# Service difficulty reports: N765DA, cancelled Apr 23, 2001

A list on [N765DA, cancelled Apr 23, 2001](https://openairdocs.org/deregistered/N765DA-2001-04-23.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR DLL19010014](https://openairdocs.org/sdr/DLL19010014.md): Circuit Breaker · failed · Jan 4, 2001 · N765DA · Lkheed 10113853 · Battery Overheat Warning System
  > BATTERY CONDITION LIGHT ON CAT. REPLACED C/B AND REPAIRED WIRE TO C/B.
- [SDR DLL19002311](https://openairdocs.org/sdr/DLL19002311.md): Girt Bar · disconnected · Nov 28, 2000 · N765DA · Lkheed 10113853 · Escape Slide
  > DOOR 3L CABIN DOOR HARD TO OPEN OR CLOSE - GIRT BAR HAS TO BE MANUALLY PLACED IN RETAINER WHEN CLOSED, CORRECTIVE ACTION REATTACHED GIRT BAR IN HOOK LOCK ASSEMBLIES DOOR OPERATES NORMALLY AND ARMS DISARMS NORMALLY
- [SDR DLL19001038](https://openairdocs.org/sdr/DLL19001038.md): Unknown · odor · May 26, 2000 · N765DA · Lkheed 10113853 · Cabin Equipment/Furnishings
  > F/A REPORTED THAT ON APPROACH A BURNING SMELL WAS AROUND ROW 22. INVESTIGATED CABIN GALLEY AND SERVICE AREAS ABOVE AND BELOW FLOOR LEVEL. RAN ALL PNEUMATIC ELECTRIC AND GALLEY SYSTEMS, ALL OPNS GOOD.
- [SDR DLL19000921](https://openairdocs.org/sdr/DLL19000921.md): Power Supply · discharged · May 9, 2000 · N765DA · Lkheed 10113853 · Emergency Lighting
  > POWER SUPPLY FOR EMERGENCY ESCAPE PATH LIGHTING SYSTEM ONLY LAST 1 MINUTE.
- [SDR DLL19000777](https://openairdocs.org/sdr/DLL19000777.md): Spoiler Panel · deployed · Apr 21, 2000 · N765DA · Lkheed 10113853 · Drag Control System
  > SPLR PANELS NR 1 AND NR 3 ON LT WING DEPLOYED ON T/O. NO INDICATIONS IN COCKPIT, LOCKED UP, WILL NOT COME DOWN. ABORTED T/O AT 100 KTS. REPLACED BELL CRANK AT SPOILER MIXER FOR FROZEN BEARING.
- [SDR DLL19992666](https://openairdocs.org/sdr/DLL19992666.md): Unknown · odor · Dec 7, 1999 · N765DA · Lkheed 10113853 · Air Distribution System
  > ODOR APPEARED IN CABIN DURING LAST 5 - 10 MINUTES OF FLIGHT PRIMARILY IN THE REAR OF B-ZONE. FORWARD TO MCO AND PLAC PER MEL 25-99-06. FLIGHT ATTENDANTS REPORTED AN ELECTRICAL ODOR. CHECKED CABIN LIGHTING SYS, ALL OK. CHECKED MID AND AFT GALLEY EQUIPMENT.
- [SDR DLL19991857](https://openairdocs.org/sdr/DLL19991857.md): Bulkhead Web · damaged · Aug 19, 1999 · N765DA · Lkheed 10113853 · Fuselage Main, Bulkhead
  > TOOLING DAMAGE WAS FOUND ON THE NLG WHEEL WELL BULKHEAD AT APPROX FS 416, RBL 22 ON THE LWR SURFACE O/B FILLET RADIUS INSIDE THE RT ECS COMPT (NLG BLKHD WEB CAP). DAMAGE DEPTH IS APPROX 0.060 BY 1 IN LENGTH (FWD/AFT) BY 0.5 (VERT). REPAIRED PER ERA 333433-14
- [SDR DLL19991828](https://openairdocs.org/sdr/DLL19991828.md): Rib · cracked · Aug 12, 1999 · N765DA · Lkheed 10113853 · Wing, Rib/Bulkhead
  > LT AND RT WING UPPER RIB CAP AT IWS 555 FOUND CRACKED DURING ROUTINE INSPECTION ERA 333431-14 REV B.
- [SDR DLL19991334](https://openairdocs.org/sdr/DLL19991334.md): Module · failed · Jun 13, 1999 · N765DA · Lkheed 10113853 · Hydraulic System, Main
  > AFTER DROPPING GEAR, 3 GREEN GEAR LIGHTS. C-SYS PRESSURE STARTED DECREASING, FLUID LOSS INDICATED. DOOR LIGHTS FOR MAIN GEAR REMAINED OPEN. WENT THRU CHECK LIST. TURNED ENG /ATM PUMPS ON, C-SYS OFF.
- [SDR DLL19982575](https://openairdocs.org/sdr/DLL19982575.md): Blade · lack of lube · Dec 6, 1998 · N765DA · Lkheed 10113853 · Turbine Engine Compressor Section
  > NR 2 ENGINE HAD HIGH FAN VIBS BOTH A AND B CHANNELS, SHOWED APPROX 2.7 UNITS. FAN VIBS INCREASED WHEN THROTTLES RETARTED TO IDLE. SHUT DOWN NUMBER TWO ENGINE PER POM. LUBED BLADES, PERFORMED VIB RUN, WITHIN M/M LIMITS.
- [SDR DLL17981507](https://openairdocs.org/sdr/DLL17981507.md): Power Supply · inoperative · Jul 20, 1998 · N765DA · Lkheed 10113853 · Emergency Lighting
  > ON LAYOVER, CHECK FOUND AFT LEFT HAND OVERHEAD EMERGENCY LIGHTS WON'T TEST. REPLACED ASSOCIATED BATTERY PACK AT 2L AND ADDITIONAL PACK AT 3R. ALL EMER LIGHTS TEST GOOD.
- [SDR DLL17981280](https://openairdocs.org/sdr/DLL17981280.md): Power Supply · inoperative · Jun 17, 1998 · N765DA · Lkheed 10113853 · Emergency Lighting
  > ON LAYOVER, FOUND EMERGENCY BATTERY PACK NOT CHARGING. REPLACED EMERGENCY LIGHT BATTERY PACK.
- [SDR DLL17981046](https://openairdocs.org/sdr/DLL17981046.md): Engine · failed · May 16, 1998 · N765DA · Lkheed 10113853 · Engine (Turbine/Turboprop)
  > ON T/O, THE NR 1 ENG GAVE LOUD BANG. VIBES PEGGED OUT AT 5 PLUS AND EGT LT CAME ON. SHUT NR 1 ENG DOWN AND LANDED ATL. REPLACE NUMBER ONE ENGINE.
- [SDR DLL17980682](https://openairdocs.org/sdr/DLL17980682.md): Counterbalance · inoperative · Mar 29, 1998 · N765DA · Lkheed 10113853 · Emergency Exits
  > AIRCRAFT ARRIVED WITH L3 EMERGENCY HANDLE PARTIALLY OPEN. REPLACED COUNTERBALANCE AND RIGGED DOOR.
- [SDR DLL17972049](https://openairdocs.org/sdr/DLL17972049.md): Power Supply · inoperative · Oct 13, 1997 · N765DA · Lkheed 10113853 · Emergency Lighting
  > OVERHEAD EMER ESCAPE PATH LIGHTS FAILED TO OPERATE DURING TEST. REPLACE POWER SUPPLY.
- [SDR DLL17971958](https://openairdocs.org/sdr/DLL17971958.md): Skin · cracked · Sep 25, 1997 · N765DA · Lkheed 10113853 · Wing, Plate/Skin
  > THE LOWER CENTER BOX SKIN ON THE LT WING WAS FOUND CRACKED AT THE S-14 RUNOUT AT WS 248. THE CRACK RUNS FORE AND AFT THROUGH THE OUTBOARD MOST FASTENERS OF S-14 AND IS APPROX 2 IN LENGTH. STOP DRILL CRACK WITH A.5 HOLE LOCATING THE HOLE.25 AHEAD OF THE CRA
- [SDR DLL17971959](https://openairdocs.org/sdr/DLL17971959.md): Frame · corroded · Sep 24, 1997 · N765DA · Lkheed 10113853 · Fuselage Main, Frame
  > DURING ACCOMPLISHMENT OF SI 7-63916-12AD PART II, A 2 INCH LONG CRACK WAS FOUND IN THE WEB OF THE RIGHT HAND FS 983 FRAME. THE CRACK RUNS VERTICALLY IN THE WEB OF THE FRAME AND ACROSS THE UPPER INTEGRAL STIFFENER AS SHOWN IN FIGURE 1 OR ER/A. ACCORDING TO AD
- [SDR DLL17971336](https://openairdocs.org/sdr/DLL17971336.md): Skin · punctured · Jun 28, 1997 · N765DA · Lkheed 10113853 · Fuselage Main, Plate/Skin
  > EXTENSIVE DAMAGE WAS INCURRED TO THE FUSELAGE SKIN PANEL BETWEEN STA 539 AND 639 BETWEEN STR 42 AND 48. THE DAMAGE CONSISTED OF FOUR LARGE SKIN PUNCTURES, TWO DENTED FRAME TO SKIN CLIPS, AND A DENTED STRINGER. THE DAMAGED FRAME TO SKIN CLIPS ARE LOCATED AT S
- [SDR DLL17970301](https://openairdocs.org/sdr/DLL17970301.md): Valve · leaking · Feb 18, 1997 · N765DA · Lkheed 10113853 · Cabin Cooling System
  > AREA E OVERHEAT ON CLIMB-OUT. RETURNED TO BASE. FOUND NR 3 PACK VALVE LEAKING AT AFT END. REPLACED NR 3 PACK VALVE. VALVE P/N 217002711 OFF KC16803 ON 065.
- [SDR DLL17970438](https://openairdocs.org/sdr/DLL17970438.md): Rccb · failed · Feb 9, 1997 · N765DA · Lkheed 10113853 · Fuel Dump System
  > COULD NOT SHUT OFF 2R INBOARD BOOST PUMP. DIVERTED TO JFK. REPLACED 2R INBD PUMP RCCB, OPS CK OK.
- [SDR DLL17962418](https://openairdocs.org/sdr/DLL17962418.md): Battery Pack · not seated · Oct 30, 1996 · N765DA · Lkheed 10113853 · Emergency Lighting
  > HALF OF THE EMERGENCY EGRESS PATH LIGHTS INOP. RESEATED BATTERY PACKS, OPS NORMAL.
- [SDR DLL17961313](https://openairdocs.org/sdr/DLL17961313.md): Battery · missing · May 29, 1996 · N765DA · Lkheed 10113853 · Emergency Lighting
  > FOUND CAPTAIN'S EMERGENCY FLASHLIGHT SEAL BROKEN AND BATTERY EMPTY DUE LIGHT MOUNTED 180 DEGREES WRONG. REPLACED FLASHLIGHT AND BATTERY.
- [SDR DLL17954181](https://openairdocs.org/sdr/DLL17954181.md): Fitting · corroded · Oct 4, 1995 · N765DA · Lkheed 10113853 · Wing, Landing Gear Attach Fittings
  > THE LT MLG ATTACH FITTING WAS FOUND CORRODED ON THE UPPER FLANGE. DURING REMOVAL, FASTENER HOLES WERE FOUND OVERSIZED AND SPOT FACED IN ACCORDANCE WITH THE SRM. SOME REQUIRED SPOT FACING DEEPER THAN THE LIMIT ALLOWED IN THE SRM. REPAIR APPROVAL PER DL ERA 2
- [SDR DLL17954194](https://openairdocs.org/sdr/DLL17954194.md): Latch Fittings · corroded · Oct 3, 1995 · N765DA · Lkheed 10113853 · Cargo/Baggage Doors
  > THE NR 1 THROUGH NR 8 C-1A CARGO DOOR LATCH FITTINGS WERE FOUND WITH PITTING IN THE UPPER WELLS. DRAIN HOLES WILL BE DRILLED IN ALL EIGHT FITTINGS PER DL ERA 271881-14AD.
- [SDR DLL17954193](https://openairdocs.org/sdr/DLL17954193.md): Bulkhead · oversized holes · Oct 3, 1995 · N765DA · Lkheed 10113853 · Fuselage Main, Bulkhead
  > SEVERAL FASTENER HOLES BETWEEN STR 21 AND 22 WERE OVERSIZED TO A.25 DIAMETER. FASTENER REMOVAL ACCOMPLISHMENT OF EO 7-69959-12AD, REPAIRED PER DL ERA 271854-14AD.
- [SDR DLL17954192](https://openairdocs.org/sdr/DLL17954192.md): Door Sill · corroded · Oct 3, 1995 · N765DA · Lkheed 10113853 · Fuselage Miscellaneous Structure
  > THE LOWER DOOR SILL INBOARD CAP FITTINGS WERE FOUND CORRODED AND REQUIRED REPLACEMENT. REPAIRED PER DL ERA 271846-14.
- [SDR DLL17954191](https://openairdocs.org/sdr/DLL17954191.md): Longeron · cracked · Oct 3, 1995 · N765DA · Lkheed 10113853 · Fuselage Main, Longeron/Stringer
  > THE OUTER CAP ANGLE OF THE LT UPPER LONGERON IN THE FUSELAGE AFTER BODY AT STA 1860 WAS FOUND CRACKED IN THE RADIUS. REPAIRED PER DL ERA 271830-14.
- [SDR DLL17954190](https://openairdocs.org/sdr/DLL17954190.md): Angle · oversized holes · Oct 3, 1995 · N765DA · Lkheed 10113853 · Fuselage Miscellaneous Structure
  > SEVERAL FASTENERS IN THE BASE HOR FLANGE OF THE FAIL-SAFE ANGLE WERE FOUND TO BE OVERSIZED, WING TO FUSELAGE. REPAIRED PER DL ERA 271865-14 AD.
- [SDR DLL17954189](https://openairdocs.org/sdr/DLL17954189.md): Rear Spar · cracked · Oct 3, 1995 · N765DA · Lkheed 10113853 · Wing Spar
  > DURING THE ACCOMPLISHMENT OF EO 7-59089-3, CRACK INDICATIONS WERE FOUND EMANATING FROM TWO FASTENER HOLES COMMON TO THE UPPER WING SKIN AND THE UPPER SPAR CAP. ACCOMPLISHED REPAIRS PER DL ERA 271961-14AD.
- [SDR DLL17954188](https://openairdocs.org/sdr/DLL17954188.md): Angle · oversized hole · Oct 3, 1995 · N765DA · Lkheed 10113853 · Fuselage Miscellaneous Structure
  > DURING REMOVAL OF EXISTING FASTENERS AT RT 1203, THE UPPER FWD HOLE COMMON TO THE VERTICAL LEG OF THE FAIL-SAFE ANGLE, SKIN PANEL, FRAME FITTING, AND OVERWING TITANIUM TEE WAS OPENED TO.438. REPAIR APPROVAL PER DL ERA 271858-14AD.
- [SDR DLL17954184](https://openairdocs.org/sdr/DLL17954184.md): Attach Fitting · damaged · Oct 3, 1995 · N765DA · Lkheed 10113853 · Wing, Landing Gear Attach Fittings
  > TOOLING DAMAGE WAS INCURRED DURING RE-WORK TO AN INBOARD.6250 INCH FASTENER HOLE THROUGH THE RT MAIN LDG ATTACH FITTING. REPAIRED IAW DL ERA 271908-14 AD.
- [SDR DLL17954182](https://openairdocs.org/sdr/DLL17954182.md): Skin · short edge dist · Oct 3, 1995 · N765DA · Lkheed 10113853 · Fuselage Main, Plate/Skin
  > WHEN PICKING UP FASTENER LOCATIONS IN THE SKIN ATTACH FLANGE OF THE 1363 BULKHEAD CAP, NINE.25 INCH FASTENER HOLES ON BOTH THE LT AND RT SIDES WERE FOUND WITH SHORT EDGE DISTANCE ON THE FUSELAGE SKIN. REPAIRED IAW DL ERA 271825-14AD.
- [SDR DLL17954179](https://openairdocs.org/sdr/DLL17954179.md): Actuator Fitiing · damaged · Oct 3, 1995 · N765DA · Lkheed 10113853 · Landing Gear Actuator
  > THE LT AND RT WING MLG ACTUATOR SUPPORT FITTING HAD THREE FASTENERS, IPC 57-14-0 FIG 1 ITEMS 280, 285, 300 ENT. THESE VERE REPLACED WITH HLT 104 BOLTS PER SRM 57-14-00 FIG 803.
- [SDR DLL17953739](https://openairdocs.org/sdr/DLL17953739.md): Skin · dented · Sep 19, 1995 · N765DA · Lkheed 10113853 · Trailing Edge Flaps
  > AT HMV, LT WING NR 1 FLAP VANE WAS FOUND WITH DENTED SKIN ON INNER SKIN PANEL. INSTALLED REPAIR DOUBLERS PER SRM 51-50-01.
- [SDR DLL17953738](https://openairdocs.org/sdr/DLL17953738.md): Skin · damaged · Sep 19, 1995 · N765DA · Lkheed 10113853 · Trailing Edge Flaps
  > AT HMV, LT WING NR 1 FLAP VANE WAS FOUND WITH HEAVY WEAR DAMAGE TO OUTER SKIN AT THE INBD END OF VANE. REPAIRED PER SRM 57-53-00, FIG 805.
- [SDR DLL17953737](https://openairdocs.org/sdr/DLL17953737.md): Skin · cracked · Sep 19, 1995 · N765DA · Lkheed 10113853 · Trailing Edge Flaps
  > AT HMV, LEFT WING NR 1 FLAP VANE WAS FOUND WITH UPPER SKIN CRACKED ALONG A RIB AT 40 INCHES FROM INBD END. REPAIRED PER SRM 57-53-00.
- [SDR DLL17954038](https://openairdocs.org/sdr/DLL17954038.md): Fittings · corroded · Sep 14, 1995 · N765DA · Lkheed 10113853 · Fuselage Miscellaneous Structure
  > THE LOWER DOOR SILL I/B CAP FITTINGS AT FS 901 RT AND LT SIDES, WERE FOUND CORRODED AND REQUIRED REPLACEMENT. ACCOMPLISHED REPAIRS PER DL ERA 271846-14.
- [SDR DLL17954195](https://openairdocs.org/sdr/DLL17954195.md): Blkhd Skin · cracked · Sep 12, 1995 · N765DA · Lkheed 10113853 · Fuselage Main, Bulkhead
  > ON 8-9-91 CRACKS WERE DISCOVERED IN THE FS 328 CANTED BULKHEAD STRUCTURE DURING HMV. THIS DAMAGE WAS REPAIRED BY LAC DWG 1646545 PER ER/A 226719-14. AFTER THAT, EO 7-53207-3AD WAS ISSUED TO REINFORCE THE FS 328 CANTED BULKHEAD STRUCTURE FOR ALL DAL L1011'S,
- [SDR DLL17954037](https://openairdocs.org/sdr/DLL17954037.md): Longeron · cracked · Sep 12, 1995 · N765DA · Lkheed 10113853 · Fuselage Main, Longeron/Stringer
  > FUSELAGE, AFTERBODY, LLT LONGERON ASSY FS 1860 WL 328.942, REPAIR OF CRACKED LONGERON. THE OUTER CAP ANGLE OF THE LT UPPER LONGERON IN THE FUSELAGE AFTERBODY AT APPROX FS 1860 AND WL 328, WAS FOUND CRACKED IN THE RADIUS. THE CRACK EXTENDS FROM THE AFT END OF
- [SDR DLL17953782](https://openairdocs.org/sdr/DLL17953782.md): Frame · cracked · Sep 8, 1995 · N765DA · Lkheed 10113853 · Fuselage Main, Frame
  > DURING HMV, 1363 BULKHEAD FRAME AT APPROX WL 160 ON RT SIDE IS CRACKED AT THE SECOND FASTENER FROM BOTTOM FWD ROW. INSTALLED REPAIR AS PER SRM 53-11-00 FIG 843.
- [SDR DLL17953723](https://openairdocs.org/sdr/DLL17953723.md): Floorbeam · corroded · Sep 7, 1995 · N765DA · Lkheed 10113853 · Fuselage Main, Floor Beam
  > DURING HMV, UPPER SURFACE OF FLOORBEAM AND SUPPORT ANGLE CORRODED AT FS 846 AT RBL 40. REPAIRED PER SRM 53-21-00 PG 849 TO 852.
- [SDR DLL17953707](https://openairdocs.org/sdr/DLL17953707.md): Floorbeam · corroded · Sep 7, 1995 · N765DA · Lkheed 10113853 · Fuselage Main, Floor Beam
  > DURING HMV, FS 901 FLOOR SUPPORT BEAM CORRODED AT LBL 49, 60, AND RBL 49, 70. REPLACED BEAM CAP PER SRM 53-21-00 PG 849 TO 852.
- [SDR DLL17953692](https://openairdocs.org/sdr/DLL17953692.md): Cowl · worn · Sep 3, 1995 · N765DA · Lkheed 10113853 · Engine Cowling System
  > AT HMV, NR 2 ENGINE RT COWL PANEL WAS FOUND WITH WEAR DAMAGE AT LOWER FORWARD CORNER OF PANEL. ACCOMPLISHED REPAIRS PER SRM 51-50-01, FIG 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 = 'N765DA' AND deregistration_id = 'N765DA-2001-04-23'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N765DA-2001-04-23/reports

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