N295AS, cancelled Oct 29, 2014
Service difficulty reports · 139
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 = 'N295AS' AND deregistration_id = 'N295AS-2014-10-29' 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 = 'N295AS' AND deregistration_id = 'N295AS-2014-10-29' 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 CIHA200759026Support Angle · corrodedSTRINGER 26L TO FRAME SUPPORT ANGLE CORRODED BS 950F. REMOVED SUPPORT ANGLE, FABRICATED AND INSTALLED NEW SUPPORT ANGLE IAW B727 SRM 51-10-3 FIG 2 & 51-30-2 FIG 1.SDR C1HA200795011Support · corrodedSURFACE CORROSION ON MAIN CABIN FWD LAV AFT WALL SUPPORT BS 344 RBL 15 - RBL 65. REPLACED LAV SUPPORT BS 344 RBL 15 TO 65 IAW B727 SRM 53-10-2.SDR C1HA200795006Frame · crackedCOCKPIT FRAME AT STA 277 AND STR 16RT IS CRACKED APPROX 1 INCH LONG, VERIFED BY HFEC (BEHIND FE CONSOLE). REPAIRED COCKPIT FRAME AT STA 277, STR 16RT IAW B727 SRM 53-10-2 AND 51-40-2.SDR C1HA200795008Seat Track · corrodedCORROSION ON SEAT TRACK BS 420-480 RBL 55. REPLACED SEAT TRACK FROM BS 420 TO 480 RBL 55 IAW B727 SRM 53-10-2 FIG 7 AND 53-10-5 FIG 7.SDR CIHA200795010Seat Track · corrodedCORROSION ON SEAT TRACK BS 344 - 380 RBL 45. REMOVED AND REPLACED SEAT TRACK IAW B727 SRM 53-10-2 AND 53-10-5 FIG 7.SDR C1HA200795004Support Angle · crackedLEFT VENTRAL STAIRWELL LT TORQUE BOX SUPPORT ANGLE IS CRACKED AT STA 1253 BELOW BAZOOKA TUBES. FABRICATED AND INSTALLED REPAIR DOUBLER AT BS 1253 LEFT TORQUE BOX SUPPORT ANGLE MATERIAL USE 7075-T6 .050, DIM 8 X 3, IAW B727 SRM 51-40-3 FIG 1 & 53-10-2 FIG 6.SDR C1HA200795001Angle · crackedRIGHT WING L/E STA 130.7 INTERNAL ANGLE AT FRONT SPAR LWR CRACKED. FABRICATED AND INSTALLED REPAIR PART IAW B727 M/M 57-20-21 PG 801 AND SEALED AS REQUIRED IAW B727 M/M 51-30-11.SDR C1HA200795021Angle · corrodedANGLE CORRODED RIGHT CUSP ANGLE TO FRAME SPLICE ATTACHED AFT SIDE OF STA 740 RIB AT FLOOR LEVEL STA 740-743 RBL 61. CORROSION FOUND OUT OF LIMITS. REPLACED ANGLE IAW B727 SRM 53-10-2 AND 51-30-2.SDR C1HA200795020Stringer · crackedFOUND STRINGER 15R CRACKED AT BS 720B. REPAIRED STR 15R AT BS 720B IAW B727 SRM 53-10-3 FIG 5.SDR C1HA200795003Skin · crackedFOUND FUSE BS 1098 RBL 1 HAS 1/2" CRACK IN FASTENER HOLE. CUT OUT CRACKED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER IAW B727 SB 727-53A0204 REV 3 FIG 2 AND AD 94-05-04-06.2SDR C1HA200795014Bracket · corrodedFOUND CORROSION EMANATING FROM BENEATH ANGLE BRACKET O/B OF AFT LAV FITTINGS AT STA 1165 RBL 45. REPLACED BRACKET ANGLE IAW B727 SRM 51-40-3 AND 53-10-2 AND REPAIRED SHEAR WEB IAW B727 SRM 53-10-2 AND 51-40-2.SDR C1HA200795012Angle · corrodedFOUND CORROSION ON WEB ANGLE IN SEVERAL MARKED AREAS BETWEEN STA 1148-1165 RBL 60. REPLACED ANGLE BETWEEN STA 1148 TO 1165 RBL 60 IAW B727 SRM 53-10-2 AND 51-40-3.SDR C1HA200795016Seat Track · corrodedFOUND SEAT TRACK CORRODED IN SEVERAL MARKED AREAS STA 999-1110 LBL 25. REMOVED AND REPLACED SEAT TRACK ON STA 1010-1130 LBL 25 IAW B727 SRM 51-30-2 AND 53-10-5 FIG 7.SDR C1HA200795033Stringer Splice · corrodedFOUND FWD CARGO COMPARTMENT AT BS 540 STR 26R HAS HEAVY CORROSION AT SPLICE. REMOVED AND REPLACED FWD CARGO BS 540 STR 26R SPLICE ANGLE IAW B727 SRM 53-10-2 AND 53-40-3.SDR C1HA200795032Stringer · corrodedFOUND CORROSION IN E/E BAY AT BS 475 STR 27L. REPAIRED STR 27L AT BS 475 IAW B727 SRM 53-10-2 FIG 9 AND 53-10-3 FIG 1.SDR C1HA200795031Stringer Splice · corrodedFOUND CORROSION IN E/E BAY AT BS 475 STR 26L. REMOVED EXISTING MANUFACTURE SPLICE, FABRICATED AND INSTALLED NEW SPLICE IAW B727 SRM 53-10-3 FIG 1.SDR C1HA200795022Seat Track · corrodedFOUND CABIN SEAT TRACK AT BS 740-760 LBL 24 IS CORRODED BEYOND LIMITS. REPLACED MAIN CABIN SEAT TRACK AT BS 740-760 LBL 24 IAW B727 SRM 53-10-2 AND 53-10-5.SDR C1HA200795019Stringer · crackedFOUND STR 15L CRACKED AT BS 720C. REPAIR STR 15L AT BS 720C IAW B727 SRM 53-10-3 FIG 5.SDR C1HA200795024Floorbeam · corrodedBS 1130 FLOORBEAM AT LOWER FORWARD FLANGE HAS CORROSION (RBL-10). FOUND CORROSION OUT LIMITS, CUT OUT DAMAGE, FABRICATED AND INSTALLED FILLERS, ANGLE, RADIUS FILLER AND STRAP REPAIRS TREATED AND PRIMED IAW B727 SRM 51-10-2, 53-10-1, 53-10-8 AND 51-30-2 FIG 1.SDR C1HA200795027Stringer · corrodedFOUND CORROSION ON FRAME STA 420 BL 0 TO STR 28R. REMOVED DAMAGED SECTION OF STRINGER, FABRICATED AND INSTALLED NEW SECTION FROM BS 400-420 STR 28R IAW B727 SRM 53-10-3 FIG 1.SDR C1HA200795005Plenum · corrodedA/C RAM AIR PLENUM HAS SURFACE CORROSION ON NR 2 TANK LWR SKIN ABOVE LT PRIMARY HEAT EXCHANGER. BLENDED OUT CORROSION DAMAGE, MAT LOSS .050, ORIGINAL THK .225. FLUORESCENT DYE PENETRANT AREA, NO DEFECTS NOTED. TREATED AND PRIMED AREA IAW B727 SRM 51-10-2. SDR C1HA200795023Shear Web · corrodedAFT CABIN LT SHEAR WEB BS 1166 LBL 35 HAS HEAVY PITTED CORROSION. REPAIRED AFT CABIN LT SHEAR WEB AT BS 1166 LBL 35 IAW B727 SRM 53-10-2 AND 51-40-2.SDR C1HA200795009Seat Track · corrodedFOUND CORROSION ON SEAT TRACK BS 380 - 460 RBL 45. REPLACED SEAT TRACK AT BS 380 TO 460 RBL 45 IAW B727 SRM 53-10-2 AND 53-10-5 FIG 7.SDR C1HA200795002Skin · crackedEXT FUSE BS 303 AT L-1 DOOR LOWER HINGE HAS REPAIR DOUBLER CRACKED IN FWD CUTOUT. REMOVED EXISTING REPAIR DOUBLER, HFEC INSP AND FOUND SKIN AND INNER DOUBLER CRACKED, CRACK APPROX 2 1/4" LONG. CUTOUT DAMAGED AREA IAW B727 SRM 51-10-1. REPAIRED AREA IAW CA ESDR C1HA200795025Stringer · corrodedFOUND CORROSION AT STA 740. CUT OUT DAMAGED AREA FROM STR 27L AT STA 740, FAB`D STR REPAIR AND SPLICE. TREATED AND PRIMED. REMOVED AND REPLACED DAMAGED FITTING AT LT STA 740 AT STR 27L. INSTALLED ALL PARTS IAW B727 SRM 53-10-3 FIG 1 AND 51-30-2.SDR C1HA200795029Frame · corrodedFOUND CORROSION STA 351.2 FRAME AT 28R. REMOVED EXISTING TEE CHORD FRAME, FABRICATED AND INSTALLED NEW TEE CHORD IAW B727 SRM 53-10-2 FIG 1.SDR C1HA200795017Seat Track · corrodedFOUND MAIN CABIN STA 880 TO 950 LBL 24 SEAT TRACK HAS CORROSION ON TOP SURFACE. FABRICATED AND INSTALLED NEW SEAT TRACK P/N BAC1520-792 (91") IAW B727 SRM 53-10-5 FIG 1.SDR C1HA200795007Seat Track · corrodedFOUND CORROSION ON SEAT TRACK AT AFT CUTOUT AND MOUNT POINT STA 1130 LBL 25. REPLACED SEAT TRACK AT BS 1110-1130 LBL 25, P/N BAC1520-792 IAW B727 SRM 53-10-5 FIG 7.SDR C1HA200795028Stringer · corrodedFOUND CORROSION STR 28L AT STA 410. REPAIRED STRINGER AT BS 410 28L IAW B727 SRM 53-10-2 AND 53-10-3 FIG 1.SDR C1HA200795030Stringer · corrodedFOUND CORROSION STR 26R STA 470. FABRICATED AND INSTALLED REPAIR PARTS FOR STRINGER 26R BS 450 - 490 IAW B727 SRM 53-10-3 FIG 1.SDR C1HA200795015Floorbeam · corrodedFOUND FLOORBEAM CORRODED AT STA 1110 LBL 25-45. REPAIRED FLOORBEAM STA 1110 FROM RBL 20 TO LBL 65 IAW B727 SRM 53-10-8 FIG 3.SDR C1HA200795018Stringer · crackedFOUND STRINGER 15L CRACKED AT BS 720B. REPAIRED STRINGER 15L AT BS 720B IAW B727 SRM 53-10-3 FIG 5.SDR C1HA200695003Valve · stuckNR 1 ENGINE WAS SHUT DOWN ON START-EGT 550 DEG AND IT APPEARED THAT IT WOULD NOT STABILIZE AT OR BELOW 550 DEG. RAN COM 2-72.9 FOUND NR 1 ENG 13 TH STAGE BLEED VALVES STUCK PER CMM 75-30-00 PAGE 603 LUBED 1 ENG. 13 TH STAGE VALVES WITH WC-393. OPS CHECKED NSDR C1HA200695002Unknown · malfunctionedAFTER TAKEOFF AC FAILED TO PRESSURIZE, RAN COM PROCEDURE 2.21.5. ON DESCENT EQUIP ENTRY LIGHT FLICKERD, RAN COM PROCEDURE 2.52.3. RETURNED TO DEN. INSPECTED BOTH E+E DOORS, FOUND TO BE SECURED AND INSPECTED E+E SWITCHES, NO DEFECTS NOTED. INSPECTED DUCTINGSDR C1HA200695001Seal · damagedON TAXI INTO DEN, UPPER RUDDER INDICATOR DIDN'T MOVE FULLY TO THE LIMIT LINE WHEN RIGHT RUDDER WAS FULLY APPLIED. LEFT RUDDER OPERATED NORMALLY FOUND FIN FAIRING DAMAGED AT NR 6 SPOT ON RT SIDE. REMOVED AND REPLACED FAIRING AND REMOVED DAMAGED RUDDER BLADE SSDR C1HA200595007Connector · looseUPON APPLICATION OF T/O THRUST (FULL), NR 1 ENGINE WOULD NOT MAKE FULL EPR OF 2.14 ONLY 2.05. ALL OTHER PARAMETERS IN YELLOW ARC + POWER LEVER AT FORWARD STOP. ENGINES 2 + 3 POWER LEVERS APPROX 1 1/2 KNOBS BEHIND NR 1 POWER LEVER. (TEMP 31DEG C) ADJUSTED NRSDR C1HA200595006Frame · corrodedE & E COMPT STA 320 RBL 17 FRAME LOWER END HAS CORROSION. EGG NEW FLOOR & CLEAR TIE AT FS 320 RBL 17 7075-0 PO 0420685 H/T TO T-6 ON PEMCO TRAVELER 795N000486. LOCATED, TRIMMED, DRILLED, TREATED & INSTALLED IAW 727 SRM 51-10-2 & 51-30-2 SPLICED NEW FRAME.SDR C1HA200595005Skin · dentedFUSELAGE SKIN 2.7 INCH AFT OF STA 259 AND JUST BELOW STR 17L HAS OUTWARD DENT, MARKED P4. CUT OUT DENT DAMAGE, FAB FILLER USING .050 2024T3 PO 0440785 AND REPAIR DOUBLER USING .063 2024T3 PO 0442440, DRILLED, ALODINE, PRIMED AND INSTALLED FILLER AND REPAIR DOSDR C1HA200595003Angle · crackedLEFT WING LOWER ANGLE CRACKED AT STA WS 124 BELOW NR 7 SPOILER SUPPORT FITTING. REMOVED 2 EA AFT ATTACH BOLTS FROM I/B FLAP TRACK, REMOVED TRACKED LOWER ANGLE CHORD AND 2 EA REPAIR ANGLES IAW B727 SRM 51-30-2. CLEANED REPAIR ANGLES IAW B727 M/M 12-90-00, FABSDR C1HA200595004Keelbeam · crackedRIGHT WHEEL WELL STA 875 ANGLE CRACKED KEELBEAM APPROX 1 INCH LONG. REMOVED AND REPLACED ANGLE IN RIGHT WHEEL WELL AT STA 875 AT KEEL BEAM IAW B727 SRM 51-30-2. REMOVED AND REINSTALLED APU IAW B727 MM 49-10-00. OPS CHECK & LEAK CHECK GOOD IAW B727 MM 42-20-SDR C1HA200595002Skin · crackedLEFT WING - L/E NR 3 SLAT AT O/B SLAT TRACK ATTACH POINT SLAT SKIN IS CRACKED APPROX .5 INCH. TRIMMED CRACKED AREA LENGTH OF CRACK APPROX .500 LONG IAW BOEING 727 SRM 57-50-01 FIGURE 2 SHEET 1-5, FOUND TO BE WITHIN LIMITS IAW BOEING EA PO27-57-014 NDT VERIFIESDR C1HA200595001Skin · crackedLEFT WING - L/E NR 3 SLAT AT I/B SLAT TRACK ATTACH POINT SLAT SKIN IS CRACKED APPROX .5 INCH. TRIMMED CRACKED AREA LENGTH OF CRACK APPROX .500 LONG IAW BOEING 727 SRM 57-50-01 FIGURE 2 SHEET 1-5, FOUND TO BE WITHIN LIMITS IAW BOEING EA PO27-57-014 REQUEST NDTSDR C1HA200495001Support Bracket · brokenNOSE GEAR FAILED TO EXTEND. COMPLIED WITH COM PROCEDURE, CRANKED ALL GEAR MANUALLY.SDR C1HA200395071Battery Pack · inoperativeOVERHEAD EMERGENCY LIGHT INOP AT ROW 4. REMOVED AND REPLACED EMERGENCY BATTERY PACK IAW 727 MM 33-50-22, ALL OPS NORMAL.SDR C1HA200395069Uplock · wornDURING TAKEOFF ROLL RED DOORS LIGHT ON FORWARD PANEL ILLUMINATED, LT GEAR DOOR LIGHT (AMBER) ON ENGINEERS PANEL ILLUMINATED TAKE OFF WAS ABORTED AT 80 KTS. VERY LIGHT BRAKING WAS USED WITH 9000 FEET OF RUNWAY REMAINING FOUND LT MLG UPLOCK ASSY HAD 2 BOLTS WITHSDR C1HA200395068Jackscrew · lack of lubeDURING FLAP RETRACTION AFTER TAKEOFF OUTBOARD FLAPS RETRACTED TO 2 DEGREE POSITION WHILE INBOARDS REMAINED AT 5 DEGREE POSITION. RAN SPLIT FLAP EMERGENCY PROCEDURE INBOARDS REMAINED AT 5 WITH ALTERNATE FLAPS. RETURNED TO ELP, VERIFIED INBOARD FLAPS LOCKED OUSDR C1HA200395066Battery · inoperativeSTA. 950 EMERGENCY CABIN AREA LIGHT IS INOPERATIVE. REMOVED AND REPLACED EMERGENCY CABIN BATTERY ASSEMBLY PER M/M 33-50-21.SDR C1HA200395065Battery Pack · inoperativeLEFT FWD OVERWING OUTSIDE EMERGENCY EXIT LIGHT INOP.SDR C1HA200395064Battery Pack · inoperativeRIGHT FWD OVERWING OUTSIDE EMERGENCY EXIT LIGHT INOP.SDR C1HA200395063Battery Pack · inoperativeLEFT FWD OVERWING EMERGENCY EXIT LIGHT INOP.
Back to N295AS, cancelled Oct 29, 2014