DURING CLIMBOUT NR 3 ENGINE EPR GAUGE AND F/O'S AIRSPEED INDICATOR CEASED OPERATION FOLLOWED BY FLAGS ON F/O'S SIDE, BOTH FLIGHT RECORDER AND NR 2 COMPUTER C/B'S TRIPPED AND WOULD NOT RESET. AIRCRAFT RETURNED TO TOL WITHOUT INCIDENT.SDR C8GA20050024Door · openDURING CLIMBOUT OPERATION, AIRCRAFT WOULD NOT PRESSURIZE ABOVE 1.5 PSID. AIRCRAFT RETURNED AND LANDED WITHOUT INCIDENT. ON POST FLIGHT FOUND L1 ENTRY DOOR NOT FULLY CLOSED, OPEN, CYCLED AND RESET DOOR, CONFIRMED FULLY CLOSED AND LOCKED. NO DEFECTS NOTED. AIRCSDR C8GA20040019Engine · damagedFLT 727 FROM DFW TO TOL. ON TAKEOFF, THE NR 3 ENGINE HAD STRONG VIBRATION. IN-FLIGHT SHUTDOWN OF THE NR 3 ENGINE AS A PRECAUTIONARY ADVISED ATC DECLARED EMERGENCY AND AIR TURN BACK TO DFW. AIRCRAFT WAS INSPECTED AND FOUND FAILURE OF TURBINE SECTION PER EVIDESDR C8GA20040007Toggle · bentAFTER DEPARTURE, DURING FLAP RETRACTION THE OUTBOARD FLAP INDICATED ASYMMETRY BETWEEN THE FLAP FIVE DEGREE AND TWO DEGREE POSITION. ACCOMPLISHED THE APPROPRIATE CHECKLIST AND RETURNED TO KBOS. NO EMERGENCY ACTION WAS TAKEN AND AIRCRAFT LANDED WITHOUT INCIDENSDR C8GA20030005Downlock · defectiveFLIGHT 705 FROM KMSP TO KTOL. ON APPROACH INTO TOLEDO, THE LEFT HAND MAIN GEAR INDICATED UNSAFE RED LIGHT ON. ACCOMPLISHED ABNORMAL CCIA AIRCRAFT OPERATIONS MANUAL CHECKLIST A-06-4. AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT WAS INSPECTED AND THE LEFT HAND GEA
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