N281KH, cancelled Jan 10, 2008
Service difficulty reports · 84
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 = 'N281KH' AND deregistration_id = 'N281KH-2008-01-10' 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 = 'N281KH' AND deregistration_id = 'N281KH-2008-01-10' 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 GAIA05037OPDownlock Switch · inoperativeDURING APPROACH, ON SHORT FINAL, NOSE GEAR LIGHT CHANGED FROM GREEN TO RED, GOT HORN. CYCLED GEAR TWICE TO NO AVAIL. VISUAL INSPECTION THROUGH PORT INDICATED DOWN AND LOCKED. LANDING AND TAXI IN UNEVENTFUL. CLEANED AND RESEATED DOWNLOCK SWITCH AND (DOWNLOCKSDR GAIA05035OPConnector · dirtyDURING APPROACH, INITIAL GEAR EXTENSIO, NOSE GEAR INDICATOR (NOT SAFE), AFTER RECYCLE AND A SHORT DELAY INDICATION NORMAL. LANDING WAS MADE WITHOUT INCIDENT. CLEAN AND RESEATED NOSE GEAR CONNECTOR PLUGS. INSPECTED NOSE GEAR AREA. NO DEFECT NOTED. CHECKED SDR GAIA05029OPLight · inoperativeDURING A-CHECK FOUND L1 EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED EXIT LIGHT AT L1 DOOR. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (K)SDR GAIA05022OPBulb · burned outL1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. RELAMPED L1 DOOR EMERGENCY EXIT LIGHT. LIGHT OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR GAIA04175OPDownlock Switch · failedDURING APPROACH, ON SHORT FINAL, NOSE GEAR LIGHT CHANGED FROM GREEN TO RED, GOT HORN. CYCLED GEAR TWICE TO NO AVAIL. VISUAL INSPECTION THROUGH PORT INDICATED DOWN AND LOCKED. DECLARED EMERGENCY. LANDING AND TAXI IN UNEVENTFUL. TROUBLESHOOT NOSE GEAR INDICSDR GAIA04080OPActuator · inoperativeFLT 716 - FWA-PHX - ON DEPARTURE AFTER RETRACTING FLAPS NOTED NR 2 LED DID NOT RETRACT, PROCEEDED TO CHECK LIST. RETURNED TO FWA WHERE A LANDING WAS MADE WITHOUT INCIDENT. FOUND NR 2 L/E SLAT ACTUATOR INOPERATIVE. REMOVED AND REPLACED ACTUATOR. OPS CHECK GSDR GAIA04078OPWire · brokenFLT 2715 - ELP-DFW-FWA - DURING CLIMB, THE UPPER RUDDER INDICATOR WAS SWINGING BETWEEN MINOR INDICIES. AT 10,000 AGL THE LOWER RUDDER SWUNG HARD LEFT AND THEN ANOTHER LEFT NOT AS HARD. CREW FOLLOWED FLIGHT CONTROL EMERGENCY PROCEDURE AND RETURNED TO ELP. ANSDR GAIA04071Coupler · malfunctionedDEPARTURE, FLIGHT, WITH AIRSPEED CHANGES, AIRCRAFT YAW CHANGES NOTICEABLY. AFTER RUDDER IS RETRIMMED AIRCRAFT DUTCH ROLLS A FEW TIMES IN A JERKING MANNER. WITH INCREASING SPEEDS MORE RT TRIM IS REQUIRED. CREW RETURNED TO DEPARTURE AIRPORT, WHERE A LANDING WSDR GAIA04002OPValve · malfunctionedFLT 2872 - LAX-FWA - DURING CRUISE, THE FILGHT CREW NOTICED THAT THE NR 2 FUEL CROSS FEED VALVE APPEARED TO BE CLOSED. THE CREW DECIDED TO MAKE A PRECAUTIONARY LANDING IN PHX. OPENED THE NR 2 TANK TO ENGINE VALVE AND SAFETIED OPEN PER THE BOEING DISPATCH DEVSDR GAIA03081OPLight · malfunctionedDURING CRUISE, THE CREW NOTICED THE COCKPIT EMERGENCY EXIT LIGHT CAME ON WITH THE SWITCH IN THE ARMED POSITION. REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT. OPS CHECK NORMAL. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR GAIA03033SPStringer · crackedDURING C-CHECK, FOUND MAIN CABIN FRAME BS 360 HAS WEB CRACKED AT STRINGER 16L FASI N/R 35753. FABRICATED REPAIR DOUBLER FROM MATERIAL 7075-T6 .063 PO NR 9911488 DIM 3.5 INCH BY 4 INCH. INSTALLED REPAIR IAW B727 SRM 51-40-2. (M)SDR GAIA03035SPStiffener · crackedDURING C-CHECK, FOUND LEFT WING FRONT SPAR STATION 475 VERTICAL STIFFENER CRACKED TWO FASI N/R 35923. FABRICATED STIFFENERS FROM MATERIAL 7075-T6 STRUT P/N 1505-29063, PO NR 3146124 DIM 10.125 INCH BY 2.25 INCH TWO EACH, INSTALLED IAW B727 SRM 51-30-2. (M)SDR GAIA03032SPFrame · dentedDURING C-CHECK, FOUND MAIN CABIN FRAME BS 360 HAS DENTS INTO THE RADIUS BETWEEN STRINGER 15L AND 17L FASI N/R 35752. CUT OUT DAMAGES AREAS, FABRICATED REPAIR DOUBLER, MATERIAL USED 7075-T6 .063 PO NR 9912571 DIM 18.5 INCH BY 6.5 INCH. TWO ATTACH ANGLES P/N BSDR GAIA03039SPSkin · debondedDURING C-CHECK, FOUND LEFT WING OUTBOARD AFT FLAP T/E DISBONDED AREAS BETWEEN WBW .348 AND WBL 442 FASI N/R 35939. CUT OUT DELAMINATED AREAS, FABRICATED FILLER FROM MATERIAL 2024-T3 .016, PO NR 209415 DIM 6.75 INCH BY 7 INCH. FABRICATED DOUBLER FROM MATERIALSDR GAIA03041SPSkin · dentedMAIN CABIN FRAME BS 580 DENTED BELOW STRINGER 8 RT FASI N/R 36052, FOUND DURING C-CHECK. CUT OUT DAMAGE 1 INCH BY 1.5 INCH, DOUBLER REPAIR 7075 T-6 IAW B-727 SRM 53-10-4 FIG 1. (M)SDR GAIA03040SPWeb · crackedDURING C-CHECK, FOUND LOWER FORWARD CARGO COMPARTMENT BS 620 FRAME WEB DOUBLER HAS PIECES BROKEN OFF FASI N/R 35707. REMOVED BROKEN PART, FABRICATED DOUBLER REPAIR FROM MATERIAL 7075-T6 .063 PO NR 991396 DIM 14 INCH BY 5.25 INCH. INSTALLED IAW B727 SRM 51-30-SDR GAIA03026SPFrame · dentedDURING C-CHECK, MAIN CABIN FRAME BS 720 HAS A DENT INTO THE RADIUS BELOW STRINGER 16R. REMOVED FASTENERS AND CUT OUT DAMAGED AREA OF FRAME, FABRICATED REPAIR DOUBLER IAW B727 SRM 53-10-4 FIG 1, MAT USED .050 7075-T6 P/O NR 9911488 DIM 10 INCH BY 5 INCH. INSTSDR GAIA03025SPStringer · crackedDURING C-CHECK, FOUND MAIN CABIN FORWARD STATION 720C, STRINGER 15L IS CRACKED AFT OF WING LIGHT. CUT OUT CRACK FROM STRINGER 15L, IAW SRM 53-10-3 FIG 5, FABRICATED REPAIR PARTS ONE CHANNEL .040 7075-T6 DIM 5.2 INCH BY 3.2 INCH, TWO FILLERS .100 7075-T6 5.2 BSDR GAIA03029SPFrame · dentedDURING C-CHECK, FOUND MAIN CABIN FRAME BS 520 HAS A DENT INTO THE RADIUS AT STRINGER 16R FASN/R 35745. CUT OUT DAMAGED AREA, FABRICATED FILLER FROM MATERIAL 7075-T6 .050 PO NR 991420, DIM 2.5 INCH BY 3 INCH, DOUBLER FROM MATERIAL 7075-T6 .063, PO NR 9912495 DSDR GAIA03028SPFrame · dentedDURING C-CHECK, FOUND MAIN CABIN FRAME BS 540 HAS DENT INTO THE RADIUS AT STRINGER 16 RT, FASI N/N 35744. CUT OUT DAMAGED AREA, FABRICATED SECTION OF FRAME MATERIAL USED 7075-T6 .063 P/O NR 991245 DIM 12 INCHES BY 3.5 INCHES, DOUBLER 7075-T6 .071 P/O NR 99120SDR GAIA03027SPFrame · dentedDURING C-CHECK, FOUND MAIN CABIN FRAME BS 600 HAS A DENT INTO THE RADIUS AT STRINGER 16R. CUT OUT DAMAGED AREA OF FRAME. FABRICATED NEW SECTION OF FRAME, MAT USED 7075-T6 .050 P/O NR 991420 DIM 12 INCH BY 5 INCH, AND FILLER MAT USED 7075-T6 .050 P/O NR 9914SDR GAIA03038SPSplice · crackedDURING C-CHECK, FOUND MAIN CARGO DOOR DECK BS 640, FLOORBEAM SPLICE PLATE CRACKED FROM SLOT RADIUS FASI N/R 35932. REMOVED AND REPLACED FLOORBEAM SPLICE PLATE P/N AE727-1-42-11, PO NR 319397 IAW STC AE179850 DTD 4-7-93. (M)SDR GAIA03037SPSplice · crackedDURING C-CHECK, FOUND MAIN CARGO DECK BS 600, FLOORBEAM SPLICE PLATE CRACKED AT SLOT RADIUS FASI N/R 35931. REMOVED AND REPLACED FLOORBEAM SPLICE PLATE P/N AE727-1-42-11, PO NR 319397 IAW STC AE 179850 DTD 4-7-93. (M)SDR GAIA03036SPFloorbeam · crackedDURING C-CHECK, FOUND MAIN CARGO DECK BS 580, FLOORBEAM SPLICE PLATE CRACKED AT SLOT RADIUS, FASI N/R 35930. REMOVED AND REPLACED SPLICE PLATE P/N AE 727-1-42-11, PO NR 319397 IAW STC AE 179850-DTD 4-7-93. (M)SDR GAIA03034SPFrame · dentedDURING C-CHECK, FOUND MAIN CABIN FRAME BS 560 HAVE DENTS INTO THE RADIUS AT STRINGER 16R AND STRINGER 8R FASI N/R 35743. CUT OUT DAMAGED AREAS, FABRICATED DOUBLERS FROM MAT 7075-T6 .063 PO NR 9912495, DIM 7 INCH BY 4.5 INCH AND 10 INCH BY 3 INCH. INSTALLED DSDR GAIA03031SPFrame · crackedDURING C-CHECK, FOUND MAIN CABIN FRAME BS 360 HAS A DENT AND CRACK BETWEEN STRINGERS 7R AND 8R FASI N/R 35751. CUT OUT DAMAGED AREA, FABRICATED DOUBLER REPAIR FROM 7075-T6 .050, PO NR 9911488 DIM 11 INCH BY 5.5 INCH. INSTALLED REPAIR IAW B727 SRM 51-30-2 ANDSDR GAIA03030SPFrame · damagedDURING C-CHECK, FOUND MAIN CABIN FRAME BS 460 HAS A TOOLING HOLE INTO THE RADIUS AT STRINGER 17R FASI N/R 35747. CUT OUT DAMAGE AREA, FABRICATED DOUBLER FROM 7075-T6 .063 PO NR 9912495 DIM 3.5 INCH BY 7.75 INCH, INSTALLED REPAIR IAW B727 SRM 51-30-2. (M)SDR GAIA03042SPSeat Track · corrodedDURING C-CHECK, FOUND MAIN CABIN SEAT TRACK CORRODED LBL 45 BS 720D FASI N/R 36068. REPLACED DAMAGED PARTS 90 INCHES LONG P/N BAC1520-792 AND BAS 1593-100122 IAW B-727 SRM 53-10-5 FIG 1. (M)SDR GAIA03024SPStringer · crackedDURING C-CHECK, FOUND AT MAIN CABIN FORWARD STATION 720B, STRINGER 15L IS CRACKED. CUT OUT CRACK FROM STRINGER 15L, IAW SRM 53-10-3 FIG 5, FABRICATED REPAIR PARTS ONE CHANNEL .040 7075-T6 DIM 4.7 INCH BY 3.2 INCH, TWO FILLRES .100 7075-T6 4.7 BY 8 IAW SRM 53-SDR GAIA03047SPSkin · chafedDURING C-CHECK, FOUND UPPER AND LOWER RUDDERS LEADING EDGES TEFLON ANTI-CHAFE PAINT WORN OUT, BOTH RUDDERS HAVE AREAS OF CHAFING. FOUND 6 AREAS ON LOWER RUDDER OUT OF LIMITS, FABRICATED 6 DOUBELRS, TWO 21.5 AND 14.25, TWO 15.25 BY 23.5, TWO 13.5 BY 15.5 ALL FSDR GAIA03046SPKeelbeam · crackedDURING C-CHECK, FOUND RIGHT WHEEL WELL BS 870 AND KEEL BEAM, VERTICAL STIFFENER CRACKED FASI N/R 35583. REPLACED VERTICLE ANGLE, P/N 65-18636-378 IAW B727 SRM 51-30-2. (M)SDR GAIA03045SPFrame · dentedDURING C-CHECK, FOUND MAIN CABIN FRAME BS 580 HAS A DENT AT STRINGER 16 RT, FASI N/R 36051. CUT OUT DAMAGE 1 INCH BY 1.5 INCH, REPAIR DOUBLER 7075 T-6 INSTALLED IAW B-727 SRM 51-40-3 FIG 1. (M)SDR GAIA03044SPSkin · chafedDURING C-CHECK, FOUND LOWER RUDDER LOWER L/E CLOSE OUT WEB CHAFED THROUGH FASI N/R 36010. REPLACED WEB P/N 65-16830-4 IAW B-727 SRM 51-30-2. (M)SDR GAIA03048SPSkin · debondedDURING C-CHECK, FOUND RT WING LOWER TRAILING EDGE PANEL 8605 HAS DISBONDED SPOT OUTER SKIN. CUT OUT 3 INCHES BY 48 INCHES, FABRICATED FILLER 3 INCHES BY 48 INCHES, LOWER DOUBLER 3 INCHES BY 48 INCHES 2024 T-3 .016 UPPER DOUBLER 4.5 BY 50 INCHES 2024 T-3 .020,SDR GAIA03023SPStringer · crackedDURING C-CHECK, FOUND FASI NR 35734, AT MAIN CABIN FRAME 720B, STRINGER 15R IS CRACKED FORWARD OF THE WING LIGHT. CUT OUT CRACK FROM STRINGER 15R IAW SRM 53-10-3 FIG 5, FABRICATED REPAIR PARTS ONE CHANNEL .040 7075-T6 DIM 4.7 INCH BY 3.2 INCH, TWO FILLERS .10SDR GAIA03022SPSkin · corrodedDURING C-CHECK, FOUND FUSELAGE RIGHT SIDE STATION 675 STRINGER R19 HAS PILLOWING AT FASTENERS. CUT OUT DAMAGED SKIN 3 INCHES BY 2.75 INCHES, ACCOMPLISHED DOUBLER REPAIR IAW B727 SRM 53-30-3 FIG 14. DOUBLER 2024 T-3, .071, FILLER 2024 T-3 .063. (M)SDR GAIA03043SPBeam · crackedDURING C-CHECK, FOUND VERTICAL BEAM BULKHEAD 1183 RBL 36.5 WL 249 INBOARD CHORD HAS A CRACK. REMOVED FASTENERS FOR ACCESS IAW 727 SRM 51-30-2. STOP DRILLED CRACK IAW B727 SRM 51-10-1. ACCOMPLISHED 727 HFEC INSPECTION. INSTALLED VERTICAL BEAM REPAIR IAW S/BSDR GAIA03001OPValve · malfunctionedFLT 884 - ONT-FWA - DURING CLIMB CREW DISCOVERED A PROBLEM WITH THE FUEL PANEL. THE NR 2 CROSSFEED VALVE WAS NOT OPEN. CREW DECLARED AN EMERGENCY AND DIVERTED TO PHX. DEFERRED NR 2 CROSSFEED VALVE PER MEL 28-7. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR GAIA01318STFrame · crackedDURING TROUBLESHOOTING FOR A PRESSURIZATION PROBLEM A 2 INCH CRACK WAS FOUND ON A FRAME ON THE FORWARD SIDE OF THE NR 3 AFT CARGO DOOR ASSEMBLY. REMOVED AND REPLACED THE NR 3 LOWER AFT CARGO DOOR ASSEMBLY. OPERATIONALLY CHECKS GOOD. THE AIRCRAFT WAS RETURNESDR GAIA01294Light · inoperativeDURING ROUTINE MAINTENANCE AT PHX, IT WAS DISCOVERED THAT THE L1 DOOR POSITION EMERGENCY EXIT LIGHT WAS INOPERATIVE. REMOVED AND REPLACED THE L1 DOOR POSITION EMERGENCY EXIT LIGHT ASSEMBLY. OPERATIONALLY CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (SDR GAIA01078OPTransmission · bindsFLT 281 - JAX - DURING APPROACH, THE INBOARD TRAILING EDGE FLAP INDICATOR WILL NOT MOVE PAST FOUR DEGREES IN FLIGHT. PERFORMED ABNORMAL PROCEDURE. DECLARED AN EMERGENCY WITH APPROACH CONTROL. THE AIRCRAFT LANDED WITHOUT ANY FURTHER DIFFICULTIES. REMOVED ANDSDR GAIA01068STSkin · crackedDURNG A LTC INSPECTION OF FLIGHTSTAR JAX, FOUND RIGHT WING L/E HAS A CRACK AT WS 464. ACCOMPLISHED RIGHT WING FIXED L/E SKIN REPAIR WS 464 IAW B727 SRM 57-30-4 FIG 4. MATERIAL FILLER 2024-T3 .040 PO NR 9812. DIM''S 2.330 INCH BY 3 INCH. DOUBLER 2024-T3 .05SDR GAIA01067STSpar · corrodedDURING A LTC INSPECTION AT FLIGHTSTAR JAX, FOUND LEFT WING STATION 431.5 CORROSION ON FRONT SPAR WEB AT LOWER CHORD. ACCOMPLISHED LEFT WING FRONT SPAR WEB REPAIR WS 431.5 IAW B727 SRM 57-10-6 FIG 1 MATERIAL 2024-T3 .250 PO NR 20093117. DIM''S 12 INCH BY 14 ISDR GAIA01066STStiffener · corrodedDURING A LTC INSPECTION AT FLIGHTSTAR JAX, FOUND LEFT WING FRONT SPAR HYDRAULIC LINE SUPPORT ANGLE (VERTICAL STIFFENER) AT FSS 386 IS CORRODED. ACCOMPLISHED VERTICAL STIFFENER REMOVAL AND REPLACEMENT FSS LEFT 386 IAW B727 SRM 51-30-2 AND 51-30-5. P/N 65-17209SDR GAIA01065STStiffener · corrodedDURING A LTC INSPECTION AT FLIGHTSTAR JAX, FOUND LEFT WING FRONT SPAR HYD LINE SUPPORT ANGLE (VERTICAL STIFFENER) AT FSS 396 IS CORRODED. ACCOMPLISHED VERTICAL STIFFENER REMOVAL AND REPLACEMENT FSS LEFT 396 YAW B727 SRM 51-30-2 AND 51-30-5 P/N 65-17210-27. TSDR GAIA01064STStiffener · corrodedDURING A LTC INSPECTION AT FLIGHTSTAR JAX, FOUND LEFT WING L/E WS 390 HAS CORROSION ON FORWARD SPAR STIFFENER. ACCOMPLISHED VERTICAL STIFFENER REMOVAL AND REPLACEMENT FSS LEFT 390 LEFT 390 IAW B727 SRM 57-10-2 FIG 3 AND 51-30-2. MATERIAL STIFFENER BAC 1517-1SDR GAIA01063STSkin · gougedDURING A TLC INSPECTION AT FLIGHTSTAR JAX, FOUND SEVERAL DENT''S AND GOUGES ON FUSELAGE SKIN BS 1050-1055 AT STRINGER 23-25R. ACCOMPLISHED FUSELAGE SKIN REPAIR BS 1050-1055 BETWEEN STRINGER 23R AND 25R IAW B727 SRM 53-30-3 FIG 3. MATERIALS FILLER 2024-T3 .06SDR GAIA01062STSkin · canningDURING LTC INSPECTION AT FLIGHTSTAR JAX, FOUND SKIN OIL CANNED AT BS 196R AREA IS MARKED. ACCOMPLISHED FUSELAGE SKIN REPAIR BS 196 R IAW B727 SRM 53-30-3 FIG 1 MATERIAL 2024-T3 .050 PO NR 991266. DIM''S 10.400 INCH BY 8.5 INCH. THE AIRCRAFT WAS RETURNED TO SDR GAIA01061STSkin · dentedDURING A LTC INSPECTION AT FLIGHTSTAR JAX, FOUND DENT IN FUSELAGE SKIN AT BS 1153 BETWEEN STRINGER 21-22 RIGHT. ACCOMPLISHED FUSELAGE SKIN REPAIR BS 1153 BETWEEN STRINGER 21R AND 22R IAW B727 SRM 53-30-3 FIG 1. MATERIALS 2024-T3 .100 PO NR 2006763. DIM''S 1SDR GAIA01060STSkin · dentedDURING A LTC INSPECTION AT FLIGHTSTAR JAX, FOUND OUTWARD FACING DENT AT BS 720A PLUS 10 INCHES ABOVE STRINGER 18 RT. ACCOMPLISHED FUSELAGE SKIN REPAIR BS 720A PLUS 10 INCHES ABOVE STRINGER 18RT IAW B727 SRM 53-30-3 FIG 1. MATERIAL 2024-T3 .063 PO NR 991420.
Back to N281KH, cancelled Jan 10, 2008