Boeing 737-2T4
Service difficulty reports · 1,269
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 aircraft_model_key = '7372T4' 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 aircraft_model_key = '7372T4' 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 SPAA2015010500001Power Supply · inoperativeMID CABIN OVERHEAD EMERGENCY LIGHT FAILS TO ILLUMINATE. REPLACED MID CABIN EMERGENCY LIGHT POWER SUPPLY IAW AMM 33-51-01. TESTED SATISFACTORY.SDR SPAA2014112000009Frame · crackedSIDE CHORD CRACKED AR WL 193, BS 178. REPAIRED IAW SB 737-53A1137 AND EO R22529 1-053-013-032.SDR SPAA2014111900007Frame · crackedFRAME WEB CRACK AT BS 639, LBL 50,UNDER FLOOR. REPAIRED OVERWING STUB BEAM WEB IAW EO R22529.1-053-015-032SDR SPAA20141105Stringer · crackedSTRINGER 16L, HAS TWO CRACKS BS 500-520. REPAIRED IAW SB 737-53-1145, REV 0 AND EO R22529 1-053-007-032.SDR SPAA2014111900004Floorbeam · corrodedCORROSION IN THREE PLACES UNDER SREW HOLES AT BS BS 328, RBL 45 TO 60. REPAIRED FLOORBEAM UPPER TEE IAW EO R22529-1-053-010-032, REV NC.SDR SPAA2014111900002Stringer · crackedSTRINGER 16R AT BS 500-520 HAS 2 CRACKS. REPAIRED IAW SB 737-53-1145 AND EO R22529-1-053-011-03.SDR SPAA2014111900008Angle · crackedCRACKED ANGLE AT BS 639, LBL 46, FRAME TO LONGITUDINAL BEAM ATTACHMENT UNDER FLOOR. ANGLE REPLACED IAW SRM 51-10-01, PARA 7, 51-10-02 AND DWG 65C25211, REV B.SDR SPAA2014111900003Stringer · corrodedCORROSION ON AFT PRESSURE BULKHEAD STIFFENER AT GROUND WIRE ATTACH POINT AT STRINGER 12L AT WL220. REMOVED STRINGER, REPAIRED IAW EO R22529-1-053-O32, REV A.SDR SPAA20141101Angle · crackedSTRINGER 15L INTERCOSTAL ANGLE CRACKED AT BS 348. REPAIRED IAW EO R22529-1-053-009-032.SDR SPAA2014111900006Floorbeam · crackedFUSELAGE BS 578, RBL 72, WL 207 FLOORBEAM WEB SUPPORT ANGLE CRACKED AT RIVET HOLE. FLOORBEAM WEB AND SUPPORT ANGLE CRACKS REPAIRED IAW EO R22529 1-053-014-032.SDR SPAA2014112000010Floorbeam · corrodedCORROSION ON UPPER AFT FLANGE OF FLOORBEAM BS 947 , RBL 48. REPAIRED IAW INSTRUCTIONS GIVEN IN EO R22529 1-053-008-032.SDR SPAA2013121600004Battery Pack · inoperativeAFT CABIN EMERGEMCY ESCAPE FLOOR PATH LIGHTING FAILS TO ILLUMINATE. REPLACED EMERGENCY ESCAPE FLOOR PATH LIGHTING AFT EGRESS BATTERY IAW CMM 33-21-27. FUNCTIONALLY TEASTED IAW AMM 33-51-11. ALL FUNCTIONS SATISFACTORY.SDR SPAA2013121600003Charger · inoperativeAFT CABIN EMERGENCY ESCAPE FLOOR PATH LIGHTING FAILS TO ILLUMINATE. REPLACED EMERGENCY ESCAPE FLOOR PATH LIGHTING AFT BATTERY CHARGER ASSY IAW CMM 33-21-27. FUNCTIONALLY TESTED EMERGENCY LIGHTS IAW AMM 33-51-11. ALL FUNCTIONS SATISFACTORY.SDR SPAA2013121600002Charger · inoperativeFWD CABIN EMERGEMCY ESCAPE PATH LIGHTING FAILS TO ILLUMINATE. REPLACED EGRESS BATTTERY CHARGER ASSEMBLY IAW CMM 33-21-27. FUNCTIONALLY TESTED EMERGENCY LIGHTS IAW AMM 33-51-11. ALL FUNCTIONS SATISFACTORY.SDR SPAA2013121600001Battery Pack · inoperativeFWD CABIN EMERGENCY ESCAPE PATH LIGHTING FAILS TO ILLUMINATE. REPLACED EGRESS BATTERY PACK IAW CMM 33-21-27. FUNCTIONALLY TESTED SATIFACTORY IAW AMM 33-51-81.SDR SPAA201311210001Skin · crackedFOUND FUSELAGE SKIN CRACKED AT BS 727A, S25L. REPAIRED IAW EO R22529, 1-053-005-032, REV D AND SR 3-24I97151079.SDR SPAA201311210002Skin · crackedDURING SCHEDULED MAINTNANCE, A SKIN CRACK WAS FOUND AT BS 727A, S15R. REPAIRED IAW SRM 53-30-3, FIG 48, REV 106 AND EO R22529.1-053-004-032, REV A.SDR SPAA1100003Skin · gougedRIGHT WING LOWER SURFACE SKIN, WBL 221; GOUGE. ACCOMPLISHED REWORK/BLEND OUT OF THE GOUGE PER REPAIR PLAN DESCRIBED ON SPA TASK CARD R3R57001. BSF FINDS REPAIR PLAN STRUCTURALLY ACCEPTABLE. BOEING DER ISSUED 8100-9.SDR SPAA1100004Bearing · frozenTUS-CYLW INTO C8 MAINTENANCE CHECK. ON APPROACH AND LANDING INTO CYLW, ELEVATOR CONTROLS STIFF. FOUND ELEVATOR INPUT TORQUE TUBE BEARINGS FROZEN/STIFF TO MOVE. REMOVED TORQUE TUBE ASSY, REPLACED AFFECTED BEARINGS, AND REINSTALLED ASSEMBLY AND RIGGED PER CMSDR SPAA1100002Actuator · crackedDURING TAXI IN, LOST ALL HYDRAULIC SYS "A" PRESSURE,( PIREP). SERVICED A SYS HYD IAW AMM 12-12-00, FOUND NR 4 KRUEGER L/E FLAP ACTUATOR LEAKING AT REAR OF ACTUATOR BODY CASTING. REPLACED ACTUATOR IAW AMM 27-81-31. RII INSP ACCOMPLISHED. SERVICED AIRPLANE HYDSDR SPAA1100001Power Supply · inoperativeFWD CTR CABIN EMERGENCY EXIT LIGHT FAILS TO ILLUMINATE. REPLACED FWD CTR AISLE EXIT LIGHT POWER SUPPLY IAW AMM 33-51-01, OPS CHECKED SATISFACTORY IAW AMM 33-51-11.SDR SPAA1000008Structure · corrodedLT OTBD MIDFLAP THRUST BEARING BORES (2 EA) CORRODED. REPLACED MIDFLAP WITH O/H UNIT IAW AMM.SDR SPAA1000007Structure · corrodedRT WING MIDFLAP HAS CORRODED THRUST BEARING BORES, 2 EA REPLACED MIDFLAP WITH SERVICEABLE UNIT IAW AMM.SDR SPAA090001Light · inoperativeAFT OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY PER AMM 33-51-01. OPERATIONAL CHECK SATISFACTORY.SDR TSAA0832009Valve · leakingNON-ETOPS FLIGHT 88 HNL-KOA, DURING TAKEOFF, THE CREW NOTED THE HYDRAULIC QUANTITY DROP FROM 3 GALLONS TO LESS THAN 1 GALLON. THE CREW ELECTED TO ABORT THE TAKEOFF AT LESS THAN 80 KNOTS INDICATED AIRSPEED. MAINTENANCE FIRST REPLACED A LEAKING O-RING SEAL ON SDR SPAA0700095Power Supply · inoperativeAFT EXIT AND FLOOR PROXIMITY EMERGENCY LIGHTING DOES NOT ILLUMINATE WHEN TURNED ON. REPLACED CHARGER AND BATTERY PACK IAW AMM 33-51-81,SYSTEM OPS TEST NORMAL IAW AMM 33-51-11.SDR SPAA0700094Power Supply · inoperativeAFT EXIT AND FLOOR PROXIMITY EMERGENCY LIGHTING DOES NOT ILLUMINATE WHEN TURNED ON. REPLACED CHARGER AND BATTERY PACK IAW AMM 33-51-81,SYSTEM OPS TEST NORMAL IAW AMM 33-51-11.SDR SPAA0700093Power Supply · inoperativeAFT EXIT AND FLOOR PROXIMITY EMERGENCY LIGHTING DOES NOT ILLUMINATE WHEN TURNED ON. REPLACED CHARGER AND BATTERY PACK IAW AMM 33-51-81,SYSTEM OPS TEST NORMAL IAW AMM 33-51-11.SDR SPAA0700092Power Supply · inoperativeFORWARD SECTION OF FLOORTRACK ESCAPE PATH LIGHTING INOP. REPLACED POWER SUPPLY AND FUNCTIONALLY TESTED SATISFACTORY IAW CMM.SDR SPAA0700091Power Supply · inoperativeAFT SECTION OF FLOORTRACK ESCAPE PATH LIGHTING INOP. REPLACED BATTERY POWER SUPPLY AND FUNCTIONAL CHECK SATISFACTORY IAW CMM 33-21-27.SDR TSAA0631102Lever · lack of lubeON TAKEOFF, THE CREW NOTED THE TAKEOFF CONFIGURATION WARNING ALARM AND PERFORMED A LOW SPEED ABORTED TAKEOFF. CREW RECYCLED THE SPEED BRAKE AND THE ALARM CLEARED. CREW PROCEEDED ON TO LIH WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED A TAKEOFF WARNING TESSDR TSAA0653101Door Frame · damagedAFT CARGO DOOR CUT-OUT DAMAGED (LOWER AFT CORNER). ALOHA ECO 3622 ISSUED.SDR TSAA0663089Skin Panel · crackedA .5 INCH CRACK FOUND LT SIDE OF FUSELAGE SKIN AT BS 270 STRINGER 16L. MAINTENANCE REPAIRED WITH APPROXIMATELY 9"X14" EXTERNAL SKIN PTACH FABRICATED DOUBLER AND TRIPPLER PER ECO 3617. FORM 8100 RECEIVED.SDR TSAA0624080Switch · failedNON-ETOPS FLIGHT 206 HNL OGG. ON TAKEOFF THE CONFIGURATION WARNING ALARM SOUNDED WHEN THROTTLES WERE ADVANCED. CREW ABORTED TAKEOFF AT 15 KTS. AIRCRAFT WAS CONFIGURED PROPERLY FOR TAKEOFF WITH THE SPEED BRAKE DOWN, FLAPS SET TO 5 AND TRIM AT 5.5 UNITS. CRESDR TSAA0653076Bulkhead · cracked3 CRACKED HOLES COMMON TO BS 178 BULKHEAD WEB BETWEEN WL 240 AND WL 230.5SDR TSAA0653068Door Frame · crackedCRACK NOTED ON FWD CARGO DOOR CUTOUT, AFT LOWER CORNER UNDER DOOR STOP.SDR TSAA0678059Warning Light · illuminatedNON-ETOPS FLT 224 LIH-HNL. ON TAKE OF ROLL, CREW NOTED THE NR 2 ENGINE THRUST REVERSER UNLOCKED LIGHT ON WITH ALL OTHER ENGINE INDICATIONS NORMAL. CREW ABORTED TAKEOFF AT 60 KTS AND TAXIED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE OPENED AND INSPECTSDR TSAA0678054Latch · lack of lubeON TAKEOFF ABOVE 80 KNOTS AND CLIMB, CREW NOTED NR 2 THRUST REVERSER UNLOCKED LIGHT ILLUMINATED INTERMITTENTLY. CREW RETURNED TO HNL WITHOUT FURTHER INCIDENT. MAINTENANCE DEFERRED PER MEL 78-2 AND RELEASED THE AIRCRAFT FOR SERVICE. ON 7/16/06 MAINTENANCE CLSDR TSAA0653046Skin Panel · cracked2.25 INCH SKIN CRACK FOUND LEFT SIDE OF FUSELAGE BS 786 JUST ABOVE STRINGER 24L. MAINTENANCE REPAIRED WITH APPROXIMATELY 11 IN X 15 IN EXTERNAL SKIN PATCH, FABRICATED DOUBLER AND TRIPLER PER SRM 53-30-3, PROCEDURE VII, DETAIL VII.SDR TSAA0653045Skin Panel · cracked2.5 INCH SKIN CRACK FOUND RIGHT SIDE OF FUSELAGE AT BS 941 JUST ABOVE STRINGER 24R. MAINTENANCE REMOVED TWO EXISTING REPAIRS AND REPAIRED WITH 36 IN X 46 IN EXTERNAL SKIN PATCH, FABRICATED FILLERS, DOUBLER, AND TRIPLER PER SRM 53-30-3, PROCEDURE VII, DETAIL XSDR TSAA0653042Skin Panel · cracked3 INCH CRACK FOUND RT SIDE OF FUSELAGE SKIN AFT OF AFT CARGO DOOR CUTOUT AS BS 867 STRINGER 23R. MAINTENANCE REMOVED ONE EXISTING REPAIR AND REPAIRED WITH APPROXIMATELY 19-1/2 IN X 19-1/2 IN EXTERNAL SKIN PATCH, FABRICATED DOUBLER AND TRIPLER PER SRM 53-30-3,SDR TSAA0653030Bulkhead · crackedTHREE CRACKS AROUND BS 1016 AFT PRESSURE BULKHEAD GORE WEBS NEAR DOME CAP. WEB SPLICE AND REPAIR DOUBLERS COMPLETED IAW ALOHA'S ECO 3567. HFEC COMPLIED IAW NDT MANUAL PART 5, 51-00-00 FIG 16. FAA FORM 8100-9 RECEIVED.SDR TSAA0653028Skin · crackedAPPROXIMATE 2 INCH SKIN CRACK AT BS 747 +10 STR 24L. REPAIR COMPLETED IAW SRM 53-30-3 FIG 48. REPAIR SIZE APPROX 15 X 11 INCHES. INSURANCE CUT MADE .040 INCH. DOUBLER .032 2024T3; TRIPLER .050 2024T3. HFEC HOLE LAY-OUT IAW NDT MANUAL 51-00-00 PT 6.SDR TSAA0627026Indication Sys · malfunctionedON APPROACH TO KOA, CREW NOTED TRAILING EDGE FLAP INDICATOR SHOWING LEFT SIDE AT 4 DEGREES AND RIGHT SIDE AT 7 DEGREES WITH 5 DEGREES OF FLAPS SELECTED. CREW UNABLE TO EXTEND FLAPS TO 15. CREW DECIDED TO RETURN TO HNL AND DECLARED AN EMERGENCY. WITH ALTERNASDR TSAA0627016Slat · bird strikeON CLIMB AT 1000 FT AIRCRAFT STRUCK A LARGE BIRD AT NR 1 LEADING EDGE SLAT. THE CREW RETURNED TO HNL WITHOUT FURTHER INCIDENT. MAINTENANCE COMPLIED WITH FORM M-106 BIRD STRIKE INSPECTION AND FOUND A LARGE DENT APPROXIMATELY 1.5 INCH WIDE ON THE OUTBOARD LEADSDR TSAA0653010Skin · crackedFOUND 3 CRACKS AROUND CENTER UPSTOP OF NR 2 SLAT; WING LEADING EDGE. BETWEEN LEFT WS 453 AND WS 479. L/E SKIN FABRICATED, TRIMMED, CLEANED, ALODINED, PRIMED, AND SEALED IAW SRM 57-30-04. REPAIR SIZE APPROX 14" BY 25".SDR TSAA0672008Engine · defectiveOGG-HNL: ON TAKEOFF NR 2 ENGINE EGT ROSE TO 650 DEGREES CELSIUS. ENGINE THROTTLED BACK UNTIL EGT WAS WITHIN LIMITS AND AIRCRAFT RETURNED TO FIELD WITHOUT INCIDENT. REMOVED AND REPLACED NR 2 ENGINE IAW FORM M-211, M-212, M-213, AND M-215. NO FAULTS NOTED. ASDR TSAA0652004Skin · crackedA 4.25 INCH SKIN CRACK ON AFT CARGO DOOR. CRACK LOCATED 18.5 INCHES FROM LOWER FWD CORNER AND 5 INCHES FROM FWD CUTOUT. MAINTENANCE REPAIRED WITH APPROXIMATELY 10 X 7 INCH EXTERNAL SKIN PATCH, FABRICATED DOUBLER (0502024-T3). REPAIR COMPLETED IAW ECO 3550.SDR SPAA0500082Battery Pack · intermittentCENTER OVERHEAD EMERGENCY EXIT LIGHT STAYS ON ONLY BRIEFLY. REPLACED CENTER OVERHEAD EMERGENCY EXIT LIGHT BATTERY CHARGER IAW MM 33-51-81. GROUND CHECK NORMAL IAW MM 33-51-11.SDR SPAA0500081Structure · crackedCRACK ON BS1156 OUTER CHORD RT SIDE WL270. REPAIRED CRACK IAW SB 737-53-1086.
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