# Service difficulty reports: N648DL, cancelled Dec 6, 2018 A list on [N648DL, cancelled Dec 6, 2018](https://openairdocs.org/deregistered/N648DL-2018-12-06.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 · 54 reports - [SDR DALA2015032402332](https://openairdocs.org/sdr/DALA2015032402332.md): Skin · damaged · Mar 12, 2015 · N648DL · Boeing 757232 · Fuselage Main, Plate/Skin > ER/A 524911-14, REV B, FUSELAGE SKIN, FS 480, S-9L, LIGHTNING DAMAGE, DTA STAGE III APPROVAL LIMIT. ER/A 524911-14, REV B/REPAIR APPROVAL IS LIMITED TO 69,600, TOTAL ACFT FLIGHT CYCLES/ DTA STAGE III APPROVAL IS REQUIRED FOR SERVICE BEYOND 69,600 TOTAL FLIGH - [SDR DALA2014082804833](https://openairdocs.org/sdr/DALA2014082804833.md): Wire · disconnected · Aug 28, 2014 · N648DL · Boeing 757232 · Light System Wiring > EMERGENCY PATH LIGHTS FROM SEAT 39 TO SEAT 45 ARE INOPERATIVE. FOUND WIRE DISCONNECTED. RECONNECTED WIRE. - [SDR DALA14021680648](https://openairdocs.org/sdr/DALA14021680648.md): Skin · damaged · Apr 9, 2014 · N648DL · Boeing 757232 · Fuselage Main, Plate/Skin > LIGHTNING STRIKE AT BS 480, STRINGER 9L. REMOVED DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01. REPAIRED IAW ERA 524911-14, REV A PERM REPAIR. - [SDR DALA2015032602405](https://openairdocs.org/sdr/DALA2015032602405.md): Skin · damaged · Apr 8, 2014 · N648DL · Boeing 757232 · Fuselage Main, Plate/Skin > SKIN DAMAGED. REPAIRED LIGHTNING STRIKE DAMAGE AT BS 480, S9L IAW ER/A 524911-14. - [SDR DALA14019410648](https://openairdocs.org/sdr/DALA14019410648.md): Light · inoperative · Mar 27, 2014 · N648DL · Boeing 757232 · Emergency Lighting > EMERGENCY LIGHT INOPERATIVE AT 39D. REPLACED LIGHT ASSY, CHECKED GOOD. - [SDR DALA14006870648](https://openairdocs.org/sdr/DALA14006870648.md): Trunnion · corroded · Jan 31, 2014 · N648DL · Boeing 757232 · Wing, Landing Gear Attach Fittings > LT WING MLG FWD TRUNNION ATTACH FITTING, LOWER BORES ARE CORRODED. - [SDR DALA14006730648](https://openairdocs.org/sdr/DALA14006730648.md): Trunnion · corroded · Jan 30, 2014 · N648DL · Boeing 757232 · Wing, Landing Gear Attach Fittings > TRUNNION ATTACH FITTING, LOWER BORES CORRODED. REPAIRED IAW ER/A 499930-14AD. - [SDR DALA14013410648](https://openairdocs.org/sdr/DALA14013410648.md): Light · inoperative · Jan 25, 2014 · N648DL · Boeing 757232 · Emergency Lighting > LT DOOR SLIDE EMERGENCY LIGHT INOPERATIVE. REPAIRED IAW ERA 522660-14, REV A. OPS CHECKED GOOD. - [SDR DALA13063140648](https://openairdocs.org/sdr/DALA13063140648.md): Skin · corroded · Nov 23, 2013 · N648DL · Boeing 757232 · Fuselage Main, Plate/Skin > FOUND ON WALK AROUND, AFT LAVATORY SERVICE PANEL HAS CORROSION ON BELLY SKIN UNDER DOUBLER ON FWD INBD SIDE. REPAIRED IAW ERA 520885-14 REV 0. - [SDR DALA13063850648](https://openairdocs.org/sdr/DALA13063850648.md): Skin · corroded · Nov 22, 2013 · N648DL · Boeing 757232 · Fuselage Main, Plate/Skin > CORROSION FOUND ON FUSELAGE SKIN UNDER THE AFT LAV SERVICE PAN, BETWEEN BS 1682-1701 S28-29R. DAMAGE REPAIRED IAW SECTION I OF ER/A 520885-14, REV ORIGINAL. - [SDR DALA13063130648](https://openairdocs.org/sdr/DALA13063130648.md): Skin · damaged · Nov 18, 2013 · N648DL · Boeing 757232 · Fuselage Main, Plate/Skin > SKIN HAS CORROSION DAMAGE AT FWD LT CORNER. REMOVED AT LAV PAN ASSY AT STA 1682 AND STR 29R-26R TO ACCESS SKIN DAMAGE AND REF PRI 520885-14 AD REV ORIG INSTALLED LAV PAN ASSY IAW DWG 146N3650. - [SDR DALA13050610648](https://openairdocs.org/sdr/DALA13050610648.md): Power Supply · inoperative · Oct 6, 2013 · N648DL · Boeing 757232 · Emergency Lighting > DURING SERVICE CHECK, FOUND L1 AND R1 VERTICAL EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY, OPS CHECKED GOOD. - [SDR DALA1230010648](https://openairdocs.org/sdr/DALA1230010648.md): Skin · cracked · May 6, 2012 · N648DL · Boeing 757232 · Fuselage Main, Plate/Skin > DURING INSPECTION FOUND FUSELAGE SKIN CRACK AT STATION 1814 BETWEEN STRINGERS 25R AND 19R. MAINTENANCE TRIMMED OUT DAMAGE AND ACCOMPLISHED HFEC OF CUT OUT AREA. FABRICATED REPAIR DOUBLER PER SRM 53-00-01 REPAIR 3 AND INSTALLED. - [SDR DALA1170370648](https://openairdocs.org/sdr/DALA1170370648.md): Contact · broken · Dec 19, 2011 · N648DL · Boeing 757232 · Emergency Lighting > LINE MAINTENANCE FOUND AFT SLIDE ILLUMINATION LIGHT INOPERATIVE. INSPECTION REVEALED CONTACT BROKEN IN LIGHT ASSEMBLY. LIGHT ASSEMBLY REPLACED AND OPERATION NORMAL. - [SDR DL757081276](https://openairdocs.org/sdr/DL757081276.md): Rib · damaged · Oct 1, 2008 · N648DL · Boeing 757232 · Wing Spar > RT WING RIB STA 18 HAS 1 EA ELONGATED HOLE AT STR 9.5 FWD OUTBOARD HOLE ON FWD LEG OF STR CHANNEL. REWORKED DAMAGED HOLE TO A FINAL SIZE OF.250, EDGE MARGIN OF.450 IAW 757 SRM 51-40-05 FIG 2. INSTALLED 1 EA FASTENER ON STRINGER CLIP U9.5 RT WING RIB 18 PER - [SDR DL757081274](https://openairdocs.org/sdr/DL757081274.md): Floorbeam · corroded · Oct 1, 2008 · N648DL · Boeing 757232 · Fuselage Main, Floor Beam > UPON DAMAGE REMOVAL OF MAIN CABIN DECK PLATE, FOUND STA 1680 FLOORBEAM CORRODED IN NUMEROUS LOCATION. BLENDED CORROSION IAW 757 SRM 51-10-02. CORROSION FOUND OUT OF LIMITS. REPLACEMENT FLOORBEAM CAP INSTALLED IAW SRM 51-40-02 AND ERA 470312-14. - [SDR DL757081273](https://openairdocs.org/sdr/DL757081273.md): Flap · gouged · Oct 1, 2008 · N648DL · Boeing 757232 · Trailing Edge Flaps > RIGHT OUTBOARD MAIN FLAP L/E GOUGED ON I/B END. BLENDED OUT GOUGE IAW 757 SRM 51-10-02; OUT OF LIMITS. INSTALLED REPAIR DOUBLER, FILLER, AND CAP END IAW 757 SRMS 51-46-02 AND 57-53-01. - [SDR DL757081272](https://openairdocs.org/sdr/DL757081272.md): Skin · gouged · Oct 1, 2008 · N648DL · Boeing 757232 · Leading Edge Devices > SMALL GOUGE ON T/E OF SLAT NR 3. REMOVED DAMAGED LOWER SKIN ON NR 3 SLAT AND PREPARED AREA FOR INSTALL OF FLUSH REPAIR IAW B757 SRM 51-70-10 REPAIR 4 FIG 202. BONDED REPAIR DOUBLER IAW SRM 51-70-10. - [SDR DL757081264](https://openairdocs.org/sdr/DL757081264.md): Fitting · damaged · Sep 30, 2008 · N648DL · Boeing 757232 · Nacelle/Pylon Miscellaneous Structure > NR 1 PYLON SHEAR TIE DRAG FITTING ASSY HAS ELONGATED HOLE. REPAIR C/W PER ERA 470311-14 REV 1 AND SRM 51-20-07. - [SDR DL757081260](https://openairdocs.org/sdr/DL757081260.md): Skin · corroded · Sep 30, 2008 · N648DL · Boeing 757232 · Fuselage Main, Plate/Skin > FUSELAGE SKIN STA 610 (AT RADIO ALT) HAS CORROSION. REPAIR C/W PER ERA 470545-14. - [SDR DL757081254](https://openairdocs.org/sdr/DL757081254.md): Skin · dented · Sep 29, 2008 · N648DL · Boeing 757232 · Fuselage Main, Plate/Skin > DURING HMV AT SAA, A DENT WAS FOUND IN A FUSELAGE SKIN SECTION WHICH HAD BEEN PREVIOUSLY SPLICED IN DURING AN EARLIER SKIN REPAIR. THE DENT WAS REMOVED AND REPAIRED PER B757 SRM GUIDELINES. THE ER/A IS CLASSIFIED AS MAJOR AND AD RELATED BECAUSE OF THE PREVIO - [SDR DL757081252](https://openairdocs.org/sdr/DL757081252.md): Skin · damaged · Sep 29, 2008 · N648DL · Boeing 757232 · Fuselage Main, Plate/Skin > DURING HMV AT SAA, ADDITIONAL DAMAGE WAS FOUND IN A PREVIOUSLY INSTALLED SKIN SPLICE REPAIR BETWEEN STA 610 AND 660, STRINGERS S-15L TO S-19L. A DENT AND CREASE WAS FOUND IN THE SPLICED IN SKIN SECTION AT STA 620 BETWEEN S-16L AND S-17L. THE EXISTING SKIN SP - [SDR DL757081249](https://openairdocs.org/sdr/DL757081249.md): Spar · gouged · Sep 29, 2008 · N648DL · Boeing 757232 · Wing Spar > DURING WINGLET MOD, THE LT WING REAR SPAR LOWER CHORD WAS DAMAGED BY TOOLING. A GOUGE WAS BLENDED SMOOTH AND TREATED FOR CORROSION PROTECTION. THE BLEND AND TREATMENT WAS APPROVED BY BOEING. - [SDR DL757081235](https://openairdocs.org/sdr/DL757081235.md): Skin · corroded · Sep 26, 2008 · N648DL · Boeing 757232 · Fuselage Main, Plate/Skin > DURING HMV AT SAA, CORROSION WAS FOUND ON THE BELLY SKIN UNDER THE RADIO ALTIMETER ANTENNA. THE CORROSION WAS REMOVED AND A REPAIR WAS INSTALLED PER BOEING INSTRUCTIONS. - [SDR DL757081233](https://openairdocs.org/sdr/DL757081233.md): Bulkhead · corroded · Sep 26, 2008 · N648DL · Boeing 757232 · Fuselage Main, Bulkhead > DURING HMV AT SAA, CORROSION WAS FOUND IN THE RADIUS OF THE AFT LOWER CHORD OF THE AFT PRESSURE BULKHEAD AT STA 1862. THE CORROSION WAS REMOVED BY BLENDING TO A DEPTH OF 0.030 INCH. THE AREA WAS TREATED FOR CORROSION PREVENTION AND APPROVED AS IS BY BOEING E - [SDR DL757081232](https://openairdocs.org/sdr/DL757081232.md): Drag Angle · damaged · Sep 26, 2008 · N648DL · Boeing 757232 · Nacelle/Pylon Miscellaneous Structure > DURING HMV AT SAA, THE NR 1 PYLON SHEAR TIE DRAG FITTING HAD AN ELONGATED HOLE. THE HOLE WAS OVERSIZED TO REMOVE THE ELONGATION AND A FREEZE PLUG BUSHING WAS INSTALLED ACCEPT A NOMINAL SIZE FASTENER PER BOEING REPAIR INSTRUCTIONS. - [SDR DL757081231](https://openairdocs.org/sdr/DL757081231.md): Floorbeam · corroded · Sep 25, 2008 · N648DL · Boeing 757232 · Fuselage Main, Floor Beam > DURING CURRENT HMV, CORROSION WAS FOUND ON THE 1681 FLOORBEAM, ON THE UPPER CHORD (UPPER AND LOWER SURFACE). DUE TO THIS, THE UPPER CAP WAS CUT OUT AND REMOVED PER BOEING INSTRUCTIONS, AND A REPLACEMENT UPPER CAP INSTALLED AS DOCUMENTED IN ER/A 470312-14 (CAT - [SDR DL757081266](https://openairdocs.org/sdr/DL757081266.md): Rib · damaged · Sep 12, 2008 · N648DL · Boeing 757232 · Wing, Rib/Bulkhead > LT WING RIB 25 LOWER SKIN PANEL RIB CHORD HAS SHORT EDGE MARGIN ON UPPER ROW OF FAST HOLES. REPAIR C/W PER ERA 470544-14 REV O AND APB DWG 757-3250 REV B. - [SDR DL757081259](https://openairdocs.org/sdr/DL757081259.md): Frame · corroded · Sep 11, 2008 · N648DL · Boeing 757232 · Fuselage Main, Frame > FRAME CHORD HAS PITTING CORROSION STA 1862 AT ACCESS DOOR 313AL. C/W REPAIR PER ERA 470550-14. - [SDR DL757081169](https://openairdocs.org/sdr/DL757081169.md): Spar · damaged · Sep 10, 2008 · N648DL · Boeing 757232 · Nacelle/Pylon, Frame/Spar/Rib > DURING CURRENT HMV, AN OVERSIZED HOLE WAS FOUND ON THE SPAR CHORD, NR 1 PYLON, DURING ACCOMPLISHMENT OF PYLON MOD. SUBJECT HOLE IS COMMON TO SIDE STRUT SKIN. BOEING WAS CONTACTED CONCERNING OVERSIZING SUBJECT HOLE, INSPECTING, AND INSTALLATION OF OVERSIZED F - [SDR DL757081261](https://openairdocs.org/sdr/DL757081261.md): Spar · damaged · Sep 7, 2008 · N648DL · Boeing 757232 · Wing Spar > LT WING REAR SPAR LWR T-CAP HAS TOOLING MARK AT RIB STA 23. COMPLETED REPAIR PER ERA 470321-14 REV O. - [SDR DL757081265](https://openairdocs.org/sdr/DL757081265.md): Skin · damaged · Aug 25, 2008 · N648DL · Boeing 757232 · Nacelle/Pylon, Plate/Skin > ONE EACH HOLE IS OVERSIZED TO.437 ON NR 1 PYLON I/B SIDE. REPAIR C/W PER ERA 469688-14 DATED 9/10/08. - [SDR DL757081217](https://openairdocs.org/sdr/DL757081217.md): Structure · damaged · Aug 25, 2008 · N648DL · Boeing 757232 · Nacelle/Pylon, Main Frame > 1 HOLE IS OVERIZED TO.437 (NEXT NOMINAL STANDARD) ON NR 1 ENG PYLON I/B SIDE. INSTALLED 1 FASTENER AND COLLAR IAW SRM 51-40-02. COMPLIED WITH ERA 469688. - [SDR DL757081221](https://openairdocs.org/sdr/DL757081221.md): Structure · dented · Aug 24, 2008 · N648DL · Boeing 757232 · Emergency Exits > LT FWD OVERWING EMERGENCY ESCAPE HATCH DOOR LWR RT SIDE EDGE DENTED. REFORMED AREA AT LT FWD OVERWING ESCAPE HATCH DOOR LWR RT SIDE IAW SRM 51-30-01. - [SDR DL757081219](https://openairdocs.org/sdr/DL757081219.md): Skin · gouged · Aug 23, 2008 · N648DL · Boeing 757232 · Leading Edge Devices > SMALL GOUGE ON T/E OF SLAT NR 3. BONDED SKIN FILLER AND INTERNAL DOUBLER AND CORE PLUG IAW SRM 51-70-10. - [SDR DL757081262](https://openairdocs.org/sdr/DL757081262.md): Seat Track · corroded · Aug 20, 2008 · N648DL · Boeing 757232 · Fuselage, Seat/Cargo Attach Fittings > SEAT TRACK HAS CORROSION STA 686-710 LBL 24.5. REMOVED AND REPLACED SEAT TRACK PER SRM 51-00-02. - [SDR DL757081225](https://openairdocs.org/sdr/DL757081225.md): Seat Track · corroded · Aug 20, 2008 · N648DL · Boeing 757232 · Fuselage, Seat/Cargo Attach Fittings > SEAT TRACK HAS EXFOLIATED CORROSION AT STA 686-710 LBL 45.5. REMOVED SEAT TRACK FROM STA 669 TO STA 788 LBL 45.5 IAW SRM 53-00-51. INSTALLED REPLACEMENT SEAT TRACK IAW SRM 51-20-01. - [SDR DL757081367](https://openairdocs.org/sdr/DL757081367.md): Terminal · broken · Aug 19, 2008 · N648DL · Boeing 757232 · Door System Wiring > EMERGENCY LIGHT TEST SWITCH AT L2 DOOR HAS A BROKEN COVER AND TERMINAL. (OFF A/C PART). PROCURED EMERGENCY LIGHT TEST SWITCH FOR L2 DOOR. REPLACED SWITCH ON DELTA OPN 1818 AND TESTED ON DELTA OPN 6813. - [SDR DL757081224](https://openairdocs.org/sdr/DL757081224.md): Skin · dented · Aug 19, 2008 · N648DL · Boeing 757232 · Fuselage Main, Plate/Skin > FUSELAGE STA 1620 BETWEEN S27R AND S28R LWR SIDE HAS DENT. INSTALLED DOUBLER AND 2 FILLERS IAW SRM 53-00-01. - [SDR DL757081271](https://openairdocs.org/sdr/DL757081271.md): Skin · damaged · Aug 18, 2008 · N648DL · Boeing 757232 · Fuselage Main, Plate/Skin > ACCOMPLISH PERM REPAIR PER SRM 53-00-01, FIG 201, SHT 6 ACTL LINE 3103; HOLE/CRACK AT STA 646 LEFT HAND SIDE BELOW S17L. REMOVED EXTERNAL SPLICE AND 5 INTERNAL DOUBLERS IAW ERA470314-14 AND B757 SRM 51-40-02. INSTALLED REPAIR DOUBLER, FILLER IAW SRM 53-00-01 - [SDR DL757061035](https://openairdocs.org/sdr/DL757061035.md): Collar · cracked · Dec 15, 2006 · N648DL · Boeing 757232 · Service Doors > REPORTED TO MTC 4R DOOR WILL NOT STAY OPEN. FOUND 4R DOOR GUST LOCK COLLAR BROKEN/CRACKED. REPLACED GUST LOCK COLLAR PER AMM 52-11-08. - [SDR DL75K040887](https://openairdocs.org/sdr/DL75K040887.md): Transmitter · intermittent · Sep 16, 2004 · N648DL · Boeing 757232 · Trailing Edge Flap Control System > DURING DESCENT INTO EWR FLAPS LOCKED OUT AT LESS THAN 1 UNIT WITH STATUS MSG T/E FLAP DISAGREE AND T/E FLAP ASYMMETRY. FLAP UP LANDING AT EWR. REPLACED LT FLAP TRANSDUCER. - [SDR DL75K031004](https://openairdocs.org/sdr/DL75K031004.md): Battery Pack · discharged · Nov 11, 2003 · N648DL · Boeing 757232 · Emergency Lighting > DOOR 4R OVERHEAD EXIT SIGN EMERGENCY LIGHT WILL NOT ILLUMINATE. FOUND BAD BATTERY ASSY. REPLACED SAME. - [SDR DL757030692](https://openairdocs.org/sdr/DL757030692.md): Tire · cut · Jul 23, 2003 · N648DL · Boeing 757232 · Landing Gear Brake System > LT. NOSE TIRE HAS FOD DAMAGE - REPLACED SAME - [SDR DL757021308](https://openairdocs.org/sdr/DL757021308.md): Light · inoperative · Nov 10, 2002 · N648DL · Boeing 757232 · Emergency Lighting > EMERGENCY EXIT LIGHT OVER 2R DOOR INOP. - [SDR DL757011662](https://openairdocs.org/sdr/DL757011662.md): Light · malfunctioned · Oct 13, 2001 · N648DL · Boeing 757232 · Landing Gear Position and Warning > ON APPROACH, PLACED GEAR HANDLE DOWN, DID NOT GET LEFT GEAR SAFE LIGHT. LIGHT TESTED GOOD. RAN GEAR LIGHT DISAGREEMENT CHECKLIST. IT FELT AS IF THE LEFT MAIN GEAR CAME DOWN AT THAT TIME, BUT NO GREEN LIGHT AND WOULD NOT TEST. COULD NOT RELAMP EASILY. REPL - [SDR DL757010684](https://openairdocs.org/sdr/DL757010684.md): Hydraulic Line · ruptured · Apr 27, 2001 · N648DL · Boeing 757232 · Hydraulic System, Main > LEFT HYD QTY LOSS IN FLIGHT. UNABLE TO STOP LOSS WITH POM PROCEDURES. FOUND RIGHT GEAR TRUCK TILT PRESSURE LINE RUPTURED. REPLACED LINE. - [SDR DL757000629](https://openairdocs.org/sdr/DL757000629.md): Panel · arced · Apr 3, 2000 · N648DL · Boeing 757232 · Dependent Position Determining System > WHILE ENGAGING CAPTAINS AUTO/MAN VOR/DME SWITCH ON MCP A SMALL AMOUNT OF SMOKE CAME OUT FROM UNDER THE GLARESHIELD. SWITCH WAS PULLED OUT AND SMOKE STOPPED. FOUND VOR/DME CONTROL PANEL BULBS ARCING. REPLACED PANEL PER M/M. OPS CHECK GOOD. - [SDR DL757991905](https://openairdocs.org/sdr/DL757991905.md): Skin · dented · Aug 23, 1999 · N648DL · Boeing 757232 · Fuselage Main, Plate/Skin > FUSELAGE SKIN FS 1689, STRINGER 15L-16L, DENT CUTOUT REPAIR. THE FUSELAGE SKIN AT FS 1689 BETWEEN STRINGERS 15L AND 16L WAS FOUND DENTED. THE DAMAGED AREA OF SKIN WAS CUTOUT SPANNING THE STRINGERS OVER A 9.8 BY 2 AREA. THE CUTOUT WAS REPAIRED WITH AN E - [SDR DL757990779](https://openairdocs.org/sdr/DL757990779.md): Valve · failed · Apr 10, 1999 · N648DL · Boeing 757232 · Trailing Edge Flap Control System > DURING APPROACH WITH FLAPS AT 1 DEG, THE /LE SLAT ASYM/EICAS MSG AND WARNING LIGHT ABOVE FLAP GAUGE CAME ON. ACCOMPLISHED CHECKLIST IN ATTEMPT TO ELECTRICALLY DRIVE FLAPS TO 20 DEG, BUT NOTHING CHANGED FROM THE 1 DEG POSITION. FLT DIVERTED TO JFK. REPLACED Next page: https://openairdocs.org/deregistered/N648DL-2018-12-06/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 = 'N648DL' AND deregistration_id = 'N648DL-2018-12-06' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N648DL-2018-12-06/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.