# Service difficulty reports: N457TM, cancelled Nov 8, 2013 A list on [N457TM, cancelled Nov 8, 2013](https://openairdocs.org/deregistered/N457TM-2013-11-08.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 2 · 88 reports - [SDR BJNA020401](https://openairdocs.org/sdr/BJNA020401.md): Battery · discharged · Apr 5, 2002 · N457TM · Boeing 737214 · Emergency Lighting > EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED ALL DEPLETED BATTERIES APPLICABLE PER BMM 33-51-51 AND 33-51-101. REPLACED L-1 LIGHT ASSEMBLY PER BMM 33-51-101. REPLACED AFT AISLE LIGHT BATTERY PER BMM 33-51-71. TESTS NORMAL. (M) - [SDR BJNA020105](https://openairdocs.org/sdr/BJNA020105.md): Power Supply · discharged · Jan 31, 2002 · N457TM · Boeing 737214 · Emergency Lighting > EMERGENCY EXIT LIGHTS FROM ROW 15 AFT INOPERATIVE, ALSO FLOOR LEVEL EXIT LIGHTS FOR BOTH AFT EXIT DOORS. REPLACED BATTERY POWER SUPPLY UNDER SEAT ROW 16 ABC IAW BMM 33-51-11. (M) - [SDR BJNA011202](https://openairdocs.org/sdr/BJNA011202.md): Circuit Breaker · failed · Dec 6, 2001 · N457TM · Boeing 737214 · Landing Gear Position and Warning > GEAR DOWN LIGHTS FAILED. THE PILOT NOTICED HE DID NOT HAVE A LANDING GEAR DOWN INDICATION (3 GREEN LIGHTS) LANDING GEAR CHECK LIST HAD BEEN COMPLETED. WITH NO INDICATIONS THE TOWER WAS NOTIFIED THE PILOT ELECTED TO DO A GO AROUND AND ASK THE TOWER TO VERIFY - [SDR BJN2001F00003](https://openairdocs.org/sdr/BJN2001F00003.md): Hydraulic Line · chafed · Nov 27, 2001 · N457TM · Boeing 737214 · Hydraulic System, Main > DURING DESCENT NOTICED A SYS HYDRAULIC QUANTITY LEVEL DROPPING. A SYS LOW PRESSURE LIGHT ILLUMINATED. CONFIGURED AC FOR A SYS HYDRAULIC FAILURE CONTINUED FLIGHT WITH B SYS. APPROX 5 MINUTES LATER, LOW PRESSURE WARNING ILLUMINATED ON BOTH B SYS LOW PRESSURE - [SDR BJN2001F00002](https://openairdocs.org/sdr/BJN2001F00002.md): Hydraulic System · failed · Nov 27, 2001 · N457TM · Boeing 737214 · Hydraulic System, Main > DURING DESCENT NOTICED A SYSTEM HYDRAULIC QUANTITY LEVEL DROPPING. A SYSTEM LOW PRESSURE LIGHT ILLUMINATED. CONFIGURED AC FOR A SYSTEM HYDRAULIC FAILURE CONTINUED FLIGHT WITH B SYSTEM. APPROX 5 MINUTES LATER, LOW PRESSURE WARNING ILLUMINATED ON BOTH B SYST - [SDR BJNA011101](https://openairdocs.org/sdr/BJNA011101.md): Battery Pack · defective · Nov 9, 2001 · N457TM · Boeing 737214 · Emergency Lighting > RIGHT OVERWING EMERGENCY LIGHT BATTERY PACK CAUSES AN ELECTRIC DRAIN ON BATTERY WITH EMERGENCY LIGHT SWITCH OFF. REMOVED AND REPLACED BATTERY PACK PER BMM 33-51-33. OPS CHECK NORMAL. (M) - [SDR BJNA011002](https://openairdocs.org/sdr/BJNA011002.md): Light · inoperative · Oct 26, 2001 · N457TM · Boeing 737214 · Emergency Lighting > R-3 OVERHEAD EMERGENCY EXIT LIGHT WILL NOT TEST. REMOVED AND REPLACED R-3 EMERGENCY EXIT LIGHT IAW BMM 33-51-51. (M) - [SDR BJNA011003](https://openairdocs.org/sdr/BJNA011003.md): Light · inoperative · Oct 26, 2001 · N457TM · Boeing 737214 · Emergency Lighting > FOUND COCKPIT EMERGENCY LIGHT WOULD NOT TEST. REMOVE AND REPLACED EMERGENCY EXIT LIGHT IAW 33-51-51 OF BMM, OPS CHECK NORMAL. (M) - [SDR BJNA010901](https://openairdocs.org/sdr/BJNA010901.md): Connector · dirty · Sep 21, 2001 · N457TM · Boeing 737214 · Flight Control System Wiring > WING FLAP POSITION INDICATOR SHOWED FLAPS NOT RETRACTED THE LAST 5 DEGREES IN FLIGHT. FUNCTIONAL TEST OF FLAP RETRACTION AND EXTENSION SYSTEM BY MAINTENANCE OK. REMOVED FLAP POSITION INDICATOR TRANSMITTER ELECTRICAL CONNECTOR, CLEANED, INSPECTED AND RECONNEC - [SDR BJNA0101603](https://openairdocs.org/sdr/BJNA0101603.md): Hydraulic Line · Jun 18, 2001 · N457TM · Boeing 737214 · Hydraulic Power System > TOTAL HYDRAULIC FAILURE, FIRST NR 1 'A' SYSTEM PRESSURE LIGHT CAME ON, 'A' SYSTEM QUANTITY WENT TO ZERO. APPROXIMATELY 2 MINUTES LATER 'B' SYSTEM LOW QUANTITY LIGHT CAME ON. DIVERTED INTO SALT LAKE CITY, UT. INSPECTION FOUND BROKEN 'A' SYSTEM PRESSURE LINE - [SDR BJNA010602](https://openairdocs.org/sdr/BJNA010602.md): Battery Pack · discharged · Jun 15, 2001 · N457TM · Boeing 737214 · Emergency Lighting > FOUND LEFT FORWARD ACCESS DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK PER BMM 33-51-71, OPS CHECK NORMAL. (M) - [SDR BJNA010601](https://openairdocs.org/sdr/BJNA010601.md): Battery Pack · discharged · Jun 15, 2001 · N457TM · Boeing 737214 · Emergency Lighting > RIGHT FORWARD ACCESS DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK PER BMM 33-51-71, OPS CHECK NORMAL. (M) - [SDR BJNA010507](https://openairdocs.org/sdr/BJNA010507.md): Hydraulic Line · May 27, 2001 · N457TM · Boeing 737214 · Flight Control System > LOST BOTH A/B HYDRAULIC SYSTEM PRESSURE. INSPECTED A/C FOUND NR 1 ENGINE 'A' SYSTEM HYDRAULIC LINE FAILURE AT PRESSURE MODULE. A/C IS SAFE FOR ITS INTENDED FERRY FLIGHT WITH THE NR 1 ENGINE 'A' PUMP IN THE OFF POSITION. INSTALLED APPROVED RATED TEMPORARY FL - [SDR BJNA010502](https://openairdocs.org/sdr/BJNA010502.md): Light · inoperative · May 3, 2001 · N457TM · Boeing 737214 · Emergency Lighting > ROW 5 SEAT EMERGENCY LIGHT INOPERATIVE. RESEATED LAMP IN SOCKET, OPS CHECK NORMAL. (M) - [SDR BJNA010501](https://openairdocs.org/sdr/BJNA010501.md): Light · inoperative · May 3, 2001 · N457TM · Boeing 737214 · Emergency Lighting > L1 EMERGENCY EXIT OVER DOOR LIGHT INOPERATIVE. RELAMPED PER BMM 33-51-101, OPS CHECK NORMAL. (M) - [SDR BJNA010401](https://openairdocs.org/sdr/BJNA010401.md): Light · inoperative · Apr 13, 2001 · N457TM · Boeing 737214 · Emergency Lighting > FOUND RIGHT LOWER EXTERIOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEMBLY PER BMM 33-51-21. OPS CHECK NORMAL. (M) - [SDR BJNA010305](https://openairdocs.org/sdr/BJNA010305.md): Battery · inoperative · Mar 28, 2001 · N457TM · Boeing 737214 · Emergency Lighting > FOUND LEFT ROW 1 THROUGH 6 SEATS, INOPERTIVE EMERGENCY EXIT LIGHTS. REMOVED AND REPLACED BATTERY POWER SUPPLY UNIT PER BMM 33-51-11, OPS CHECK NORMAL. (M) - [SDR BJNA010304](https://openairdocs.org/sdr/BJNA010304.md): Light · inoperative · Mar 26, 2001 · N457TM · Boeing 737214 · Emergency Lighting > FOUND ROW 12 AISLE EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT AT ROW 12 AISLE, OPS CHECK NORMAL IAW BMM 33-51-11. (M) - [SDR BJNA010205](https://openairdocs.org/sdr/BJNA010205.md): Strut · leaking · Feb 21, 2001 · N457TM · Boeing 737214 · Nose/Tail Landing Gear Strut/Axle > NOSE LANDING GEAR SHOCK STRUT LEAKING. REMOVED AND REPLACED NOSE LANDING GEAR STRUT ASSEMBLY PER B737 MM 32-21-0. (M) - [SDR BJNA010101](https://openairdocs.org/sdr/BJNA010101.md): Light · loose · Jan 3, 2001 · N457TM · Boeing 737214 · Emergency Lighting > FOUND SEAT 21B EMERGENCY EXIT AISLE LIGHT LOOSE FROM SEAT. REATTACHED EMERGENCY EXIT LIGHT. OPS CHECK GOOD IAW BMM 33-51-11B. (M) - [SDR BJNA001205](https://openairdocs.org/sdr/BJNA001205.md): Light · loose · Dec 29, 2000 · N457TM · Boeing 737214 · Emergency Lighting > SEAT 21 EMERGENCY LIGHT ASSEMBLY IS LOOSE FROM MOUNT. RE-ATTACHED LIGHT ASSEMBLY. - [SDR BJNA001204](https://openairdocs.org/sdr/BJNA001204.md): Hydraulic Line · chafed · Dec 27, 2000 · N457TM · Boeing 737214 · Hydraulic System, Main > AT 31,000FT THE, B, LOW QUANTITY LIGHT ILLUMINATED IN FLIGHT, SYSTEM QUANTITY SHOWED 1.25 GALLONS, PILOT PERFORMED THE QRH FOR LOSS OF, B, SYSTEM HYDRAULICS, AND DIVERTED TO CEDAR RAPIDS IOWA.FOUND PRESSURE LINE NR6 SPOILER CHAFFED THRU, REPLACED HARD LINE WIT - [SDR BJNA001202](https://openairdocs.org/sdr/BJNA001202.md): Light · inoperative · Dec 8, 2000 · N457TM · Boeing 737214 · Emergency Lighting > FORWARD OVERHEAD CENTER EMERGENCY LIGHT ASSEMBLY. REMOVED AND REPLACED LIGHT ASSEMBLY. - [SDR BJNA000702](https://openairdocs.org/sdr/BJNA000702.md): Seal · broken · Jul 18, 2000 · N457TM · Boeing 737214 · Hydraulic Pump (Electric/Engine), Main > NR 1 HYDRAULIC LOW PRESSURE LIGHT ILLUMINATED IN FLIGHT. SYSTEM QUANTITY SHOWED 1-3 GALLONS. REMOVED AND REPLACED NR 1 HYDRAULIC PUMP, IAW BMM 29-11-31. OPS CHECK AND LEAK CHECK GOOD, IAW BMM 29-11-31. (M) - [SDR BJNA000503](https://openairdocs.org/sdr/BJNA000503.md): Adc · inoperative · May 14, 2000 · N457TM · Boeing 737214 · Air Data Computer > MODE C, 1 AND 2 INOPERATIVE BY 3,000 TO 4,000 FEET. RETURNED TO POINT OF ORIGIN. REMOVED AND REPLACED ADC, OPS CHECK GOOD, IAW BMM 34-12-11. (M) - [SDR BJNA000412](https://openairdocs.org/sdr/BJNA000412.md): Light · inoperative · Apr 22, 2000 · N457TM · Boeing 737214 · Emergency Lighting > R2 DOOR EMERGENCY EXIT OVER DOOR LAMP INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT ASSEMBLY IAW 33-51-101. (M) - [SDR BJNA000402](https://openairdocs.org/sdr/BJNA000402.md): Engine · malfunctioned · Apr 7, 2000 · N457TM · Boeing 737214 · Engine (Turbine/Turboprop) > DURING FLIGHT FROM COS PILOT NOTICED ENGINE OIL LEVEL GETTING LOW. OIL LEVEL CONTINUED TO DECREASE AND LOW LEVEL LIGHT STARTED TO ILLUMINATE. PILOT DECIDED TO SHUTDOWN NR 1 ENGINE 15 MINUTES OUT OF LAS. PILOT DECLARED EMERGENCY, AND LANDED SAFELY AT LAS. P - [SDR BJNA000403](https://openairdocs.org/sdr/BJNA000403.md): Skin · cracked · Apr 4, 2000 · N457TM · Boeing 737214 · Fuselage Main, Plate/Skin > ON WALK AROUND, FOUND CRACKS ABOVE FORWARD WING TO BODY FAIRING AFT OF WING ILLUMINATION LIGHT OF LEFT WING IN FUSELAGE. REMOVED PAINT NDT VERIFIED 8 EACH CRACKS AT 8 RIVETS. REMOVED DAMAGE AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 53-30-3. (M) - [SDR BJNA000302](https://openairdocs.org/sdr/BJNA000302.md): Bulb · failed · Mar 29, 2000 · N457TM · Boeing 737214 · Emergency Lighting > TWO NON ADJACENT AISLE LIGHTING FIXTURES INOPERATIVE. AIRCRAFT RELEASED PER MEL 33-19, DMI NR 0321 ITEM TRANSFER TO DMI LOG NR 518687394. REMOVED AND REPLACED EMERGENCY LIGHT FIXTURE BULBS. OPS CHECK GOOD IAW BMM 33-51-11. (M) - [SDR BJNA000102](https://openairdocs.org/sdr/BJNA000102.md): Blade · damaged · Jan 27, 2000 · N457TM · Boeing 737214 · Turbine Engine Compressor Section > NR 2 ENGINE FLAMED OUT ON TAKEOFF ROLL. INSPECTION OF ENGINE DETERMINE CAUSE TO BE INGESTION OF FOD, DAMAGING C-1, C-7, C-8 AND C-9 COMPRESSOR BLADES. (M) - [SDR BJNA981101](https://openairdocs.org/sdr/BJNA981101.md): Line · failed · Nov 15, 1998 · N457TM · Boeing 737214 · Hydraulic System, Main > 'A' SYSTEM HYDRAULIC FAILED, LACK OF HYDRAULIC PRESSURE. REPLACED HYDRAULIC LINE LEFT WING T/E, PERFORMED LEAK CHECK OF BOTH ENGINES AND IN WHEEL WELL, NO LEAKS FOUND. REPLACED NR 1 AND NR 2 ENGINE DRIVEN HYDRAULIC PUMP DUE TO CAVITATION. (M) - [SDR BJNA981003](https://openairdocs.org/sdr/BJNA981003.md): Panel · delaminated · Oct 24, 1998 · N457TM · Boeing 737214 · Horizontal Stabilizer, Plate/Skin > UPON (PHASE 9) INSPECTION DISCOVERED RIGHT HORIZONTAL STABILIZER UPPER TRAILING EDGE PANEL DELAMINATING. REPAIRED HORIZONTAL 1E PANEL WORK ORDER 02-0001, AND 02-0002, JOB NR 10-1166, WORK PERFORMED BY EVERGREEN AIR CENTER. (M) - [SDR BJNA981002](https://openairdocs.org/sdr/BJNA981002.md): Light · inoperative · Oct 23, 1998 · N457TM · Boeing 737214 · Passenger Compartment Lighting > EMERGENCY LIGHT ON PASSENGER SEAT 10C IS BROKEN. REMOVED AND REPLACED EXIT SIGN LIGHT ASSY PER BMM 33-51-11. (M) - [SDR BJNA981001](https://openairdocs.org/sdr/BJNA981001.md): Battery Pack · discharged · Oct 6, 1998 · N457TM · Boeing 737214 · Emergency Lighting > RIGHT FORWARD SERVICE DOOR SLIDE EMERGENCY LIGHT INOP. REPLACED BATTERY PACK ON RIGHT ENTRY DOOR PER BMM 33-51-71. (M) - [SDR BJNA980901](https://openairdocs.org/sdr/BJNA980901.md): Light · inoperative · Sep 19, 1998 · N457TM · Boeing 737214 · Emergency Lighting > EMERGENCY EXIT LIGHT ABOVE L-2 DOOR INOP. REPLACED EMERGENCY LIGHT ASSY IAW BMM 33-51-101, GROUND CHECKS NORMAL. (M) - [SDR BJNA980701](https://openairdocs.org/sdr/BJNA980701.md): Sensor · malfunctioned · Jul 7, 1998 · N457TM · Boeing 737214 · Overheat Detection > LEFT WING BODY OVERHEAT LIGHT ILLUMINATED. AIRCRAFT RELEASED PER MEL 26-12, DMI 701, ITEM TRANSFERRED TO DMI LOG AND PLACARDED. REF: DMI 701, REMOVED AND REPLACED OVERHEAT LOOP IN APU COMPARTMENT IAW 26-18. OPS CHECKS NORMAL. (LOG PAGE 10721). (X) - [SDR BJNA980604](https://openairdocs.org/sdr/BJNA980604.md): Insulator · mislocated · Jun 28, 1998 · N457TM · Boeing 737214 · Overheat Detection > ON GROUND LEFT WING BODY OVERHEAT ILLUMINATED. IN THE APU COMPARTMENT, THE OVERHEAT LOOP ELEMENT IS POSITIONED A FEW INCHES ABOVE THE BLEED AIR SUPPLY DUCT. THIS ELEMENT IS HELD IN POSITION BY NUMEROUS CLAMPS WITH INSULATORS DURING TROUBLESHOOTING, AN INSULA - [SDR BJNA980603](https://openairdocs.org/sdr/BJNA980603.md): Detector · out of position · Jun 26, 1998 · N457TM · Boeing 737214 · Overheat Detection > NR 1 WING BODY OVERHEAT ILLUMINATED INTERMITTENTLY AFTER TAKEOFF AT BFF WITH BLEEDS OFF, APU ON TAKEOFF, REMAINED OFF AFTER BLEEDS RECONFIGURED. DISCOVERED OVERHEAT DETECTOR AGAINST APU BLEED SUPPLY DUCT, RELOCATED AND RAN APU AT MAX TEMP FOR 40 MIN, NO DISCR - [SDR BJNA980506](https://openairdocs.org/sdr/BJNA980506.md): Overheat Light · illuminated · May 28, 1998 · N457TM · Boeing 737214 · Overheat Detection > LEFT WING BODY OVERHEAT LIGHT ILLUMINATED DURING THE DESCENT INTO KEKO. AIRCRAFT RELEASED PER MEL 26-12, DMI 10508, ITEM PLACARDED AND TRANSFERRED TO DMI LOG. (M) - [SDR BJNA980505](https://openairdocs.org/sdr/BJNA980505.md): Fire Detector · malfunctioned · May 27, 1998 · N457TM · Boeing 737214 · Fire Detection > LEFT WING BODY OVERHEAT ILLUMINATES, QRH PROCEDURE, LIGHT WENT OUT THEN CONTINUED FLICKERING DURING DESCENT. CHECKED ALL LOOPS WITH OHM METER AND MAGER, FOUND NO PROBLEM CHANGED FIRE DETECT ASSY UNIT TEST FLEW AIRCRAFT COULD NOT DUPLICATE PROBLEM. (M) - [SDR BJNA980504](https://openairdocs.org/sdr/BJNA980504.md): Clamp · loose · May 27, 1998 · N457TM · Boeing 737214 · Pneumatic Distribution System > LEFT WING BODY OVERHEAT LIGHT ILLUMINATED, FOLLOWED QRH PROCEDURE AND AFTER A FEW MOMENTS THE OVERHEAT LIGHT WENT OUT. RETORQUED CLAMP ON INBOARD END OF AIR CLEANER AT FORWARD END OF LEFT A/C BAY PER BMM 36-19-11, GRUOND CHECKS NORMAL. (M) - [SDR BJNA980503](https://openairdocs.org/sdr/BJNA980503.md): Connector · dirty · May 26, 1998 · N457TM · Boeing 737214 · Overheat Detection > LEFT WING BODY OVERHEAT ILLUMINATES INTERMITTENTLY. CLEANED CONNECTORS ON FORWARD AND AFT KEEL BEAM SENSOR, OPS CHECK NORMAL. OK FOR SERVICE. (M) - [SDR BJNA980502](https://openairdocs.org/sdr/BJNA980502.md): Connector · dirty · May 25, 1998 · N457TM · Boeing 737214 · Overheat Detection > LEFT WING BODY OVERHEAT LIGHT CAME ON DURING DESCENT. CLEANED CONNECTORS OF SENSING ELEMENT ON LEFT ENGINE STRUT CAVITY TESTED WING AND LOWER AFT BODY OVERHEAT DETECTION SYSTEM PER BMM 26-18-0, PAGE 501, TO 502, TEST OK. (M) - [SDR BJNA980501](https://openairdocs.org/sdr/BJNA980501.md): Overheat Light · illuminated · May 24, 1998 · N457TM · Boeing 737214 · Overheat Detection > LEFT WING BODY OVERHEAT LIGHT CAME ON EN ROUTE. REMOVED AND REPLACED COMP OVERHEAT UNIT PER BMM 26-17-0, OPS TEST PERFORMED PER BMM 26-18-0, TEST OK. (M) - [SDR BJNA9803007](https://openairdocs.org/sdr/BJNA9803007.md): Connector · failed · Apr 28, 1998 · N457TM · Boeing 737214 · Overheat Detection > ENGINE OVERHEAT LIGHT FLICKERED ON AND OFF. REMOVED AND REPLACED CONNECTOR PER BSWM 20-67-14, OPS CHECK NORMAL PER BMM 26-11-0. (M) - [SDR BJNA9803006](https://openairdocs.org/sdr/BJNA9803006.md): Fire Loop · chafed · Apr 7, 1998 · N457TM · Boeing 737214 · Overheat Detection > LEFT ENGINE OVERHEAT LIGHT COMES ON INTERMITTENTLY. DISCOVERED CHAFED WIRES ON FIRE LOOP CONNECTORS, LT ENGINE, AFT. REMOVED AND REPLACED CONNECTORS PER BSWPM 20-62-16, OPS CHECKS NORMAL. (X) - [SDR BJNA9800303](https://openairdocs.org/sdr/BJNA9800303.md): Connectors · dirty · Apr 7, 1998 · N457TM · Boeing 737214 · Smoke Detection > NR 1 ENGINE OVERHEAT LIGHT ON. CLEANED OVERHEAT LOOP CONNECTORS, REPLACED COPPER GASKETS. OPS CHECKED OK, IAW BMM 26-10-00. (M) - [SDR BJNA9803005](https://openairdocs.org/sdr/BJNA9803005.md): Control Module · defective · Apr 6, 1998 · N457TM · Boeing 737214 · Fire Detection > NR 1 ENGINE OVERHEAT LIGHT ILLUMINATED IN-FLIGHT INTERMITTENTLY. REMOVED AND REPLACED ENGINE AND APU FIRE CONTROL MODULE, RAN ENGINE, NO LEAKS FOUND. CHECKED WIRING, ALL OK. REF MM 26-21-41, AND 26-21-0. (X) - [SDR BJNA9803004](https://openairdocs.org/sdr/BJNA9803004.md): Fire Detector · defective · Apr 3, 1998 · N457TM · Boeing 737214 · Fire Detection > LEFT ENGINE OVERHEAT LIGHT ILLUMINATES INTERMITTENTLY. REMOVED AND REPLACED FIRE DETECTION ACCESSORY UNIT PER bMM20-10-111, GROUND TEST NORMAL PER BMM 26-11-0. (EKO) (X). - [SDR BJNA9800302](https://openairdocs.org/sdr/BJNA9800302.md): Connector · dirty · Apr 2, 1998 · N457TM · Boeing 737214 · Overheat Detection > SLT - NR 1 ENGINE OVERHEAT LIGHT IS ON INTERMITTENT IN FLIGHT, ON 100 PERCENT ON GROUND. AIRCRAFT RELEASED PER MEL 26-2, DMI 0402, PER PLACARD INSTALLED. CLEANED OIL FROM CONNECTORS ON NR 1 ENGINE PER BMM 26-11-0. TESTS NORMAL PER BMM 26-11-0. (M) Next page: https://openairdocs.org/deregistered/N457TM-2013-11-08/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 = 'N457TM' AND deregistration_id = 'N457TM-2013-11-08' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N457TM-2013-11-08/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.