Pratt & Whitney PW2037
Service difficulty reports · 12,810
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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 engine_model_key = 'PW2037' 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 engine_model_key = 'PW2037' 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 UALA2013030401280Unknown · unknownRIGHT AFT OVERWING EMERGENCY EXIT SIGN INOPERATIVE WHEN TESTED. ACCOMPLISHED EMERGENCY LIGHTS SYSTEM AND OPERATIONAL TEST AS REQUIRED. ALL LIGHTS CHECKED GOOD.SDR UALA2013030101231Actuator · faultySTATUS MSG ELEV ASYM T-S PER FIM 27-09-00 FIG 106. REMOVED AND REPLACED ASYMMETRY LIMITER ACTUATOR IAW AMM, OPS CHECK GOOD. P/N 1846T100-3 SN 872 TT 1499375.SDR UALA2013030401243Seat Track · damagedLEFT O/B SEAT TRACK FLOOR SUPPORT O/B SIDE IS DAMAGED AT STA 975. MAJOR REPAIR ACCOMPLISHED. TRIMMED OUT DAMAGED AREA, FABRICATED AND INSTALLED A REPAIR STRAP PER ECRA 5310-05690.SDR UALA2013030401248Floorbeam · corrodedCORROSION IN SEVERAL PLACES BS 1661 RBL 60 TO BL 0 FLOORBEAM. REMOVED CORROSION FOUND ALL AREAS TO BE IN LIMITS IAW B757-200 SRM 53-00-51 FIG 101 DETAI L III EXCEPT DISCREPANT AREA ON UPPER CAP BS 1661 RBL 35 TO RBL 39 WHICH WAS FOUND TO BE OUT OF LIMITS IAW SDR UALA2013030401250Support · corrodedCORROSION AROUND NUT PLATE HOLES ON THRESHOLD SUPPORT CHORD, IN AFT CARGO COMPARTMENT BS 1380 - BS 1440, RBL 26. REMOVED AND REPLACED REPLACED THRESHOLD SUPPORT CHORD IN AFT CARGO COMPARTMENT BETWEEN STA 1380 TO STA 1440 RBL 26.SDR UALA2013030401251Structure · dentedEVALUATE DENTS AT STA 760 AND 765 BETWEEN STR 15L AND 16L. MAJOR REPAIR ACCOMPLISHED. HFEC NO CRACKS. TRIMMED OUT DENTS AT BS 760 AND 765 STR 15L TO 16L DUE TO DENTS OUT OF LIMITS. FABRICATED AND INSTALLED TRIPLER INTERIM REPAIR.SDR UALA2013030401252Skin · dentedAFT CARGO COMPARTMENT DOOR EXT SKIN, LOWER FWD AREA HAS A DENT AT 16 INCHES FROM FWD EDGE AND 14 INCHES FROM LOWER EDGE. MCN 73217:44 27403 6862-23-1 MAJOR REPAIR ACCOMPLISHED. FOUND GOUGE IN DENT. DAMAGE OUT OF LIMITS. TRIMMED OUT DAMAGE, FABRICATED ASDR UALA2013030401254Skin · damagedCS RIVET .098 DIA. NEXT TO .128 DIA. RIVET, PITCH BETWEEN FASTENER .250 BS 1320, BL LBL 2, WL 138. REPAIRED FUSELAGE SKIN AT DISCREPANT FASTENER LOCATION BS 1320 BL 2 WL 138 IAW ECRA 5361-01041, PART 1. HFEC INSP FOUND NO CRACKS.SDR UALA2013030401255Skin · dentedDENT ON LOWER FUSELAGE SKIN AT BS 1738 LBL 10. REPAIRED FUSELAGE SKIN, LOWER AT BS 1738 LBL 10 IAW B757-200 SRM 53-00-01 FIG 201 REPAIR 3. HFEC INSP FOUND NO CRACKS.SDR UALA2013030401259Skin · dentedDENT ON NR 6 LEADING EDGE SLAT JUST INBD OF NR 2 ENGINE DENT IS WITHIN LIMITS OF SRM 57-43-01 LEADING EDGE SLAT SKIN ALLOWABLE DAMAGE FIGURE 101 DENT IS 6" WIDE BY .150 DEEP A OVER Y = 15 OK PER TABLE 7 DENT HAS BEEN NDT AND VISUALLY INSPECTED AND NO DEFECTS NSDR UALA2013030401288Girt Bar · out of positionSLIDE ARM LIGHTS DOOR 1R 4R INOP. RELAMPED DOOR 1R INDICATOR, OPS CHECKS GOOD. REPOSITIONED GIRT BAR AT DOOR 4R, OPS CHECKS GOOD.SDR UALA2013030401289Switch · faultyNO SLIDE ARM LIGHT AT 4R WITH DOOR ARMED. CLEANED ARMED SWITCH AND LIGHT, OPS CHECK GOOD.SDR UALA2013030401290Coupler · unknownLEFT HF COUPLER REPLACED. OPS CHECK REQUIRED OUTSIDE OF HANGER. ACCOMPLISHED TEST AND TESTED OKAY.SDR UALA2013022801207Coupler · faultyLEFT HF RADIO UNABLE TO TRANSMIT. REPLACED LEFT HF COUPLER PER MM, OPS CHECK GOOD. TUNE FREQUENCY 6.640 TOOK BETWEEN 4 AND 7 SECONDS. RADIO TRANSMISSION MADE ON TUNED FREQUENCY TRANSMIT & RECEIVE VOICE COMMUNICATION.SDR UALA2013022801217Engine · faultyDIRTY SOCK ODOR IN COCKPIT AFTER DEPT PASSING THROUGH 7000 FT. LASTED ABOUT 5 MINUTES. REPLACED NR 1 ENGINE PER AM M 71-00-02. COMPLETED INSPECTION OF NR 3 BEARING & PNEUMATIC DUCTS, AND SPINNER. NO OIL FOUND. DRAINED GEARBOX, ONLY TWO QTS FROM GEARBOX. SDR UALA2013030101218Skin · damagedLIGHTNING STRIKE STA 310 BETWEEN S-23L AND S-24L. INTERIM REPAIR INSTALLED STA 304-316 BETWEEN S-22L AND S-24L BY ECRA 5330-04448.SDR UALA2013030101219Skin · damagedLIGHTNING STRIKE STA 329 BETWEEN AT S-23L. INTERIM REPAIR INSTALLED STA 324-334 BETWEEN S-22L AND S-24L BY ECRA 5330-04448.SDR UALA2013030101221Structure · corrodedCORROSION ON FLOORBOARD DIVIDER BS 367 RBL 61. MAJOR REPAIR ACCOMPLISHED. REMOVED AND REPLACED FLOORBOARD DIVIDER BS 367 RBL 61 IAW B757-200 SRM 51-40-02 PAR 7D FIG 12.SDR UALA2013030101222Structure · corrodedCORROSION IN BOLT HOLES, BS 1640, BL 0 TO RBL 64 WL 208. REMOVED CORROSION AT BOLT HOLES FLOORBEAM BS 1640 RBL 64 WL 208 IAW B757-200 SRM 51-10-02-0G PAR 14 FIG 1. ORG MAT THICKNESS IS .125.MAT REMAINING IS .094. MAT REMOVED IS .031 AND IS OUT OF LIMITS IAW SDR UALA2013030101223Floorbeam · corrodedCORROSION ON FLOORBEAM BS 365 BL 0-RBL 63 15EA. FLOORBEAM BS 365 BL 0 - RBL 63 IAW ECRA 5310-05536 REPAIR 3 FIG 203.SDR UALA2013030101224Skin · dentedAFT FUSELAGE SKIN DENTED AT STA 1606 STR 23L. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SKIN, ACP'D HFEC OF SKIN CUT-OUT & FASTENER HOLES. NO DEFECT NOTED. FAB & INSTALLED .050 DOUBLER ON STA 1606 STR 23L-24L PER SRM 53-00-01 RPR 3.SDR UALA2013030101225Skin · dentedAFT FUSELAGE SKIN DENTED AT STA 1549 STR 23L. MAJOR REPAIR ACCOMPLISHED. MAINT TEXT: CUT OUT DAMAGED SKIN, ACP'D HFEC OF SKIN CUT-OUT & FASTENER HOLES. NO DEFECT NOTED. FAB & INSTALLED .050 DOUBLER ON STA 1549 STR 23L-24L PER SRM 53-00-01 REPAIR 3.SDR UALA2013030101232B-Nut · unsecureAPU FIRE BOTTLE ACCESS PANEL HAS FLUID ALONG BOTTOM. SECURED 'B' NUTS ON ELEVATOR FEEL COMPUTER. CLEANED UP FLUID ON APU DOOR AND FIRE BOTTLE ACCESS PANEL.SDR UALA2013030101237Skin · dentedSLAT 3 NOSE SKIN DENT LOCATED 59" FROM I/B END. AT 'C' CHECK MEASURED DENT AND FOUND IT TO BE WITHIN LIMITS OF SRM 57-43-01 FIG 101 DETAIL 7 PG 104. A=1.4 Y=0.020 AY=70 HFEC INSP PER NDT PART 6 51-00-19 NO CRACKS FOUND.SDR UALA2013030101238Skin · gougedRIGHT WING UPPER EXTERNAL SKIN HAS A DENT GOUGE BS 1017, BBL 87 STR U5 FOUND TO BE OUT OF LIMITS. MAJOR REPAIR ACCOMPLISHED. DAMAGE AT RIGHT WING UPPER SKIN BS 1017 BBL 87 STR U5. TRIMMED CUT DAMAGE AND INSTALLED REPAIR PER ESR#23 PER AAR EA 130182 & ECRA 5SDR UALA2013030101239Feeder Cable · defectiveCABIN 'A' ZONE EMERGENCY LIGHT INOPERATIVE. REPAIRED 'A' ZONE EMERGENCY LIGHT FEEDER CABLE, OPS CHECKED GOOD.SDR UALA2013030101240Battery Pack · dischargedRIGHT OVERWING EXIT LIGHT INOPERATIVE. REPLACED RIGHT OVERWING EXIT LIGHT BATTERY PACK PER AMM, OPS CHECK GOOD.SDR UALA2013030101241Feeder Cable · defective'C' ZONE EEL ROW 29 ABC 37ABC INOPERATIVE. REMOVED AND REPLACED FEEDER IAW B757 MM, OPS CHECKS GOOD.SDR UALA2013030101220Skin · damagedLIGHTNING STRIKE BS 345 JUST ABOVE S23L. INTERIM REPAIR INSTALLED BS 340-352 BETWEEN S22-24L IAW ECRA 5330-04448.SDR UALA2013022701202Lever · missingAFT FWD LAV LOCKING LEVER MISSING. REPLACED MISSING AFT FWD LAV LOCKING LEVER. OPS CHECK GOOD.SDR UALA2013022801203Floorbeam · corrodedCORROSION IN SEVERAL PLACES, BS 1640 LBL 65 BL 0 WL 208 FLOORBEAM. MAJOR REPAIR ACCOMPLISHED. REMOVED CORROSION AT BS 1640 LBL 14, 31, AND 56 IAW B757-200 SRM 51-10-02 ORG MAT THICKNESS IS .125 MAX REMOVED IS .011 AND IS WITHIN LIMITS IAW B757-200 SRM 53-00-SDR UALA2013022801204Floorbeam · corrodedCORROSION IN SEVERAL PLACES, BS 1640 LBL 65 BL 0 WL 208 FLOORBEAM. MAJOR REPAIR ACCOMPLISHED. REMOVED CORROSION AT BS 1640 LBL 14, 31 AND 56 IAW B757-200 SRM 51-10-02. ORG MAT THICKNESS IS .125 MAX REMOVED IS .011 AND IS WITHIN LIMITS IAW B757-200 SRM 53-00SDR UALA2013022801214Altimeter · failedCREW REPORTS: CAPT ALTIMETER FAILED FOR SEVERAL MINUTES WITH OFF FLAG TAPS WITH A KNUCKLE BROUGHT IT BACK. REMOVED AND REPLACED CAPTAIN'S ALTIMETER AS OUTLINED IN AMM. ALTIMETER TEST, TESTS NORMAL.SDR UALA2013022801215Blade · damagedBLADE FOD DAMAGE ON LEFT ENGINE NOTED ON SEVERAL BLADES 18 INCHES FROM BLADE TIP-SMALL NICKS. NICKS ARE WITHIN LIMITS PER MM. THE 18 INCHES FROM BLADE TIP IN (AREA 5) NICKS NEED TO BE BLENDED WITHIN 25 HOURS.SDR UALA2013022801216Transceiver · faultySWAPPED HF TRANSCEIVERS FOR TROUBLESHOOTING. SWAPPED HF TRANSCEIVER FOR TROUBLESHOOTING, MR NUMBERS MR23173-199 IN POSITION NR 2 AND MR23173-98 IN POSITION NR 1.SDR UALA2013030401287Adc · faultyF/O ELEC ALTIMETER WRONG. SELECT ALTN STATIC FIXES PROB SEE LOG BOOK FOR READINGS. CREW COMMENTS: F/O ALTM 80 FT HIGHER THAN CAPTS. CORRECTS USING ALTN AIR DATA. REPLACED RIGHT AIR DATA COMPUTER REF AMM. ACCOMPLISHED SELF TEST AND MCDP TEST 30, ALL NORMALSDR UALA2013022701190Transceiver · faultyLEFT HF RADIO FAULTY, FLIGHT DIVERTED. AIRBORNE CLIMBING THROUGH FL190 LEFT HF RADIO TOOK 17 SECONDS TO AUTOTUNE AND WOULD NOT TSMT. REPLACED LEFT TRANSCEIVER AND CALLED SFO ON 6.640 KHZ, OPS CHECK OK. COUPLER TUNED IN 11 SECONDS. ALL WITHIN TOLERANCE OF ASDR UALA2013022701172Floorbeam · corrodedCORROSION ON T-CAP, 3"X2" AREA AT STA 310 WL 208 RBL 39. REPAIRED T-CAP AREA AT STA 310 WL 208 RBL 39 IAW REO-M0602 AND ECRA 5315-01061.SDR UALA2013022701173Floor Support · corrodedCORROSION IN MULTIPLE AREAS ON FLOOR SUPPORT BS 1681 TO BS 1640 LBL 57. MAJOR REPAIR ACCOMPLISHED. CORROSION FOUND TO BE OUT OF LIMITS AT BS 1660-BS 1661 LBL 57. ORIGINAL MATERIAL .071, 100% MATERIAL LOSS IAW BOEING DRAWING 146N5246. REMOVED AND REPLACED FSDR UALA2013022701182Skin · damagedDENT ARCHIVE ITEM APPEARS TO HAVE ADDITIONAL DAMAGE OVER WHAT IS DESCRIBED IN ARCHIVED TXT. AT BS 610, STR 16L TO 17L. REPAIRED AREA IAW SRM 53-00-01 REPAIR 2, FIG 201.SDR UALA2013022701200Cover Plate · brokenUPPER HINGE COVER PLATE AT DOOR 4R FOUND BY CATERING BROKEN. REMOVED COVER PLATE IAW CDL 52A. CONFERRED WITH TOMC.INF:COVER PLATE IS IN IPC 52-11-01-001A ITEM #73 (146N6220-28). ORIGINAL PLATE IS MISSING (NOT IN LOB).SDR UALA2013022801205Oxygen Mask · faultyF/O OXYGEN MASK MICROPHONE VOLUME INAUDIBLE OUT OF F/O COCKPIT SPEAKER. REPLACED F/O OXYGEN MASK PER AMM, CHECK'S OKAY.SDR UALA2013022801206Stowage Box · faultyF/O OXYGEN MASK EXHALE VALVE DOES NOT OPEN PROPERLY WHEN F/O BREATHES. REPLACED CREW OXYGEN STOWAGE BOX PER AMM, CHECK'S OK.SDR UALA2013022601148Sign · intermittentOVERWING EMERGENCY SIGN AT LEFT FWD SIDEWALL IS INOPERATIVE. CYCLED POWER AND OPERATED NORMAL.SDR UALA2013022701171Floorbeam · corrodedCORROSION ON FLOORBEAM WEB UPPER SURFACE BS 1042 LBL 72. REMOVED AND REPLACED FLOORBEAM WEB IAW SRM 51-40-02 FIG 12. FABRICATED NEW FLOORBEAM WEB IAW SRM 51-30-01 FIG 7 AND DRAWING 144N5140. MAJOR REPAIR.SDR UALA2013022701175Structure · corrodedCORROSION ON LONGERON BETWEEN RBL 65-72. BLENDED CORROSION ON LONGERON BS 369 IAW SRM 51-10-02 PAR 15 FIGS 1&5. REMOVED AND REPLACED LONGERON IAW SRM 51-40-02 PAR 7D. MAJOR REPAIRSDR UALA2013022701176Floorbeam · corrodedCORROSION ON AFT CABIN FLOORBEAM REPAIR ANGLE LOWER SURFACE BS 1680 RBL 47 WL 208. REMOVED LWR REPAIR ANGLES. LOCATED, DRILLED AND INSTALLED REPAIR ANGLE IAW SRM 53-60-51 REPAIR 3 FIG 201. MAJOR REPAIR.SDR UALA2013022701177Web · corrodedMAIN CABIN SUB FLOOR WEB, CORRODED SEVERAL PLACES BS 1680, RBL 40 - 60. REMOVED AND REPLACED WEB IAW 51-40 02 AND ECRA 5330-04259. REPAIR DOUBLER INSTALLED. MAJOR REPAIR.SDR UALA2013022701178Stringer · damagedBS 610 STRINGER 17L HAS DOUBLE DRILLED HOLE. REPAIRED STRINGER IAW ECRA 5361-01040 AND REO 615957 REV A. MAJOR REPAIR.SDR UALA2013022701179Frame · gougedFWD CARGO DOOR LOWER END ATTACH FRAME IS GOUGED IN SEVERAL PLACES. REMOVED AND REPLACED LOWER ATTACHED FRAME IAW SRM. MAJOR REPAIR.
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