# Service difficulty reports: N925DL, cancelled Mar 19, 2019 A list on [N925DL, cancelled Mar 19, 2019](https://openairdocs.org/deregistered/N925DL-2019-03-19.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 · 91 reports - [SDR DALA2017062705010](https://openairdocs.org/sdr/DALA2017062705010.md): Wire · damaged · Jun 24, 2017 · N925DL · Doug MD88 · Fire Protection System Wiring > DURING FLIGHT, A RT ENGINE FIRE LOOP MESSAGE DISPLAYED. FOLLOWED QRH, PUT INTO LOOP B. FWD RT ENGINE LOOP A. REPAIRED A DAMAGED WIRE. - [SDR DALA2017050803632](https://openairdocs.org/sdr/DALA2017050803632.md): Receptacle · loose · May 5, 2017 · N925DL · Doug MD88 · Aerodynamic Fairings > TAILCONE ACCESS DOOR CAMLOCK RECEPTICALS LOOSE AND MISSING ON TAILCONE. DOOR CONTAMINATED WITH HYDRAULIC FLUID. REPLACED THE RECEPTICALS. OK FOR SERVICE. FOUND HYD LEAK AND REPAIRED. - [SDR DALA2017040202667](https://openairdocs.org/sdr/DALA2017040202667.md): Trim System · binding · Apr 1, 2017 · N925DL · Doug MD88 · Aileron Tab Control System > AILERON TRIM WHEEL STUCK IN FLIGHT WITH AUTOPILOT ON OR OFF, IT WORKED PRIOR TO DEPARTURE. CHECKED ACTUATOR SCREW ROD END DIMENSION AND DRUM. AILERON TRIM RIG IS GOOD AND NO SIGNS OF BINDING NOTED. COMPLETED IAW AMM 27-10. - [SDR DALA1702990925](https://openairdocs.org/sdr/DALA1702990925.md): Stringer · not reported · Jan 31, 2017 · N925DL · Doug MD88 · Wing, Longeron/Stringer > WING MAIN FRAME STRINGER 11. REPAIRED IAW 5712-01030, SECT 04. - [SDR DALA2017020100823](https://openairdocs.org/sdr/DALA2017020100823.md): Spar · cracked · Jan 31, 2017 · N925DL · Doug MD88 · Wing Spar > RIGHT WING REAR SPAR CRACKED AT XRS 164 LOWER AFT CORNER OF FLAP HINGE FITTING. REPAIRED THE SPAR IAW DWG J060271 REV T. - [SDR DALA2017020100822](https://openairdocs.org/sdr/DALA2017020100822.md): Spar · cracked · Jan 31, 2017 · N925DL · Doug MD88 · Wing Spar > RIGHT WING REAR SPAR CRACKED AT XRS 164 LOWER AFT CORNER OF FLAP HINGE FITTIING. REPAIRED THE SPAR IAW DWG J060271 REV T. - [SDR DALA2017020100821](https://openairdocs.org/sdr/DALA2017020100821.md): Stringer · cracked · Jan 31, 2017 · N925DL · Doug MD88 · Wing, Longeron/Stringer > RIGHT MAIN FUEL TANK STRINGER 11 CRACKED. CUT OUT THE DAMAGED SECTION AND REPAIRED RT WING STRINGER AT XRS 160-164 IAW DWG SR09570100 REV B, AND ERA 553842-14 REV O. - [SDR DALA2016112909376](https://openairdocs.org/sdr/DALA2016112909376.md): Switch · failed · Nov 29, 2016 · N925DL · Doug MD88 · Landing Gear Position and Warning > ON APPROACH, RECEIVED NOSE GEAR UNSAFE LIGHT DURING GEAR EXTENSION. COMPLIED WITH QRH AND NORMAL EXTENSION FOLLOWED. IAW MCC, AN EMERGENCY WAS DECLARED. MAINTENANCE REPLACED THE NOSE GEAR INTERLOCK SWITCH WITH POSITIVE RESULTS DURING MULTIPLE NOSE GEAR EXTENSI - [SDR DALA2016112709281](https://openairdocs.org/sdr/DALA2016112709281.md): Cable · dislodged · Nov 26, 2016 · N925DL · Doug MD88 · Hydraulic System, Main > LEFT FIRE TEE HANDLE FEELS SPONGY. FOUND CABLE GOING TO HYD SHUTOFF VALVE OFF THE PULLEY. REPOSITIONED IAW AMM 20-10. OPS CHECKED NORMAL. INSPECTED PULLEY AND GUARDS. CHECKED GOOD. - [SDR DALA2016102807864](https://openairdocs.org/sdr/DALA2016102807864.md): Psu · malfunctioned · Oct 27, 2016 · N925DL · Doug MD88 · Passenger Oxygen System > DURING CABIN DEPRESSURIZATION EVENT, PSU PANEL DID NOT OPEN AT SEATS 10ABC, 10DE, 13ABC, 12DE, 13DE, 14DE, 15DE, 16DE, 23DE, 24DE, 25ABC, 32ABC, 35ABC, 35DE, 36AB & 36DE. RESET PSU PANELS AND PREFORMED MANUAL EJECT OF OXYGEN MASKS, ALL SEATS AND LAVS PASSED - [SDR DALA2016102707863](https://openairdocs.org/sdr/DALA2016102707863.md): Controller · malfunctioned · Oct 27, 2016 · N925DL · Doug MD88 · Cabin Pressure Controller > THE CREW DECLARED AN EMERGENCY DUE TO LOSS OF CABIN PRESSURE. AN EMERGENCY DESCENT WAS MADE TO FL100 AND THE OXYGEN MASKS DEPLOYED. MAINTENANCE FOUND BOTH 1 AND 2 PRESSURE CONTROLLERS SHOWING A CONTROLLER FAULT. THE LEFT ACM LOWER CONNECTING ELBOW DUCT BOOT WA - [SDR DALA2016062004775](https://openairdocs.org/sdr/DALA2016062004775.md): Battery · discharged · Jun 18, 2016 · N925DL · Doug MD88 · Emergency Lighting > DURING SERVICE CHECK FOUND EMERGENCY LIGHTS AT CEILING ROW 13-15 INOPERATIVE. R & R EMERGENCY LIGHT BATTERIES. OPS CHECK NORMAL. ACFT OK FOR SERVICE. - [SDR DALA2016032502384](https://openairdocs.org/sdr/DALA2016032502384.md): Battery Pack · inoperative · Mar 25, 2016 · N925DL · Doug MD88 · Emergency Lighting > THE CREW FOUND THE AFT LT AND RT OVERWING EXIT SIGNS INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY BATTERIES AND THE LIGHTS CHECKED OK. - [SDR DALA2016011200207](https://openairdocs.org/sdr/DALA2016011200207.md): Girt Bar · detached · Jan 12, 2016 · N925DL · Doug MD88 · Escape Slide > DURING A FORCASTED SLIDE DEPOYMENT, CVG MAINTENANCE FOUND THAT THE L1 DOOR EMERGENCY ESCAPE SLIDE DID NOT DEPLOY DUE TO THE VELCRO TABS AT THE GIRT BAR BEING UN-ATTACHED. A NEW SLIDE WAS INSTALLED AT POSITION L1; REF LOG SHEET 2305013. - [SDR DALA2015081805130](https://openairdocs.org/sdr/DALA2015081805130.md): Floor Support · corroded · Aug 8, 2015 · N925DL · Doug MD88 · Fuselage Miscellaneous Structure > ENTRANCE DOOR FLOOR SUPPORT FRAME, SIX INCHES FROM DOOR SILL HAS CORROSION. REPLACED THE FLOOR SUPPORT IAW DWG 9936534. - [SDR DALA2015081805096](https://openairdocs.org/sdr/DALA2015081805096.md): Support Angle · corroded · Aug 7, 2015 · N925DL · Doug MD88 · Fuselage Miscellaneous Structure > CORROSION AT CARGO TRACK SUPPORT ANGLE, BS 1166, TASK 53-139-05. REMOVED AND INSTALLED NEW ZEE CHANNEL IAW SRM 51-01, PARA 4. - [SDR DALA14032330925](https://openairdocs.org/sdr/DALA14032330925.md): Oven · smoke · May 24, 2014 · N925DL · Doug MD88 · Buffet/Galleys > WHILE ENROUTE, THE F/A REPORTED SMOKE FROM FIRST CLASS GALLEY OVEN. OVEN WAS TURNED OFF AND THE CIRCUIT BREAKERS WERE PULLED. THE F/A DISCHARGED A HALON FIRE EXTINGUISHER INTO THE OVEN. SMOKE DISSIPATED AND FLIGHT CONTINUED. REPLACED OVEN. - [SDR DALA14031380925](https://openairdocs.org/sdr/DALA14031380925.md): Wire Harness · damaged · May 19, 2014 · N925DL · Doug MD88 · Light System Wiring > DURING LINE CHECK, MAINTENANCE FOUND THE EMERGENCY PATH LIGHTING WAS INOPERATIVE AT 27DE. MAINTENANCE REPLACED THE HARNESS AT SEAT 27DE AND THE LIGHTS RETURNED TO AN OPERATIONAL STATE. - [SDR DALA13072580925](https://openairdocs.org/sdr/DALA13072580925.md): Wire · loose · Dec 30, 2013 · N925DL · Doug MD88 · Light System Wiring > DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 27 IN THE CABIN WAS INOPERATIVE. MAINTENANCE FOUND A LOOSE WIRE IN THE CONNECTOR, REPAIRED THE CONNECTOR PIN, AND THE SYSTEM RETURNED TO NORMAL OPERATION. - [SDR DALA13040780925](https://openairdocs.org/sdr/DALA13040780925.md): Rib · cracked · Aug 22, 2013 · N925DL · Doug MD88 · Horizontal Stabilizer, Spar/Rib > RT HORIZONTAL STABILIZER L/E INBD CLOSURE RIB WAS FOUND TO HAVE A CRACK EIGHT INCHES FORWARD OF THE THERMAL ANTI-ICE DUCT. THE CLOSURE RIB WAS REPLACED. - [SDR DALA13042530925](https://openairdocs.org/sdr/DALA13042530925.md): Longeron · cracked · Aug 21, 2013 · N925DL · Doug MD88 · Fuselage Main, Longeron/Stringer > LFEC SHOWS INTERNAL CRACK AT BS 1193, LONGERON 3RT. ACCOMPLISHED HFEC INSPECTION IAW NDT 06-10-01.001 NO CRACKS FOUND. REPAIRED IAW ER/A 517907-14AD, REV O. - [SDR DALA13040530925](https://openairdocs.org/sdr/DALA13040530925.md): Inlet · cracked · Aug 21, 2013 · N925DL · Doug MD88 · Vertical Stabilizer, Plate/Skin > DURING SCHEDULED HEAVY MAINTENANCE, A ONE INCH LONG CRACK WAS FOUND AT THE VERTICAL STABILIZER RAM AIR INLET DUCT RT AFT CORNER. REPAIRED IAW ER/A 517896-14. - [SDR DALA13039950925](https://openairdocs.org/sdr/DALA13039950925.md): Receptacle · worn · Aug 19, 2013 · N925DL · Doug MD88 · Aerodynamic Fairings > MX DISCOVERED THAT ALL OF THE TAILCONE RELEASE SYS GUIDE PIN RECEPTACLES WERE WORN BEYOND ALLOWABLE LIMITS. THE RECEPTACLES WERE REPLACED IAW SRM 51-30 AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS. THE FUNCTIONAL CHECK WAS COMPLETED SATISFACTORILY. - [SDR DALA13039970925](https://openairdocs.org/sdr/DALA13039970925.md): Battery Pack · inoperative · Aug 17, 2013 · N925DL · Doug MD88 · Emergency Lighting > DURING LINE CHECK, MX FOUND THEY HAD NO CONTROL OF THE EMERGENCY ESCAPE LIGHTING AT THE OVERWING EXITS IN THE CABIN, WOULD NOT TURN OFF. MX REPLACED THE BATTERY PACK FOR THE NOTED LIGHTED AREA AND THE LIGHTS RETURNED TO A CONTROLLABLE CONDITION. OPS CHECKED - [SDR DALA13026970925](https://openairdocs.org/sdr/DALA13026970925.md): Battery Pack · inoperative · May 27, 2013 · N925DL · Doug MD88 · Emergency Lighting > DURING LINE CHECK, MX FOUND THAT THE LT WING EXTERIOR EMERGENCY LIGHT WAS MALFUNCTIONING IN THAT IT WOULD REMAIN ON AFTER SELECTOR WAS CHANGED TO "ARMED". MX REPLACED THE BATTERY PACK AND THE LIGHTS RETURNED TO AN OPS CONDITION. - [SDR DALA12011160925](https://openairdocs.org/sdr/DALA12011160925.md): Lanyard · misinstalled · Oct 23, 2012 · N925DL · Doug MD88 · Escape Slide > TAILCONE SLIDE DEPLOYMENT LANYARD WAS NOT LOOPED AROUND THE TAILCONE RELEASE MECHANISM CAM. DISCONNECTED THE LANYARD FROM CLEVIS AT THE SLIDE BOX AND RECONNECTED THE TAILCONE SLIDE DEPLOYMENT LANYARD IAW AMM 25-62-01-201. INSPECTION OF LANYARD INSTALLATION WAS - [SDR DALA1233670925](https://openairdocs.org/sdr/DALA1233670925.md): Pin · worn · May 22, 2012 · N925DL · Doug MD88 · Aerodynamic Fairings > DURING FUNCTIONAL CHECK OF TAILCONE RELEASE SYSTEM OPS 6908, MAINTENANCE FOUND THE TEE PIN, BUSHING, AND CABLE WORN BEYOND THE TEE PIN 11, CAM ASSEMBLY, AND CABLE WERE ALL REPLACED AND THE RII COMPLETED. - [SDR DALA1213520925](https://openairdocs.org/sdr/DALA1213520925.md): Battery · discharged · Mar 4, 2012 · N925DL · Doug MD88 · Emergency Lighting > DURING LINE CHECK, MAINTENANCE FOUND THAT BOTH OF THE FORWARD OVERWING EMERGENCY EXIT SIGNS WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. OPERATIONAL CHECK WAS GOOD. - [SDR DALA1212040925](https://openairdocs.org/sdr/DALA1212040925.md): Skin · corroded · Feb 29, 2012 · N925DL · Doug MD88 · Fuselage Main, Plate/Skin > DURING HMV CORROSION WAS FOUND ON FUSELAGE SKIN STA Y=773 BTW LONGERON 27 TO 28RT. FUSELAGE SKIN WAS BLENDED AND DOUBLER INSTALLED PER REPAIR IAW MD88 SRM 53-04D PARA 57. - [SDR DALA1210850925](https://openairdocs.org/sdr/DALA1210850925.md): Support Fitting · corroded · Feb 26, 2012 · N925DL · Doug MD88 · Wing, Landing Gear Attach Fittings > CORROSION ON RT GEAR SUPPORT FITTING BUSHING BORE I/B SIDE AND NICKS ON LOWER AND UPPER SURFACE, ALSO WEAR ON VERTICAL WALL. REPAIRED PER ERA 500108-14AD ORIG REV. - [SDR DALA1211940925](https://openairdocs.org/sdr/DALA1211940925.md): Fastener · missing · Feb 25, 2012 · N925DL · Doug MD88 · Vertical Stabilizer, Plate/Skin > DURING HMV LOOSE AND MISSING FASTENERS WERE FOUND ON UPPER AND LOWER ROWS OF FASTENERS ABOVE AND BELOW THE SPLICE AT STATION ZFS=52.26 AT VERTICAL STABILIZER LEADING EDGE. LEADING EDGE SKIN/SPLICE WAS REPAIRED IAW ERA 500113-14AD REV ORIG. - [SDR DALA1211920925](https://openairdocs.org/sdr/DALA1211920925.md): Skin · cracked · Feb 25, 2012 · N925DL · Doug MD88 · Fuselage Main, Plate/Skin > DURING HMV THREE CRACKS WERE FOUND ON FUSELAGE SKIN AT THE UPPER FWD DOOR JAMB CORNER AND BTW LONGERON 20 AND 21RT OF THE FWD CARGO COMPARTMENT:0.125"LENGTH;0.437" LENGTH AND 0.468 LENGTH. FUSELAGE SKIN WAS REPAIRED IAW ERA 500104-14AD ORIG. - [SDR DALA1210600925](https://openairdocs.org/sdr/DALA1210600925.md): Skin · damaged · Feb 25, 2012 · N925DL · Doug MD88 · Fuselage Main, Plate/Skin > LIGHTNING STRIKES ON FWD /AFT EDGE OF WINDOW BELT FRAME BTW STA Y=427 AND 446, 465 AND 484, 541 AND 560 AT FUSELAGE SKIN. REPAIRED PER ERA 500106-14 REV ORIG. - [SDR DALA1210590925](https://openairdocs.org/sdr/DALA1210590925.md): Skin · scratched · Feb 25, 2012 · N925DL · Doug MD88 · Fuselage Main, Plate/Skin > SCRATCHES ON FUSELAGE SKIN UPPER FORWARD CORNER OF THE WINDOW BELT PANEL BTW STA Y=693 AND Y=712. REPAIRED PER ERA 500106-14 REV ORIG. - [SDR DALA1210540925](https://openairdocs.org/sdr/DALA1210540925.md): Skin · damaged · Feb 25, 2012 · N925DL · Doug MD88 · Fuselage Main, Plate/Skin > DURING HMV LIGHTNING STRIKE WAS FOUND ON AFT UPPER CORNER IN STA Y=769 AND 750 FUSELAGE SKIN WINDOW BELT FRAME_RT. REPAIRED PER ERA 500111-14. - [SDR DALA1210530925](https://openairdocs.org/sdr/DALA1210530925.md): Structure · damaged · Feb 25, 2012 · N925DL · Doug MD88 · Fuselage Miscellaneous Structure > DURING HMV LIGHTNING STRIKE WAS FOUND ON FWD LOWER CORNER AND AFT EDGE OF WINDOW BELT FRAME BTW STA Y=731-750 RT. SUPPLEMENT TO N/R T0237100 WITH CORRECTIVE ACTION REPAIRED PER ERA 500111-14. - [SDR DALA1209310925](https://openairdocs.org/sdr/DALA1209310925.md): Skin · corroded · Feb 19, 2012 · N925DL · Doug MD88 · Fuselage Main, Plate/Skin > DURING HMV CORROSION WAS FOUND ON FUSELAGE SKIN STA Y=1103-1110 LONGERON 28RT REF MD88 SRM 53-04D FIG 53 FOR REPAIR. CORROSION WAS REMOVED AND ARE WITHIN LIMITS PER SRM53-04D. - [SDR DALA1209300925](https://openairdocs.org/sdr/DALA1209300925.md): Skin · corroded · Feb 19, 2012 · N925DL · Doug MD88 · Fuselage Main, Plate/Skin > DURING HMV CORROSION WAS FOUND ON FUSELAGE SKIN UNDER WING TO FUSELAGE FILLET FAIRING STA Y=1084-1089 ON L29L, Y=1124-1133 BTW LONGERON 23-26L, Y=1115 BTW LONGERON 20-21L AND Y=1105 BTW LONGERON 19-20L REF MD88 SRM 53-04D FIG 53 FOR REPAIR. FUSELAGE SKIN WAS - [SDR DALA1209320925](https://openairdocs.org/sdr/DALA1209320925.md): Skin · corroded · Feb 19, 2012 · N925DL · Doug MD88 · Fuselage Main, Plate/Skin > DURING HMV CORROSION WAS FOUND ON FUSELAGE SKIN UNDER WING TO FUSELAGE FILLET FAIRING STA Y=1043 AND Y=1060-1068 BTW LONGERON 18-19LT REF MD88 SRM 53-04D FIG 53. FUSELAGE WAS BLENDED OUT AND WITHIN LIMITS REF MD88 SRM 53-0 4D PARA 57. - [SDR DALA1209290925](https://openairdocs.org/sdr/DALA1209290925.md): Skin · corroded · Feb 19, 2012 · N925DL · Doug MD88 · Fuselage Main, Plate/Skin > DURING HMV CORROSION WAS FOUND ON FUSELAGE SKIN STA Y=998-1041 BETWEEN LONGERONS 18-17LT. REF MD88 SRM 53-04D FIG 53 FOR REPAIR. FUSELAGE SKIN WAS BLENDED OUT AND WITH LIMITS REF MD88 M 53-04D PARA 57. - [SDR DALA1209270925](https://openairdocs.org/sdr/DALA1209270925.md): Rudder · damaged · Feb 19, 2012 · N925DL · Doug MD88 · Rudder Structure > DAMAGED FLAME SPRAY ON SEVERAL AREAS AT RT RUDDER SURFACE. FLAME SPRAY WAS REPAIRED IAW MD88 SRM 51-70-1AD. 0-1AD PARA 23. - [SDR DALA1209160925](https://openairdocs.org/sdr/DALA1209160925.md): Skin · cracked · Feb 18, 2012 · N925DL · Doug MD88 · Fuselage Main, Plate/Skin > DURING HMV A CRACK WAS FOUND OF 0.093" ON FUSELAGE SKIN AT STA Y=1212 BTW LONGERON 1 AND 2LT. REPAIRED PER ERA 500114-14AD REV ORIG. - [SDR DALA1208530925](https://openairdocs.org/sdr/DALA1208530925.md): Plate · corroded · Feb 15, 2012 · N925DL · Doug MD88 · Horizontal Stabilizer Miscellaneous Structure > HIDDEN DAMAGE; CORROSION AND SCRATCHES ON BARREL NUTS AND HOLES AT RT/LT HORIZONTAL STABILIZER UPPER PLATE AFT EDGE. HORIZONTAL STABLIZER UPPER PLATE WAS REPAIRED IAW ERA 499479-14 REV ORIG. - [SDR DALA1206630925](https://openairdocs.org/sdr/DALA1206630925.md): Skin · corroded · Feb 7, 2012 · N925DL · Doug MD88 · Fuselage Main, Plate/Skin > DURING HMV CORROSION WAS FOUND BETWEEN INNER FUSELAGE SKIN AND PRODUCTION DOUBLER STA Y=575 AT MID CARGO COMPARTMENT BETWEEN LONGERON 28L AND 28R. REF ERA 483854-14 REV C FOR REPAIR. REPAIRED PER ERA 500664-14. - [SDR DALA1206640925](https://openairdocs.org/sdr/DALA1206640925.md): Fastener · missing · Feb 7, 2012 · N925DL · Doug MD88 · Vertical Stabilizer, Plate/Skin > DURING HMV LOOSE AND MISSING FASTENERS WERE FOUND ON UPPER AND LOWER ROWS OF FASTENERS ABOVE AND BELOW THE SPLICE AT STATION ZFS=52.26 AT VERTICAL STABLIZER LEADING EDGE REF EA 09-470871-12. - [SDR DALA1206560925](https://openairdocs.org/sdr/DALA1206560925.md): Panel · debonded · Feb 6, 2012 · N925DL · Doug MD88 · Spoilers > DURING HMV DISBONDED CARBON SHEET WAS FOUND ON RT WING GROUND SPOILER PANEL OUTBD EDGE. REF MD-88 SRM 51-70-1B PARA12 FOR REPAIR. - [SDR DALA1206550925](https://openairdocs.org/sdr/DALA1206550925.md): Skin · nicked · Feb 6, 2012 · N925DL · Doug MD88 · Fuselage Main, Plate/Skin > DURING HMV NICKS WERE FOUND ON EXTERNAL FUSELAGE SKIN ALTERNATE STATIC PORT STA Y=454 BTW LONGERON 27RT AND 28RT REF MD88 SRM 53-04D FIG 12C FOR REPAIR. - [SDR DALA1206230925](https://openairdocs.org/sdr/DALA1206230925.md): Doubler · corroded · Feb 6, 2012 · N925DL · Doug MD88 · Fuselage Main, Plate/Skin > DURING HMV CORROSION WAS FOUND ON FUSELAGE SKIN INTERNAL DOUBLE AT STA Y=244 BTW LONGERON 16L TO 17L. DOUBLER WAS REPLACED IAW MD88 SRM 53-04D FIG 12B. - [SDR DALA1202680925](https://openairdocs.org/sdr/DALA1202680925.md): Beam · corroded · Jan 19, 2012 · N925DL · Doug MD88 · Fuselage Miscellaneous Structure > DURING HMV CORROSION WAS FOUND ON LOWER DOOR JAMB BEAM FROM STA Y=642-687 AT MID CARGO COMPARTMENT REF MD88 SRM 53-05 FIG 123 FOR REPAIR. - [SDR DALA1208260925](https://openairdocs.org/sdr/DALA1208260925.md): Skin · cracked · Jan 11, 2012 · N925DL · Doug MD88 · Fuselage Main, Plate/Skin > CRACK EXT FUSELAGE STA 1437 BETWEEN LONGS 4RT AND 5RT DAMAGED AREA TRIMMED OUT. REPAIR DOUBLER AND FILLER WERE INSTALLED IAW DC9/MD80 SRM 53-04D FIG 27. AIR DOUBLER AND FILLER WERE INSTALLED IAW DC9/MD80 SRM 53-04D FIG 27. Next page: https://openairdocs.org/deregistered/N925DL-2019-03-19/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 = 'N925DL' AND deregistration_id = 'N925DL-2019-03-19' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N925DL-2019-03-19/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, except the copies of manufacturers’ service documents, which belong to their rights holders.