# Service difficulty reports: N136DL, cancelled Jan 24, 2018 A list on [N136DL, cancelled Jan 24, 2018](https://openairdocs.org/deregistered/N136DL-2018-01-24.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 · 59 reports - [SDR DALA2016080805979](https://openairdocs.org/sdr/DALA2016080805979.md): Light · inoperative · Jul 31, 2016 · N136DL · Boeing 767332 · Emergency Lighting > EMERGENCY LIGHT ABOVE COCKPIT DOOR FOUND INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY AND BATTERIES. SYSTEM OPS NORMAL. - [SDR DALA2016021801360](https://openairdocs.org/sdr/DALA2016021801360.md): Light · unsecure · Feb 13, 2016 · N136DL · Boeing 767332 · Emergency Lighting > EMERGENCY LIGHT AT SEAT 17AB ARE HANGING. SECURED THE LIGHTS. SYS OPERATION IS NORMAL. - [SDR DALA2016020701133](https://openairdocs.org/sdr/DALA2016020701133.md): Skin · cracked · Feb 6, 2016 · N136DL · Boeing 767332 · Fuselage Main, Plate/Skin > UPPER FASTENER HOLE CRACKED IN SKIN UNDER FAIL-SAFE. - [SDR DALA2016020601128](https://openairdocs.org/sdr/DALA2016020601128.md): Failsafe · cracked · Feb 5, 2016 · N136DL · Boeing 767332 · Fuselage Internal Mounting Structure > DURING CHECK, FOUND RT FAILSAFE CRACKED. REPAIRED RT FAILSAFE IAW ERA 543034-14AD. - [SDR DALA2014102705834](https://openairdocs.org/sdr/DALA2014102705834.md): Shroud · failed · Oct 24, 2014 · N136DL · Boeing 767332 · Emergency Lighting > EMERGENCY FLOOR LIGHTING INOPERATIVE AT 46A. MAINTENANCE REPLACED EMERGENCY LIGHT SHROUD AT 46 A/B. SYS OPS IS NORMAL. - [SDR DALA2014081904604](https://openairdocs.org/sdr/DALA2014081904604.md): Light · inoperative · Aug 13, 2014 · N136DL · Boeing 767332 · Emergency Lighting > EMERGENCY LIGHT INOPERATIVE AT 19B. MAINTENANCE INSTALLED A NEW EMERGENCY LIGHT ASSEMBLY.. - [SDR DALA1400500136](https://openairdocs.org/sdr/DALA1400500136.md): Skin · cracked · Feb 6, 2014 · N136DL · Boeing 767332 · Fuselage Main, Plate/Skin > BS 1725 S7R SKIN CRACKED, REPAIRED IAW ERA 522378-14AD. - [SDR DALA14007560136](https://openairdocs.org/sdr/DALA14007560136.md): Skin · corroded · Feb 4, 2014 · N136DL · Boeing 767332 · Fuselage Main, Plate/Skin > INSPECTION FOUND CORROSION AT UPPER CENTER WING SKIN PANEL RT SIDE, RBL 97 AND BETWEEN BS 933 AND 955. REPAIRED IAW ERA 522253-14. - [SDR DALA14007550136](https://openairdocs.org/sdr/DALA14007550136.md): Floor Support · corroded · Feb 4, 2014 · N136DL · Boeing 767332 · Fuselage Miscellaneous Structure > RT AFT LAVATORY OTBD FLOOR SUPPORT CORRODED AT ZEE ANGLE RADIUS FOR R2 DOOR THRESHOLD, BS 1483. - [SDR DALA14007540136](https://openairdocs.org/sdr/DALA14007540136.md): Stringer · damaged · Feb 4, 2014 · N136DL · Boeing 767332 · Fuselage Main, Longeron/Stringer > STRINGER 7 END TIE FITTING DAMAGED. REPAIRED IAW ERA 522-483-14. - [SDR DALA13067420136](https://openairdocs.org/sdr/DALA13067420136.md): Wire · broken · Dec 4, 2013 · N136DL · Boeing 767332 · Light System Wiring > ROW 4AB AFT EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE AT CONNECTOR. OPS NORMAL. - [SDR DALA13067410136](https://openairdocs.org/sdr/DALA13067410136.md): Wire · broken · Dec 4, 2013 · N136DL · Boeing 767332 · Light System Wiring > ROW 35GF EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE. OPS CHECKED NORMAL. - [SDR DALA1149170136](https://openairdocs.org/sdr/DALA1149170136.md): Wire · broken · Aug 21, 2011 · N136DL · Boeing 767332 · Light System Wiring > EMERGENCY OVERHEAD PROXY LIGHTS AT ROW 4 AND 17 ARE INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE AT ROW 4 AND SEAT 17A. SYSTEM OPERATION IS NORMAL. - [SDR DALA1119280136](https://openairdocs.org/sdr/DALA1119280136.md): Rib · cracked · Mar 7, 2011 · N136DL · Boeing 767332 · Turbine Engine Compressor Section > NR 1 ENGINE AFT FAN ASSY / AFT FAN CASE FWD RIB CRACKED AT 12 O'CLOCK POSITION DURING INSTALLATION. NR 1 ENGINE AFT FAN CASE CRACKED FWD T RIB REPAIRED IAW ER/A 488809-14 REV ORIGINAL. - [SDR DALA1118840136](https://openairdocs.org/sdr/DALA1118840136.md): Fitting · damaged · Feb 23, 2011 · N136DL · Boeing 767332 · Nacelle/Pylon, Frame/Spar/Rib > NR 1 PYLON O/B MID SPAR FTF BOTH I/B AND O/B HOLES DIAMETER FOUND GREATER THAN 0.875"-0.877" DURING ACCOMPLISHMENT OF EA 01-074904-03AD REV D. NR 1 PYLON O/B MID SPAR UNDERWING FTG BOTH I/B AND O/B HOLES REWORKED AND REPAIRED IAW ER/A 488810-14AD REV ORIGINAL - [SDR DALA1118830136](https://openairdocs.org/sdr/DALA1118830136.md): Fitting · damaged · Feb 23, 2011 · N136DL · Boeing 767332 · Nacelle/Pylon, Frame/Spar/Rib > NR 2 PYLON O/B MID SPAR FITTING BOTH I/B AND O/B HOLES DIA FOUND GREATER THAN 0.875"-0.877" DURING ACCOMPLISHMENT OF EA 01-074904-03AD REV D. NR 2 PYLON O/B MID SPAR UNDERWING FITTING I/B AND O/B HOLES REWORKED AND REPAIRED PER ER.A 488810-14AD REV ORIG. - [SDR DALA1118820136](https://openairdocs.org/sdr/DALA1118820136.md): Fitting · damaged · Feb 23, 2011 · N136DL · Boeing 767332 · Nacelle/Pylon, Frame/Spar/Rib > NR 2 PYLON I/B MID SPAR FTG I/B HOLE DIA FOUND GREATER THAN 0.875"-0.877" DURING ACCOMPLISHMENT OF SIP MOD PER EA 01-074904-03AD REV D. NR 1 PYLON I/B MID SPAR UNDERWING FTG I/B HOLE. REWORKED AND REPAIRED PER ER/A 488810-14AD REV ORIGINAL. - [SDR DALA1118810136](https://openairdocs.org/sdr/DALA1118810136.md): Fitting · damaged · Feb 23, 2011 · N136DL · Boeing 767332 · Nacelle/Pylon, Frame/Spar/Rib > NR 1 PYLON I/B MID SPAR FITTING BOTH I/B AND O/B HOLE DIA FOUND TO BE GREATER THAN 0.875"-0.877" DURING ACCOMPLISHMENT OF SIP MOD PER EA 01-074904-03AD REV D. NR 1 PYLON MID SPAR UNDER WING FITTING BOTH I/B AND O/B HOLES REWORKED AND REPAIRED PER ER/A488810-1 - [SDR DALA1118650136](https://openairdocs.org/sdr/DALA1118650136.md): Skin · misrepaired · Feb 22, 2011 · N136DL · Boeing 767332 · Fuselage Main, Plate/Skin > FUSELAGE SKIN EXTERIOR SURFACE AT STA 390 LT STR 12L PREVIOUS EXTERNAL REPAIRED DOUBLER UN-IDENTIFIED. AREA EVALUATED AND FOUND REPAIR NOT COMPLIED WITH APPROVED REPAIR PER SRM AND 02EA OVERSIZED FASTENER INSTALLED. EXISTING REPAIR REMOVED EVALUATED AND AREA - [SDR DALA1118600136](https://openairdocs.org/sdr/DALA1118600136.md): Spar · cracked · Feb 21, 2011 · N136DL · Boeing 767332 · Nacelle/Pylon, Bulkhead/Firewall > DURING HFEC OPEN HOLE INSP OF FASTENER HOLES PER SB767-54-0081 REV 1 FIG 20 THE OUTBOARD AFT FASTENER HOLE FOUND WITH CRACK INDICATION IN THE AFT SPAR WEB AND MID STRUT BULKHEAD FITTING. 767 SIP MOD (GE ENGINE) - RT STRUT, FREEZE PLUG REPAIR ON OUTBOARD AFT F - [SDR DALA1118800136](https://openairdocs.org/sdr/DALA1118800136.md): Strap · cracked · Feb 18, 2011 · N136DL · Boeing 767332 · Nacelle/Pylon Miscellaneous Structure > 767 SIP MOD (GE ENGINE)-RT WING (01EA) FASTENER HOLE ON NR 2 STRUT STRAP,CHORD P/N:311T3156-1 FOUND GOUGED WHEN ACCOMPLISHING SB 767-54-0081 FIG 7 OPEN HOLE. HFEC INSPECTION, DAMAGED FASTENER HOLE 01 EA AT NR 2 PYLON I/B FWD MOST HOLE COMMON TO MID SPAR F - [SDR DALA1115900136](https://openairdocs.org/sdr/DALA1115900136.md): Skin · cracked · Feb 17, 2011 · N136DL · Boeing 767332 · Wing, Plate/Skin > HFEC OPEN HOLE INSP CARRIED OUT ON RT WING UPPER LINK PITCH LOAD FITTING, COMMON TO WING IN REF TO SB B767-54-0081, FIG 38, REV 1 AND FOUND 03EA HOLES WITH CRACK INDICATION ON UPPER SKIN. 03 EA HOLES ON RT WING UPPER SKIN REPAIRED IAW ER/A 488787-14AD, REV - [SDR DALA1118630136](https://openairdocs.org/sdr/DALA1118630136.md): Spar · cracked · Feb 13, 2011 · N136DL · Boeing 767332 · Nacelle/Pylon, Frame/Spar/Rib > NR 1 PYLON MID SPAR FWD WEB FOUND CRACKED DURING ACCOMP OF SB 767-54-0081 REV 1. NR 1 PYLON MID SPAR CRACKED WEB REPAIRED IAW ER/A 488781-14. - [SDR DALA1115890136](https://openairdocs.org/sdr/DALA1115890136.md): Floorbeam · corroded · Feb 13, 2011 · N136DL · Boeing 767332 · Fuselage Main, Floor Beam > AFT CARGO STA 1219, LBL 35.0 AND LBL 44.0 FLOORBEAM UPPER CHORD FOUND CORRODED. FLOORBEAM UPPER CHORD TRIMMED AT LBL 14 AND REMOVED BET LBL 14 TO LBL 44.0 AND SECTIONAL CHORD REPAIR CARRIED OUT IAW SRM 53-00-07, FIG 201, REPAIR 4 OTIS. - [SDR DALA1115880136](https://openairdocs.org/sdr/DALA1115880136.md): Floorbeam · corroded · Feb 13, 2011 · N136DL · Boeing 767332 · Fuselage Main, Floor Beam > AFT CARGO STA 1197 AT RBL 6.5 AND RBL 44.0 FLOORBEAM UPPER CHORD FOUND CORRODED. FLOORBEAM UPPER CHORD TRIMMED AT RBL 0 AND REMOVED BET RBL0 TO RBL 44.0 AND SECTIONAL CHORD REPAIR CARRIED OUT IAW SRM 53-00-07, FIG 201, REPAIR 4 OTIS. - [SDR DALA1116210136](https://openairdocs.org/sdr/DALA1116210136.md): Floorbeam · corroded · Feb 11, 2011 · N136DL · Boeing 767332 · Fuselage Main, Floor Beam > FWD GALLEY AREA FLOORBEAM AT STA 287 UPPER HORIZ FLANGE UPPER SURFACE FOUND CORRODED AT RBL22 (NRC 0634) AND RBL 62 (NRC 0635). CORROSION AT RBL 62 IS ON EXISTING REPAIR. CABIN FLOORBEAM AT STA 287 UPPER HORIZ FLANGE CUT AND TRIMMED BET RBL8 TO RBL45 FROM R - [SDR DALA1116200136](https://openairdocs.org/sdr/DALA1116200136.md): Stringer Splice · corroded · Feb 11, 2011 · N136DL · Boeing 767332 · Fuselage Main, Longeron/Stringer > FWD CARGO: STRINGER 34 RT AT STA 434 FOUND CORRODED. STA 434, STRINGER 34R REPAIRED IAW SRM 53-30-03, FIG 201, REPAIR 1. - [SDR DL76S091079](https://openairdocs.org/sdr/DL76S091079.md): Line · leaking · Jun 25, 2009 · N136DL · Boeing 767332 · Hydraulic System, Main > CTR HYD QTY DROPPING IN FLT, FOUND HYD LINE FROM BRAKE CNTRL VALVE SOLENOID TO "T" FITTING ON OUTBOARD SIDE OF VALVE LEAKING. FLT CREW VERBAL PUMPS TURNED OFF AT.4 QTY REPLACED HYD LINE FROM BRAKE CONTROL VALVE SOLENOID TO T FITTING ON OUTBOARD SIDE OF VA - [SDR DL76S090918](https://openairdocs.org/sdr/DL76S090918.md): Starter · overheated · May 22, 2009 · N136DL · Boeing 767332 · APU Start/Ignition System > AFTER APU START NOTICED ACRID SMELL IN CABIN. NO VISIBLE SMOKE. FOUND STARTER ON APU BURNED. APU BATTERY AND CHARGER DEAD. REMOVED AND REPLACED APU BATTERY/CHARGER AND STARTER IAW AMM. CHECKED SPRAG CLUTCH NTF. ACFT OK FOR SERVICE. - [SDR DL76S081699](https://openairdocs.org/sdr/DL76S081699.md): Actuator · malfunctioned · Dec 7, 2008 · N136DL · Boeing 767332 · Drag Control Actuator > ON DEPARTURE FROM LAS CREW REPORTED TO DISPATCH THAT L HYD QTY READ ZERO. DISPATCH NOTIFIED MCC THAT ACFT WAS RETURNING TO LAS. REMOVED AND REPLACED NR 6 SPOILER PCA PER AMM. PERFORMED REQUIRED INSPECTION. - [SDR DL76S081285](https://openairdocs.org/sdr/DL76S081285.md): Skin · dented · Oct 3, 2008 · N136DL · Boeing 767332 · Fuselage Main, Plate/Skin > HMV AT ACTS, A FUSELAGE SKIN DENT WAS FOUND AND REPAIRED PER ER/A 01-098988-14. NOTE: AT THE TIME OF ISSUE, THE ER/A WAS NEVER FORMALLY APPROVED, NOR WAS AN MRR SUBMITTED. THIS SITUATION HAS NOW BEEN CORRECTED. - [SDR DL76S081284](https://openairdocs.org/sdr/DL76S081284.md): Frame · cracked · Oct 3, 2008 · N136DL · Boeing 767332 · Fuselage Main, Frame > HMV AT YVR, THE INNER CHORD OF THE RT STA 903.5 FRAME WAS FOUND CRACKED. THE CRACK WAS REPAIRED PER ER/A 01-098604-14AD INSTRUCTIONS. NOTE: AT THE TIME OF ISSUE, THE ER/A WAS NEVER FORMALLY APPROVED, NOR WAS AN MRR ISSUED. THIS SUBMITTAL CORRECTS THIS SITU - [SDR DL76S080362](https://openairdocs.org/sdr/DL76S080362.md): Apu · malfunctioned · Mar 13, 2008 · N136DL · Boeing 767332 · APU Core Engine > SMOKE DETECTORS AT STATIONS 214-215-219 SOUNDED DUE TO LIGHT OIL MIST IN THE CABIN, ALL 3 MID LAVS. THIS HAPPENS ONLY ON THE GROUND WITH APU AIR AND NO ENGS RUNNING. FWD APU TO MCO AND PLACARD PER MEL 49-11-01A. REPLACED APU PER M/M. LEAK CKS GOOD. GENERA - [SDR DL76S080182](https://openairdocs.org/sdr/DL76S080182.md): Wire · broken · Feb 9, 2008 · N136DL · Boeing 767332 · Light System Wiring > FOUND EMERGENCY LIGHT AT SEAT 26F INOP. REPAIRED BROKEN WIRE AND RELAMPED. - [SDR DL76S071527](https://openairdocs.org/sdr/DL76S071527.md): Actuator · cracked · Nov 20, 2007 · N136DL · Boeing 767332 · Drag Control Actuator > DURING TAXI C HYD LOW PRESS LIGHT ILLUM AND QTY WENT TO 0. A/C TOWED BACK TO GATE. FOUND NR 5 SPOILER ACT HOUSING CRACKED. REPLACED SAME, OP CHK AND LEAKS NORMAL. - [SDR DL76S071102](https://openairdocs.org/sdr/DL76S071102.md): Control Cable · broken · Aug 20, 2007 · N136DL · Boeing 767332 · Aileron Control System > LEFT OUTBOARD AILERON LOCKED IN DOWN POSITION. FOUND CABLE A3B-3 FOR LT O/B AIL BROKEN JUST O/B OF THE LT O DROOP QUADRANT. REMOVED BROKEN CABLE RECEIVED NEW CABLE FROM BOEING P/N BACC2C4C04961FG. REPLACED CABLE A3B PER OPN 2000 CABLE REPLACEMENT AND RIGGED - [SDR DL76S050328](https://openairdocs.org/sdr/DL76S050328.md): Skin · lightning strike · Jun 17, 2005 · N136DL · Boeing 767332 · Fuselage Main, Plate/Skin > LIGHTENING STRIKE BLEND OUT AT STA 390 STR 12L BEYOND LIMITS REF SRM 53-00-01 FIG 101. SKIN REPAIRED PER SRM 53-00-01 FIG 201 CAT B REPAIR REPEAT INSPECTIONS PER SRM 53-00-01 FIG 201. AIRCRAFT LOG ITEM F744553. - [SDR DL76S050068](https://openairdocs.org/sdr/DL76S050068.md): Smoke · detected · Jan 28, 2005 · N136DL · Boeing 767332 · Air Distribution System > VISIBLE HAZE / FUMES IN AFT CABIN WITH ENGINE ANTI-ICE ON. RAN ENGINE AND APU WITH PACKS ON, RAN CARGO HEAT, RAN GALLEY OVENS AND ENTERTAINMENT SYSTEM. RAN POTABLE WATER COMPRESSOR, NO SIGNS OF FUMES OR HAZE. - [SDR DL76S040928](https://openairdocs.org/sdr/DL76S040928.md): Tube · unserviceable · Sep 28, 2004 · N136DL · Boeing 767332 · Hydraulic System, Main > C-HYD QTY DRAINED TO 0 WITH SUBSEQUENT C-SYS FAILURE. FOUND CRACKED HYD LINE RT WHEEL WELL REF IPC 32-31-55- 01 ITEM 519. INSTALLED INTERIM LINE. LEAK CHECK OK. LINE TO BE INSPECTED WITHIN 175 FLT HRS AND REPLACED WITH PERMANENT LINE WITHIN 350 FLT HRS, NE - [SDR DL76S040452](https://openairdocs.org/sdr/DL76S040452.md): Light · inoperative · May 20, 2004 · N136DL · Boeing 767332 · Emergency Lighting > 1L DOOR SLIDE LIGHT INOP. REPAIRED SAME. - [SDR DL76S030239](https://openairdocs.org/sdr/DL76S030239.md): Lanyard · separated · Mar 13, 2003 · N136DL · Boeing 767332 · Escape Slide > DOOR DIFFICULT TO ARM/DISARM. SLIDE PACK FELL OUT WHILE DOOR WAS OPENING (2R). INSTALLED NEW SLIDE, OPS NORMAL. - [SDR DL76S021138](https://openairdocs.org/sdr/DL76S021138.md): Charger · failed · Sep 25, 2002 · N136DL · Boeing 767332 · Emergency Lighting > LOWER EMERGENCY LIGHTS AT FWD LT AND RT DOORS EXIT SIGNS INOPERATIVE. REPLACED BATTERY CHARGER AND BATTERY PACK OPS CK GOOD - [SDR DL76S021064](https://openairdocs.org/sdr/DL76S021064.md): Light · inoperative · Sep 11, 2002 · N136DL · Boeing 767332 · Escape Slide > 2L DOOR SLIDE LIGHT INOPERATIVE, RELAMPED - OPS NORMAL. - [SDR DL76S020215](https://openairdocs.org/sdr/DL76S020215.md): Idg · failed · Feb 20, 2002 · N136DL · Boeing 767332 · AC Generator-Alternator > BOTH GENS FAILED AT 1500 FT AFTER TAKEOFF FOR ABOUT 10 SEC/RT GEN CAME BACK ON LINE. LEFT GEN REMAINED FAILED. CK'D OIL LEVEL ON RT IDG FOR CORRECT SERVICING, ALL GOOD. RAN RT ENG, RT IDG CKS GOOD. REPLACED LT ENG IDG PER M/M. RAN LT ENG, IDG OPS AND LEAK - [SDR DL76S020013](https://openairdocs.org/sdr/DL76S020013.md): Manifold · defective · Jan 6, 2002 · N136DL · Boeing 767332 · Engine Fuel Distribution > ENGINE FLAME-OUT ON CLIMBOUT AT 34000. RETURNED FOR LANDING AT MCO. ENGINE FAILED NO MORE THAN 27 MINUTES FROM LANDING. REPLACED FUEL MANIFOLDS AT 11 O'CLOCK AND 6 O'CLOCK POSITIONS RAN NR 2 ENG PER PFHB TEST 4 T/O POWER AND LEAK CK ALL PARAMETERS OK OK FOR - [SDR DL76S011452](https://openairdocs.org/sdr/DL76S011452.md): Flashlight · inoperative · Sep 1, 2001 · N136DL · Boeing 767332 · Emergency Equipment > FLASHLIGHT INOP FWD AC. REPLACED SAME. - [SDR DL76S010622](https://openairdocs.org/sdr/DL76S010622.md): Skin · dented · Apr 15, 2001 · N136DL · Boeing 767332 · Fuselage Main, Plate/Skin > AN EXISTING SKIN REPAIR WAS FOUND WITH A DENT AREA AT THE UPPER EDGE ROW OF THE REPAIR AT BS 1197+78. THE EXISTING REPAIR WAS REMOVED AND ALL UNDELYING DAMGE CUTOUTS COMBINED INTO ONE CUTOUT EXTENDING FROM STRINGER 38L TO STRINGER 36L.THE CUTOUT WAS REPAI - [SDR DL76S010606](https://openairdocs.org/sdr/DL76S010606.md): Light · inoperative · Apr 12, 2001 · N136DL · Boeing 767332 · Emergency Lighting > ON L/O FOUND RIGHT OVERWING FORWARD EMERGENCY LIGHT INOP. RELAMPED - [SDR DL76S002171](https://openairdocs.org/sdr/DL76S002171.md): Panel · failed · Nov 5, 2000 · N136DL · Boeing 767332 · Flight Compartment Lighting > ON DESCENT, SMOKE IN COCKPIT WITH BURNING RUBBER SMELL, SMOKE VISIBLE TO THE EYE. DECLARED EMERGENCY. C/W APPLICABLE POM. FOUND LT R-W T/O SWTCH LIGHT ASSY AND TERMINAL WIRE LUG BURNT AND MELTED. REPLACED WHOLE PANEL ASSY, OPS CKS GOOD. - [SDR DL76S002032](https://openairdocs.org/sdr/DL76S002032.md): Engine · leaking · Oct 16, 2000 · N136DL · Boeing 767332 · Engine (Turbine/Turboprop) > LOSS OF OIL QTY DURING FLT WITH DECREASING OIL PRESSURE. AT TOP OF DESENT WITH THROTTLE TO IDLE OIL PRESSURE WENT THRU 10 PSI INTO RED AREA AND CREW SHUT DOWN ENG. ENG WINDMILLED FOR 15 MIN WITH ZERO OIL PRESSURE. REPLACED ENGINE. Next page: https://openairdocs.org/deregistered/N136DL-2018-01-24/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 = 'N136DL' AND deregistration_id = 'N136DL-2018-01-24' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N136DL-2018-01-24/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.