Pratt & Whitney PW2037
Service difficulty reports · 12,809
Newest first. General aviation reporting is voluntary.
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 CALA2015083194263Cover · unsecureEMERGENCY LIGHTING STRIP AT SEAT ROWS 32 - 34 INOPERATIVE. SECURED COVER TESTED LIGHT IAW 33-51-96-0401.SDR DALA2015082105124Engine · making metalDIVERTED DUE TO A RT ENGINE OIL FILTER CAUTION EICAS MESSAGE. FOLLOWED THE QRH AND THE ENGINE WAS SHUTDOWN. EMERGENCY WAS DECLARED. TROUBLESHOT IAW FIM 79-21-00-815-803-P00. FOUND MAGNETIC CHIP DETECTOR CONTAMINATED IN EXCESS OF INSPECTION LIMITS AMM 79-21SDR CALA2015082094233Switch · inoperativeEMERGENCY LIGHT TEST SWITCH AT L2 DOOR INOPERATIVE. R & R EMER LIGHT TEST SWITCH AT L2 DOOR. PERFORMED OPERATIONS CHECK & FOUND OK IAW SWPM 20-84-14 & AMM 33-51-00.SDR CALA2015082094234Skin · dentedDURING FINALIZING INSPECTION ON HORIZONTAL STAB PIVOT PINS NOTICED A DENT AT BOTTOM SURFACE OF LT HORIZONTAL STAB AT INCHES DIAMETER. INSTALLED REPAIR ON HORIZONTAL STAB LOWER SKIN INBD SIDE IAW SRM 51-70-01. R4 APPROX LE EDGE STATION 94.455 & 17" AFT OF AUXSDR DALA2015081905027Idg · failedACFT 680, ON TAKEOFF ROLL, NR 2 IDG DROPPED OFF LINE. ABORTED TAKEOFF. PERFORMED BITE OF BPCU IAW FIM 24-20-00-810-802. FAULTS RIGHT IDG. REPLACED RT IDG IAW AMM 24-11-01. TESTS GOOD AND NO LEAKS IAW AMM 71-00 AND 24-11.SDR CALA2015081494220Skin · dentedTWO DENTS WERE FOUND OUT OF LIMITS AT 619, STRINGER 16L. INSTALLED REPAIR AT FUSELAGE SKIN BS 615 - 624.5, STRINGER 16L IAW SRM 53-00-01 REP 3 FIG 201.SDR CALA2015081194193Light · looseEMERGENCY EXIT FLOOR STRIP LIGHTS LOOSE AT 26C. SPLICED IN NEW PIECE OF CABLE & SECURED COVER. OPERATIONS CHECKED NORMAL.SDR CALA2015080794182Cusp Web · corrodedMAIN CABIN CORROSION ON WEB CUSP STATION 1180, STRINGER 17R. FABRICATED & INSTALLED NEW CUSP WEB IAW SRM 53-40-13 PG 3 FIG 1 SH 3 OF 4. PN 144N5210-4 FABRICATED FROM 7075-0, .063, HEAT TREAT TO 7075 T6. INSTALLED IAW SRM 51-40 -02.SDR DALA2015071604452Liner · damagedFOUND DAMAGE TO LINER AFT OF FAN 7 O'CLOCK POSITION ON NR 1 ENGINE INSTALLED, PERMANENT REPAIR IAW MM 72-33-03-348-010.SDR CALA2015070694051Pca · faultedSPOILERS MSG ON UPPER EICAS INFLIGHT WHEN EXTENDING FULL FLAPS SET AT 15 DEG. REF WD 27-61-13 TO 18 SPOILERS PCA'S RESISTANCE CHECK OK. PER PREVIOUS PCA NR 2 FAULTED. ACCOMPLISHED SPOILERS PCA NR 2 & 11 RVDT PHASE SYNC VOLTMETER IAW MM 27- 61-00 P 500 PROCESDR DALA2015071504394Unknown · odorAFTER TAKE OFF AND ON GEAR RETRACTION, A BURNED RUBBER ODOR WAS IN THE COCKPIT, LASTING APPROXIMATELY 2 MINUTES. DURING CLIMB, F/A SMELLED SWEET/ELECTRICAL ODOR IN L2 LAVATORY AREA. SLIGHT VIBRATION LATE TAKE OFF ROLL THROUGH GEAR RETRACTION. 3 HOURS INTOSDR CALA2015062994030Wire · damagedEMERGENCY EXIT LIGHT TRACK COVER CAME OFF WITH WIRE DAMAGED IN AFT CABIN. REPAIRED & CHECKED EMER EXIT LIGHT FOR CORRECT OPERATION.SDR CALA2015062994033Skin · gougedSKIN GOUGE FOUND IN SECTION 48 AREA UPPER SKIN SURFACE, APPROX STRINGER 3L. DURING NDT INSPECTION NOTED SMALL CRACK. SMALL HOLE REPAIR IAW SRM 53-00-01 REPAIR 7.SDR CALA2015062994034Skate Angle · cracked2 SHEARED FASTENERS AT ATTACH ANGLE, RT LOWER SURFACE, OTBD PYLON AFT FAIRING AREA. REMOVED FASTENERS. FOUND SKATE ANGLE AT RT WING TO NACELLE OTBD PYLON SIDE CRACKED. ANGLE PN 112N4006-2 WAS FABRICATED IAW OEM DWG 112N4006SH1-4. NO DEVIATIONS. NO FURTHERSDR CALA2015062994028Pca · faultyUNCOMMANDED ROLL TO THE RT WITH THE RT SYS HYD SELECTED OFF. INSTALLED NR 11 SPOILER PCA IAW AMM 27-61-02. OPERATIONS CHECKED OK.SDR CALA2015062694022Heat Exchanger · malfunctionedCABIN ALTITUDE 10,000 FEET AT FL300, DIVERTED. FOUND SECONDARY HEAT EXCHANGER BLOWN OUT AT LOWER END. REPLACED IAW AMM 21-51-02.SDR CALA2015061993996Structure · crackedL2 DOOR UPPER HINGE CUT OUT CRACKED. CF 9128 DATED 2/27/15. REMOVE, MFG & INSTALLED PART 1 ANGLE IAW SRM 52-10-02 REPAIR 1.SDR CALA2015061193890Fcu · faultyENGINE 1 ENG VLV LIGHT CAME ON DURING FLIGHT, ALL ENG PARAMETERS WERE NORMAL. VLV WENT OFF AT SHUTDOWN. REPLACED RELAYS K10462 & K10463 PRECAUTIONARY. WHILE ACCOMPLISHING FIM 76-11-00 BLOCK 1, 11,21 PG 110, FOUND FUEL CONT UNIT CONN PARTIAL. REPLACED NR 1 SDR CALA2015060893870Connector · unsecureEMERGENCY LIGHTS INOPERATIVE AT OVERWING EXITS LT FWD & RT AFT DOORS. SECURED CONNECTOR AT POWER SUPPLY 20 ABC. EXIT LIGHTS CHECKED GOOD.SDR CALA2015060893877Frame · dentedAFT PIT FRAME DENTED STATION 1400, STRINGER 25L - 26L, WU 46814. INSTALLED DOUBLER REPAIR IAW SRM 53-00-07 REPAIR 5 DETAIL III PG 208 & SRM 51-40-02, SRM 53-00-07 REPAIR 5 PAGE 210 TABLE II. AIRPLANE SOLD AS IS. BUYER WAS AWARE OF THIS ITEM PRIOR TO SALE BESDR CALA2015060893878Frame · dentedAFT PIT STATION 1480, STRINGER 26L, FRAME DENTED. REPAIRED FRAME DENTS IAW SRM 53-00-07 REPAIR 5 TABLE II ZONE 1. AIRPLANE SOLD AS IS. BUYER WAS AWARE OF THIS ITEM PRIOR TO SALE BEING FINALIZED.SDR CALA2015060893879Frame · dentedAFT PIT STATION 1540, BETWEEN STRINGER 25L & 27L FRAME DENTED, 3 EA DENTS. REPAIRED FRAME DENTS IAW SRM 53-00-07 REPAIR 5 TABLE II ZONE 1. AIRPLANE SOLD AS IS. BUYER WAS AWARE OF THIS ITEM PRIOR TO SALE BEING FINALIZED.SDR CALA2015060893880Skin · damagedLEFT LOWER FUSELAGE FWD OF STATION 1701 ABOVE THE PREVIOUS REPAIR DOUBLER SKIN HAS DENT OR HAS BEEN BLENDED & PAINTED. INSTALLED A SKIN REPAIR BETWEEN BS 1685 & 1710, STRINGER 18L & 21L IAW ECRA 5360-01328. AIRPLANE SOLD AS IS. BUYER WAS AWARE OF THIS ITEM SDR CALA2015060893881Skin · dentedDENT LOCATED AT STATION 755 BETWEEN STRINGER 15L & 16L, MEASURING 1.5"W X 1.75"L & .070"D IS TO BE REPAIRED AT THE NEXT C CHECK. THAT CHECK IS NOW BEING ACCOMPLISHED. EA 130704 & ECRA 5330-04658 HAVE BEEN ISSUED IN ORDER TO REPAIR THE DENT WITH THE INSTALLATSDR CALA2015060893882Skin · damagedPER TASC CARD 597454012 INSTALL DOUBLER AT STATION 1393. ACCOMPLISH THIS TASK IAW EA 130660 & ECRA 5360-0 1313. THE SKIN REPAIR AT BS 1384 - 1401 BETWEEN STRINGER 28L & 29R HAS BEEN APPROVED AS STRINGER 1 & 2 VIA FORM 8100-9 DATED 6-7-13. REPAIRED EXTERIOR SDR CALA2015052193801Light · inoperativeDURING TESTING FOUND MED 2 LT EMER EVACUATION LIGHT INOPERATIVE. RELAMPED EXTERIOR EMER EVACUATION LIGHT & TESTED, NO DEFECTS NOTED.SDR DALA2015052203434Skin · delaminatedNR 1 ENGINE, INBD FAN COWL, INNER SIDE HAS AREAS OF DELAMINATION. REMOVED DAMAGE AND APPLIED REPAIR IAW SRM.SDR CALA2015052693810Light · inoperativeDURING TESTING FOUND MAIN ENTRY DOOR 2LT EMER EVACUATION LIGHT INOPERATIVE. RELAMPED EXTERIOR EMER EVACUATION LIGHT & TESTED, NO DEFECTS NOTED.SDR CALA2015051593780Light · inoperativeEMERGENCY LIGHTING DOES NOT TURN ON IN FRONT OF AFT FWD LAVATORY FLOOR. REPLACED EMER LIGHT LAMP STRIP. EMER LIGHT TEST FROM AFT ATTENDANT PANEL OK IAW AMM 33-51-00.SDR CALA2015051593786Stringer Splice · corrodedAFT PIT STRINGER 28R SPLICE CORRODED AT STATION 1458. SPLICE REPLACED IAW DWG 146N3820 & SRM 51-40-02.SDR CALA2015051593787Angle · crackedDOOR 2L LT FWD FRAME, EXISTING REPAIR ANGLE WAS FOUND CRACKED. REPAIRED ANGLE. FABRICATED & INSTALLED IAW SRM 52-10-02 FIG 201 REPAIR 1.SDR CALA2015050193648Oven · smokeCREW REPORTS MOMENTARY SMOKE FROM FWD GALLEY OVEN 107, FOOD ODOR. FOOD REMOVED & OVEN NOT USED FOR THE REST OF THE FLIGHT. ACCOMPLISH MM 05-51-56 P201, REMOVED CHOCOLATE CHIP COOKIE DOUGH THAT WAS STUCK TO THE TOP OF THE OVEN, CLEANED AS REQUIRED. CYCLED OVSDR DALA2015043003078Filter · leakingCREW REPORTED A FUEL DISAGREE-PROG 2 MESSAGE AFTER 4 HRS OF FLIGHT WITH A 3500LB DIFFERENCE BETWEEN TOTALIZER AND CALCULATED. THE CHECKLIST WAS USED TO VERIFY THAT THERE WAS NOT A FUEL LEAK. TOTALIZER WAS 3500 LB LESS THAN CALCULATED. MAINTENANCE TROUBLESHOSDR DALA2015042002813Control Valve · failedDESCENDING OUT OF FL330 TO FL270 CABIN ALTITUDE LIGHT ILLUMINATED, CONTINUED DESCENT TO 10000, CABIN ALTITUDE REACH 10,500. CABIN ALTITUDE DROPPED BELOW 10,000 AS DESCENT CONTINUED THROUGH 20,000. CABIN STABILIZED AT 8500 FEET WHEN ACFT WAS AT 10,000 FEET. SDR CALA2015041393516Bracket · damagedLEFT INBD FORE FLAP, OTBD AFT FLAP FAIRING, INBD FWD BRACKET HOLES ELONGATED. BRACKET WAS FOUND UNATTACHED & HANGING, FASTENERS MISSING PRESUMABLY DUE TO WORN OR BROKEN. REPAIRED LH INBD FLAP, REAMED ELONGATED HOLES THROUGH MAIN FLAP & SPAR CAP CHORD. FABRISDR CALA2015041393521Frame · corrodedCORROSION AT AFT CARGO COMPARTMENT FRAME AT BS 1460, STRINGER 25R. R & R FRAME AT BS 1460, STRINGER 25R IAW SRM 51-40-02 PAR 7 FIG 12.SDR CALA2015041393522Strap · crackedCABIN FLOORBEAM STABILITY STRAP REPAIR CRACKED AT BS 365.25, LBL 25.5. REPAIRED CABIN FLOORBEAM STABILITY STRAP BS 365.5, LBL 25.5 IAM SRM 53-00-51 REPAIR 13.SDR CALA2015032093447Structure · corrodedRIGHT WING OVERFILL PORT CUT OUT HAS CORROSION. REMOVED CORROSION, INSTALLED .032" FABRICATED FILLER WASHER IAW SRM 57-20-01, REPAIR 6, STEP 4D, 4E, & 4F. ALL NDT & SHOT PEEN ACCOMPLISHED IAW ABOVE SRM, ALL CORROSION REMOVED.SDR CALA2015031793436Slider · defectiveDOOR 4R SLIDE ARMED LIGHT INOPERATIVE. REPLACED FWD GIRT BAR SLIDER IAW 52-11-25.SDR CALA2015031793428Doubler · damagedDOOR 4L HAS DAMAGE TO THE INTERNAL SKIN DOUBLER REPAIR. REMOVED, FABRICATED & INSTALLED NEW REPAIR DOUBLER ON R4 DOOR INNER STRUCTURE IAW ECRA 5210-02405 STEPS 5, 13 & 20 - 31.SDR CALA2015030493185Skin · corrodedAFT CARGO CIRCUMFERENTIAL STRAP & FUSELAGE SKIN CORRODED BS 1400, STRINGER 27L - 28L. REMOVED PREVIOUSLY INSTALLED DOUBLER & CIRCUMFERENTIAL STRAP SPLICE SECTION. FABRICATED & INSTALLED 6 STRAIGHT SHANK FREEZE PLUGS, REPAIR DOUBLER, 146N3810-8200 SKIN SPLICESDR CALA2015030493190Skin · damagedTHIS NON-ROUTINE IS TO CAPTURE FABRICATION OF THE REPAIR DOUBLER AT BS 1393, BL0, IAW COA 50745 & TASK CARD 59745401C, DUE TO THIS REPAIR CAN BE ACCOMPLISHED IAW THE SRM WITHOUT DEVIATION. TRIMMED OUT SKIN & FABRICATED & INSTALLED A REPAIR DOUBLER IAW REO G15SDR CALA2015030493192Frame · dentedAIRCRAFT CARGO FRAME DENTED STATION 1420, STRINGER 27L. CUT OUT DAMAGED AREA OF FRAME INBD FLANGE & FORMED A REPAIR ANGLE IAW SRM 53-00-07 REPAIR 5 & INSTALLED. THIS IS A CAT B REPAIR IN ZONE 3 & REQUIRES SUPPLEMENTAL INSPECTIONS TO BEGIN 12,000 CYCLES AFTERSDR CALA2015030493193Frame · dentedAFT CARGO FRAME DENTED STATION 1540, STRINGER 26L. CUT OUT DAMAGED SECTION OF INBD FLANGE & FORMED REPAIR ANGLE IAW SRM 53-00-07 REPAIR 5. INSTALLED IAW SRM 53-00-07 REPAIR 5 TABLE II. THIS IS A CAT B REPAIR IN ZONE 1 & REQUIRES SUPPLEMENTAL INSPECTIONS BEGSDR CALA2015030493194Frame · bentAFT CARGO FRAME BENT STATION 1400, STRINGER 26L TO 27L. REPAIR DAMAGE FRAME IAW SRM 53-00-07 REPAIR 5 DETAIL I. THIS REPAIR IS A CAT B REPAIR IN ZONE 3. REQUIRES SUPPLEMENTAL INSPECTIONS STARTING IN 12,000 FLIGHT CYCLES & 11,000 FLIGHT CYCLES THEREAFTER THISDR CALA2015030493195Floorbeam · corrodedMAIN CABIN FLOORBEAM CORRODED AT BS 324 BETWEEN RBL 40R - 64R. REMOVED DAMAGED SECTION OF T CAP. FABRICATED & INSTALLED T CAP SPLICE REPAIR ANGLES & STRAPS IAW REO G16382 REV A & SRM 53-10-08 REPAIR 1 IAW ECRA 5310-05795 THIS IS A CAT B REPAIR. THE THRESHOLSDR CALA2015030493197Skin · dentedFUSELAGE DENT 5 FT FWD OF DOOR 2L AT FLOOR LINE. MEASURES .75" X .062" DEEP. DENT IS CRACK FREE & MUST BE REPAIRED BY NEXT C CHECK. THE DENT WAS FOUND OUT OF LIMITS IAW SRM 53-00-03. THE REPAIR AT BS 605 - 618 FUSELAGE BETWEEN STRINGER 15L & 18L HAS BEEN ASDR CALA2015030493198Frame · corrodedAFT PIT BS 1480 FRAME CORRODED BETWEEN STRINGER 26 & 27 RT. REMOVED CORROSION IAW STM 51-10-02 & FOUND IT TO BE OUT OF LIMITS IAW SRM 53-02-07 & SRM 53-30-07. EA 130911 & ECRA 5360-01340 WERE ISSUED TO ADDRESS THE DAMAGE. IAW ECRA 5360-01340, THE BS 1480 BESDR CALA2015030493199Floorbeam · corrodedFORWARD FUSELAGE STATION 324, RBL 59 HAS CORROSION AT FASTENER HOLES. BLENDED THE CORROSION & DETERMINED IT TO BE OUT OF LIMITS IAW SRM 51-10-02. EA 130893 & ECRA 5310-05820 WERE ISSUED TO ADDRESS THE DAMAGE. IAW ECRA 5310-05820 REV A, INSPECTION OF THE BS SDR CALA2015030293183Unknown · malfunctionedLEADING EDGE & TE FLAP DISAGREE AT 20. CREW SELECTED FLAP 30, BUT FLAP WAS STOPPED AT 22, USED ALT TO PUT FLAP AT 20 & DIVERTED. TEST ON FSEU IAW AMM 27-51-01, ALSO DID A VISUAL INSP OF FLAPS, FOUND NO DEFECTS.
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