N313AW, cancelled Oct 13, 2011
Service difficulty reports · 261
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 = 'N313AW' AND deregistration_id = 'N313AW-2011-10-13' 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 = 'N313AW' AND deregistration_id = 'N313AW-2011-10-13' 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 AWXA200500942Web · crackedDURING C18 CHECK DISCOVERED L1 DOOR CUTOUT WEB CRACKED, .5 INCHES IN LENGTH, AT THE FORWARD INBOARD SIDE AT BS 294.5, STRINGER 12L. MAINTENANCE REMOVED THE L1 DOOR CUTOUT AT BS 294.5, STRINGER 12L WEB IAW BOEING 737-300 SRM 51-40-02-0. FABRICATED NEW INTERCOSDR AWXA200500941Angle · corrodedDURING C18 CHECK DISCOVERED CORROSION ON FLOOR WEB ANGLE AT BS 270, FROM BL8L TO BL8R. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-10-51-1 FIG 101. MAINTENANCE REMOVED DAMAGED SECTION ON ANGLE AT BS 270, BL8L TO BL8R IAW BOEING 737-300SDR AWXA200500940Angle · corrodedDURING C18 CHECK DISCOVERED CORROSION ON THE R1 INNER CHORD, UPPER ANGLE AT BS 305 TO BS 324, BL 58R, WL 209. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-10-13-1 FIG 101. MAINTENANCE REMOVED ANGLE AT BS 305 TO BS 324, BL 58R, WL 209 IAWSDR AWXA200500933Beam · corrodedDURING C18 CHECK DISCOVERED CORROSION ON BS 312 BEAM FROM BL 0 TO BL 21R, WL 208. PREVIOUS BLEND OUT PRESENT, MATERIAL LOSS GREATER THAN ALLOWED, IAW BOEING 737-300 SRM 53-10-51-1. MX CUT OUT DAMAGED SECTION OF BEAM IAW BOEING 737-300 SRM, 53-10-51-2 FIG 205SDR AWXA200500833Support Angle · crackedMCN - MAJOR REPAIR - DISCOVERED, DURING C16 CHECK, L1 DOOR CUTOUT SIDEWALL LINER SUPPORT ANGLE CRACKED AT BS 344, ST 14L. MAINTENANCE REMOVED THE DAMAGED AREA ON THE SUPPORT ANGLE FOR THE L1 DOOR CUTOUT SIDEWALL LINER IAW BOEING 737-300 SRM 51-70-11-0 FIG. 1.SDR AWXA200500997Skin · debondedMCN - DURING C18 CHECK, DISCOVERED DISBOND AREA ON TOP SURFACE OF THE NR 3 SLAT AT THE INBOARD END. MAINTENANCE REMOVED DISBOND SKIN AND CORE ON THE NR 3 SLAT IAW BOEING 737-300 SRM 51-70-10-0 FIG 16. FABRICATED REPAIR DOUBLER AND CORE IAW BOEING 737-300 SRMSDR AWXA200500984Skin · crackedMCN - DURING C18 CHECK, DISCOVERED FOUR CRACKS IN THE NR 1 SLAT, .250 INCHES IN LENGTH, LOCATED AT THE LOWER SKIN AT OUTBOARD END SS 385. MAINTENANCE REMOVED AND REPLACED THE NR 1 SLAT IAW BOEING 737-300 AMM 27-81-21-004-001 AND 27-81-21-404-002. OPERATIONALSDR AWXA200500959Frame · crackedDURING C18 CHECK DISCOVERED FRAME CRACKED, .17 INCHES IN LENGTH, UNDER DOOR ASSIST HANDLE AT THE R2 DOOR, BS 954, STR14R. MAINTENANCE TRIMMED OUT CRACK AT DOOR ASSIST HANDLE AT THE R2 DOOR, BS 954, STR 14R IAW AMERICA WEST AIRLINES (AWA) ENGINEERING REPAIR (ESDR AWXA200500924Spoiler · debondedDURING C18 CHECK FOUND A DISBOND AREA ON THE UPPER SURFACE OF THE NR 4 SPOILER, 36" FROM INBOARD END FROM WBL 123.75 TO WBL 135.75. MAINTENANCE REMOVED DISBOND AREA FROM THE UPPER SURFACE OF THE NR 4 SPOILER, 36" FROM INBOARD END IAW BOEING 737-300 SRM. FABRSDR AWXA200500918Clip · crackedDURING C18 CHECK FOUND SEVERAL CLIPS CRACKED LOCATED AT BS 380, STRINGER 1 (1.5" LONG), STRINGER 2R (1.5" LONG) AND STRINGER 8L (.26" LONG). MAINTENANCE REMOVED CRACKED CLIPS AT BS 380, STRINGER 1, STRINGER 2R AND STRINGER 8L IAW BOEING 737-300 SRM 51-40-02-0SDR AWXA200500916Clip · crackedDURING C18 CHECK DISCOVERED ATTACH CLIP AT BS 500A, STRINGER 16R CRACKED .275 INCHES IN LENGTH. MAINTENANCE REMOVED CRACKED CLIP AT BS 500A, STRINGER 16R. RECEIVED AND PREPARED NEW STRINGER CLIP FOR INSTALLATION IAW BOEING 737-300 SRM 51-40-05-0 FIG 2 & 3. SDR AWXA200500994Skin · crackedMCN - DURING C18 CHECK DISCOVERED, 4 CRACKS IN THE NR 2 SLAT SKIN BELOW THE INBOARD AUXILIARY TRACK, FROM SS 90 TO SS 164. MAINTENANCE REMOVED DAMAGED AREA OF NR 2 SLAT SKIN BELOW THE INBOARD AUXILIARY TRACK, FROM SS 90 TO SS 164 IAW BOEING 737-300 SRM 57-43SDR AWXA200500993Skin · crackedDURING C18 CHECK DISCOVERED, THE NR 3 SLAT SKIN AT OUTBOARD END, SS 124, CRACKED .375 INCHES IN LENGTH. MAINTENANCE REMOVED DAMAGED AREA OF THE NR 3 SLAT SKIN IAW BOEING 737-300 SRM 57-43-01-2. FABRICATED FILLER AND SPLICE PLATE IAW BOEING 737-300 SRM 52-43-SDR AWXA200500925Tab · delaminatedDURING C18 CHECK DISCOVERED, THE LT HORIZONTAL ELEVATOR TAB DELAMINATED, AT OUTBOARD END, TOP SURFACE FROM ES 127L TO ES 129L. MAINTENANCE CUT OUT DELAMINATED AREA ON THE LT HORIZONTAL ELEVATOR TAB IAW BOEING 737-300 SRM 51-70-17-0 FIG 11. SANDED AND CLEANEDSDR AWXA200500922Frame · crackedDURING C18 CHECK DISCOVERED ANGLE CRACKED, .375 INCHES IN LENGTH, AT FORWARD UPPER CORNER OF THE R1 DOOR, CUTOUT. MAINTENANCE CUT OUT CRACKED AREA OF FRAME ANGLE IAW BOEING 737-300 SRM 51-70-11-0. FABRICATED FILLER AND DOUBLER IAW BOEING 737-300 SRM 51-70-11SDR AWXA200500915Skin · crackedDURING C18 CHECK DISCOVERED FUSELAGE SKIN CRACK, 1.43 INCHES IN LENGTH, AT BS 727E+4 INCHES, STRINGER 24R. MAINTENANCE CUT OUT DAMAGED AREA OF SKIN AT BS 727E+4 INCHES, STRINGER 24R IAW BOEING 737-300 SRM 53-00-01-3 FIG 229. FABRICATED DOUBLER, TRIPLER AND SDR AWXA200500909Clip · crackedDURING C18 CHECK DISCOVERED CLIP CRACKED, .375 INCHES IN LENGTH, AT BS 336 STRINGER 6R. MAINTENANCE REMOVED CRACKED CLIP AT BS 336 STRINGER 6R IAW BOEING 737-300 SRM 51-40-02-0 FIG 8. FABRICATED NEW CLIP IAW BOEING 737-300 DWG 65-45874 AND BOEING 51-30-01-0 SDR AWXA200500907Stringer Clip · crackedDURING C18 CHECK DISCOVERED STINGER CLIP CRACKED, .200 INCHES IN LENGTH, AT BS 277, STRINGER 10R. MAINTENANCE REMOVED STRINGER CLIP AT BS 277, 10RT IAW BOEING 737-300 SRM 51-40-02-0 FIG 8. FABRICATED NEW STRINGER CLIP IAW BOEING DWG 65-45805. MAINTENANCE INSDR AWXA200500930Frame · crackedDURING C18 CHECK DISCOVERED R1 DOOR FORWARD STOP CUTOUT, FOURTH FROM TOP, CRACKED, .60 INCHES IN LENGTH. MAINTENANCE TRIMMED OUT CRACK AREA AT R1 DOOR FORWARD STOP CUTOUT, FOURTH FROM TOP IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5200-5214-SS1. FABRSDR AWXA200500921Strap · crackedDURING C18 CHECK DISCOVERED STABILIZER STRAP CRACKED, .65 INCHES IN LENGTH, ON CABIN FLOOR AT BS 330, BL 15L, WL 204. MX STOP DRILLED CRACK IN STABILIZER STRAP AT BS 330, BL 15L, WL 204 IAW BOEING 737-300 SRM 53-10-51-2. FABRICATED REPAIR PLATE IAW BOEING 7SDR AWXA200500917Wedge · delaminatedDURING C18 CHECK DISCOVERED LT INBOARD FORE FLAP LOWER SURFACE DELAMINATED, AT THE INBOARD TRACK ATTACHMENT. MAINTENANCE REMOVED DAMAGED AREA ON THE LT INBOARD FORE FLAP LOWER SURFACE AND CLEANED AREA IAW BOEING 737-300 SRM 51-70-10. FABRICATED FILLER AND DOSDR AWXA200500914Wedge · delaminatedMCN - DURING C18 CHECK, DISCOVERED THE LT OUTBOARD AFT FLAP DELAMINATED AT THE INBOARD END OF THE UPPER AND LOWER SURFACES AT WBL 23.68 TO WBL 235.68. MAINTENANCE REMOVED DAMAGED AREA ON THE LT OUTBOARD AFT FLAP AND PREPARED FOR REPAIR IAW BOEING 737-300 SRM SDR AWXA200500932Structure · crackedDURING C18 CHECK DISCOVERED SEVERAL SUBSTRUCTURES CRACKED AT THE L1 FWD ENTRY DOOR CUTOUT FROM STR 15L TO STR 16L, BS 348.20. MX REMOVED ALL DAMAGED PARTS, (1) CLIP CRACKED .5", (2) CLIP CRACKED .5", (3) CLIP CRACKED .5", (4) CLIP CRACKED .5" IAW AMERICA WESTSDR AWXA200500433Wire · backed outPHX - EEL - DURING 4-DAY CHECK FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 2 LT INOPERATIVE. MAINTENANCE FOUND WIRE PULLED OUT OF RECEPTACLE WITH EVIDENCE OF ARCHING. REPLACED EMERGENCY ESCAPE PATH LIGHT WIRE HARNESS AT SEAT ROW 2 LT, OPERATIONAL WAS GSDR AWXA200500022Packing · tornLAS - DIVERSION - FLT 0765 - APPROXIMATELY 20 MINUTES OUT OF PHX EN ROUTE TO SMF NOTICED HYDRAULIC FLUID LEAKING FROM THE TOP OF LEFT WING, ALSO OBSERVED B-SYSTEM HYDRAULIC QUANTITY DECREASING, FLUID LEVEL STABILIZED AT 1/2 QUANTITY ON INDICATOR, DIVERTED INTOSDR AWXA200400464Support Angle · crackedMCN - MAJOR REPAIR - DURING C-17 CHECK A 1 INCH CRACK WAS FOUND IN SUPPORT ANGLE (CLIP) OF AFT CARGO COMPARTMENT DOOR SILL BS 807, RBL 30. MAINTENANCE REMOVED CRACKED SUPPORT ANGLE (CLIP) AT AFT CARGO COMPARTMENT DOOR SILL BS 807, RBL 30; FABRICATED A NEW REPSDR AWXA200400474Web · corrodedMCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT DOOR SILL WEB IN SEVERAL LOCATIONS BETWEEN BS 794.3 AND BS 847, RBL 20. MAINTENANCE REMOVED CORRODED SECTION OF AFT CARGO COMPARTMENT DOOR SILL WEB FROM BS 794.3 TOSDR AWXA200400466Strap · corrodedDURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT DOOR SILL WEB (STRAP) BS 794.3, RBL 20. MAINTENANCE REMOVED CORRODED AFT CARGO COMPARTMENT DOOR SILL STRAP AT BS 794.3, RBL 20; FABRICATED A NEW REPLACEMENT STRAP PER DWG 65-47957; INSTSDR AWXA200400456Support Angle · corrodedMCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT DOOR SILL SUPPORT ANGLE AT BS 794.3, RBL 20. MAINTENANCE REMOVED CORRODED AFT CARGO DOOR SILL SUPPORT ANGLE, BS 794.3, RBL 20; FABRICATED A NEW REPLACEMENT ANGLE PSDR AWXA200400453Reveal · corrodedMCN - MAJOR REPAIR - DURING C-17 CHECK CORROSION WAS FOUND ON R-1 DOOR CUTOUT UPPER AFT REVEAL AT FASTENER HOLE BS 336, STR 10 RT. MAINTENANCE REMOVED CORRODED R-1 DOOR UPPER AFT REVEAL AT BS 336, STR 10 RT; FABRICATED A NEW REPLACEMENT REVEAL; INSTALLED REPASDR AWXA200400454Panel · crackedMCN - MAJOR REPAIR - DURING C-17 CHECK A 1 INCH CRACK WAS FOUND IN NR 5 SLAT OUTBOARD COVE PANEL SKIN AT STAB STA 255.7. MAINTENANCE REMOVED CRACKED NR 5 SLAT OUTBOARD COVE PANEL AT SS 255.7; FABRICATED A NEW REPLACEMENT PANEL PER DWG 65C26602; INSTALLED REPASDR AWXA200400467Web · corrodedMCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND UNDER FORWARD INBOARD CORNER OF AFT CARGO COMPARTMENT DOOR SILL WEB BS 794, RBL 30. MAINTENANCE REMOVED CORRODED AFT CARGO COMPARTMENT DOOR SILL WEB AT BS 794, RBL 30; FABRICATED A NEW REPLSDR AWXA200400465Web · crackedMCN - MAJOR REPAIR - DURING C-17 CHECK A 1/2 INCH CRACK WAS FOUND IN L-1 DOOR SILL WEB, BS 328, LBL 60. MAINTENANCE REMOVED CRACKED L-1 DOOR SILL WEB AT BS 328, LBL 60; FABRICATED A NEW REPLACEMENT WEB PER DWG 65-17688; INSTALLED REPAIR PART IAW B737-300 SRM 5SDR AWXA200400450Bolt · corrodedMCN - MAJOR REPAIR - DURING C-17 CHECK GALVANIC CORROSION WAS FOUND ON RT VERTICAL STABILIZER FORWARD SPAR TO BODY BOLT BS 1016, STR 2 RT. MAINTENANCE REMOVED AND REPLACED RT VERTICAL STABILIZER FORWARD SPAR TO BODY BOLT IAW T/C I6B5502.SDR AWXA200400446Bolt · corrodedMCN - MAJOR REPAIR - DURING C-17 CHECK GALVANIC CORROSION WAS FOUND ON THE LT VERTICAL STABILIZER FORWARD SPAR TO BODY BOLT BS 1016, STR 2 LT. MAINTENANCE REMOVED AND REPLACED L/H VERTICAL STABILIZER FORWARD SPAR TO BODY BOLT IAW T/C I6B55002.SDR AWXA200400451Bolt · corrodedMCN - MAJOR REPAIR - DURING C-17 CHECK GALVANIC CORROSION WAS FOUND ON RT AFT INBOARD VERTICAL STABILIZER ATTACH BOLT BS 1085, STR 2 RT. MAINTENANCE REMOVED AND REPLACED RT AFT INBOARD VERTICAL STABILIZER ATTACH BOLT IAW T/C I6B55002.SDR AWXA200400439Vertical Beam · crackedMCN - MAJOR REPAIR - DURING C-17 CHECK A 1/2 INCH CRACK WAS FOUND IN BS 178 BULKHEAD VERTICAL WEB BEAM AT LBL 5.7, WL 176. MAINTENANCE CUTOUT DAMAGED SECTION OF BS 178 BULKHEAD VERTICAL WEB; PERFORMED A HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRSDR AWXA200400441Intercostal · crackedMCN - MAJOR REPAIR - DURING C-17 CHECK A 1" CRACK WAS FOUND IN UPPER ANGLE OF INTERCOSTAL BETWEEN BS 927 AND BS 947, BL "0". MAINTENANCE REMOVED CRACKED UPPER ANGLE ON INTERCOSTAL FROM BS 927 TO BS 947, BL "0"; FABRICATED A NEW REPLACEMENT UPPER INTERCOSTAL ANSDR AWXA200400445Bolt · corrodedDURING C-17 CHECK GALVANIC CORROSION WAS FOUND ON THE RT HORIZONTAL STABILIZER FORWARD LOWER ATTACH BOLT BS 1088, WL 258. MAINTENANCE REMOVED AND REPLACED R/H HORIZONTAL STABILIZER FORWARD LOWER ATTACH BOLT IAW T/C I6C55038.SDR AWXA200400499Skin · crackedMCN - MAJOR REPAIR, DURING C-17 CHECK A .2500 CRACK WAS FOUND AT FASTENER HOLE IN FUSELAGE SKIN AT LOWER FORWARD CORNER OF R-2 DOOR CUTOUT BS 981.8 TO BS 984.8, WL 198. MAINTENANCE STOP DRILLED CRACK AND PERFORMED A HFEC INSPECTION TO VERIFY CRACK WAS CONTAINSDR AWXA200400452Skin · bulgedMCN - MAJOR REPAIR - DURING C-17 CHECK THE SKIN WAS FOUND BULGING BETWEEN FASTENERS INSIDE THE FORWARD CARGO COMPARTMENT AT A PREVIOUSLY INSTALLED REPAIR DOUBLER BS 370 TO BS 390, RBL 36. MAINTENANCE REMOVED REPAIR DOUBLER BS 370 TO BS 390, RBL 36 AND FOUND ESDR AWXA200400475Stringer · corrodedDURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON STRINGER 27 LT AT BS 967. MAINTENANCE CUTOUT DAMAGED SECTION OF STRINGER 27 L/H AT BS 967; FABRICATED A 4 EACH ANGLES & SHIMS, 2 EACH CHANNELS, AND A HAT SECTION; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-0SDR AWXA200400437Floor Support · crackedMCN - MAJOR REPAIR - DURING C-17 CHECK A 1 INCH CRACK WAS FOUND IN FORWARD CABIN FLOOR SUPPORT ANGLE BETWEEN BS 380 AND BS 400, AT BL "0". MAINTENANCE REMOVED CRACKED FLOOR SUPPORT ANGLE FROM BS 380 TO BS 400, AT BL "0"; FABRICATED A NEW REPLACEMENT FLOOR SUPPSDR AWXA200400498Angle · corrodedMCN - MAJOR REPAIR, DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON L-1 DOOR SILL IB STIFFENER ANGLES AT SCREW HOLES BS 328, LBL 60. MAINTENANCE REMOVED 2 EACH CORRODED STIFFENER ANGLES AT BS 328, LBL 60; FABRICATED 2 EACH NEW REPLACEMENT ANGLES IAW DWG 6SDR AWXA200400482Panel · crackedDURING C-17 CHECK 2 EACH CRACKS WERE FOUND ON NR 6 SPOILER PANEL ABOVE ACTUATOR AT WBL 245 RT. MAINTENANCE REMOVED AND REPLACED NR 5 SPOILER PANEL IAW AMM 27-62-11, FIG. 401, PG. 1-5.SDR AWXA200400476Skin · delaminatedDURING C-17 CHECK FOUND THE UPPER NO. 5 SLAT WEDGE DELAMINATED AT SS 147.5. MAINTENANCE REMOVED PREVIOUSLY INSTALLED REPAIR DOUBLERS ON NO. 5 SLAT WEDGE AT SS 147.5; FABRICATED NEW REPLACEMENT DOUBLERS; BONDED REPAIR PARTS TO SLAT IAW B737-300 SRM 51-70-10, FISDR AWXA200400481Panel · corrodedMCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON NO. 5 SPOILER PANEL ALONG LEADING EDGE OF LOWER SEAL BETWEEN WBL 71.24 AND WBL 191 R/H. MAINTENANCE REMOVED AND REPLACED NO. 5 SPOILER PANEL IAW AMM 27-62-12, FIG. 401, PG. 1-5.SDR AWXA200400480Seat Track · crackedDURING C-17 CHECK EXFOLIATION CORROSION AND A 1 INCH CRACK WAS FOUND ON SEAT TRACK BS 420 TO BS 425, RBL 45. MAINTENANCE REMOVED DAMAGED SECTION OF SEAT TRACK FROM BS 380 TO BS 480, RBL 45; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK PER DWG 65-46813; ISDR AWXA200400443Skin · delaminatedDURING C-17 CHECK THE UPPER SURFACE OF LT OUTBOARD FORE FLAP WAS FOUND DELAMINATED 89.5 INCHES FROM INBOARD END WS 378 TO WS 386. MAINTENANCE REMOVED DELAMINATED PREVIOUS REPAIR ON LT OUTBOARD FORE FLAP FROM WS 378 TO WS 386; FABRICATED A REPAIR DOUBLER; BONDESDR AWXA200400442Wedge · delaminatedDURING C-17 CHECK THE UPPER SURFACE OF LT INBOARD MID FLAP TRAILING EDGE WEDGE WAS FOUND DELAMINATED 9 INCHES FROM INBOARD END. MAINTENANCE CUTOUT DAMAGED UPPER SKIN AND CORE ON LT INBOARD MID FLAP TRAILING EDGE AT WS 82 LT; FABRICATED A NEW REPLACEMENT CORE A
Back to N313AW, cancelled Oct 13, 2011