# Service difficulty reports: N316DL, cancelled Aug 6, 2007

A list on [N316DL, cancelled Aug 6, 2007](https://openairdocs.org/deregistered/N316DL-2007-08-06.md).

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

- [SDR DL73S050276](https://openairdocs.org/sdr/DL73S050276.md): Actuator · sticking · May 17, 2005 · N316DL · Boeing 737232 · Engine Thrust Reverser
  > NR 2 ENGINE THRUST REVERSER UNLOCKED LIGHT ON DURING TAKEOFF ROLL. CLEANED LOWER ACTUATOR FOR STICKING.
- [SDR DL73S041053](https://openairdocs.org/sdr/DL73S041053.md): Skin · cracked · Nov 20, 2004 · N316DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN AND UNDERLYING BEARSTRAP WERE FOUND CRACKED AT THE LOWER FWD CORNER OF THE R2 DOOR CUTOUT. THE CRACK WAS REMOVED WITH A 2.5 INCH CUTOUT IN THE SKIN AND BEARSTRAP. THE TRIMOUT WAS REPAIRED WITH 3 EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 39
- [SDR DL73S040503](https://openairdocs.org/sdr/DL73S040503.md): Frame · corroded · Jun 2, 2004 · N316DL · Boeing 737232 · Fuselage Main, Frame
  > FOUND ON W-2 LETTER CHECK CORROSION LOWER FRAME INBOARD OF STR 27L AT STA 1006. REPAIRED PER SRM 53-10-4 FIG 10.
- [SDR DL73S040500](https://openairdocs.org/sdr/DL73S040500.md): Stringer · corroded · Jun 2, 2004 · N316DL · Boeing 737232 · Fuselage Main, Longeron/Stringer
  > FOUND ON W-2 LETTER CHECK STRINGER 27 LEFT CORRODED STA 967-1006. REPAIRED PER SRM 53-10-3 FIG 1.
- [SDR DL73S040349](https://openairdocs.org/sdr/DL73S040349.md): Power Supply · failed · Apr 17, 2004 · N316DL · Boeing 737232 · Emergency Lighting
  > EMERGENCY INSEAT LIGHTING SEATS 21-24 INOP. REPLACED FUSE IN PWR SUPPLY M9013. CHECKS OK.
- [SDR DL73S040197](https://openairdocs.org/sdr/DL73S040197.md): Power Supply · inoperative · Feb 27, 2004 · N316DL · Boeing 737232 · Emergency Lighting
  > EMERGENCY PATH LIGHTS AT ROWS 22-25D INOP. REMOVED AND REPLACED POWER SUPPLY.
- [SDR DL73S030883](https://openairdocs.org/sdr/DL73S030883.md): Control Panel · smoke · Sep 28, 2003 · N316DL · Boeing 737232 · Airfoil Anti/De-ice System
  > PRIOR TO PUSHBACK FLT 1111 CREW SMELLED ELEC BURNING ODOR IN COCKPIT THEN NOTICED SMOKE COMING FRM F/O EYEBROW WINDOW AREA. FOUND SMOKE TO COMING FROM ENG/WING ANTI-ICE PANEL. REPLACED PANEL.
- [SDR DL73S030747](https://openairdocs.org/sdr/DL73S030747.md): Wire · inoperative · Aug 12, 2003 · N316DL · Boeing 737232 · Light System Wiring
  > SEAT MOUNTED EMERGENCY LIGHTS INOPERATIVE AT ROWS 18-21. REPAIRED WIRING NOW OPS, NORMAL.
- [SDR DL73K011465](https://openairdocs.org/sdr/DL73K011465.md): Warning System · malfunctioned · Sep 1, 2001 · N316DL · Boeing 737232 · Landing Gear Brake System
  > UPON INITIAL T/O ROLL EWR, AUTOBRAKE DISARM LIGHT ILLUMINATED. CYCLED RTO SWITCH AND THE AUTOBRAKE LIGHT ILLUMINATED AGAIN. PERFORMED AUTOBRAKE TEST PER M/M. UNABLE TO DUPLICATE.
- [SDR DL73K011458](https://openairdocs.org/sdr/DL73K011458.md): Autothrust Sys · malfunctioned · Sep 1, 2001 · N316DL · Boeing 737232 · Auto Throttle System
  > T/O ROLL NOTICED ENGINE PARAMETERS FLUCTUATING. T/O ABORTED AUTOTHROTTLES WERE ENGAGED. MAINT OPERATED ENGS AT T/O PWR PER PFHB WITH OUT AUTOTHROTTLES ALL PARAMETERS CK NML. RAN ENGS AT T/O PWR AGAIN WITH AUTOTHROTTLES ENGAGED PER PFHB - NTF
- [SDR DL73K011184](https://openairdocs.org/sdr/DL73K011184.md): Air Duct · leaking · Jul 17, 2001 · N316DL · Boeing 737232 · Air Distribution System
  > FUMES IN CABIN AND COCKPIT. STRONGEST SMELL IN FIRST 5 ROWS OR SO. SMELLED LIKE RUBBER BURNING. NOTICED AT 2500 FT ABOUT 2 MINUTES AFTER DEPARTURE. FOUND GASPER AIR DUCT LEAKING AND RETAPED.
- [SDR DL73K010678](https://openairdocs.org/sdr/DL73K010678.md): Heater · faulty · Apr 26, 2001 · N316DL · Boeing 737232 · Potable Water System
  > A/C DIVERTED TO CHS.SMOKE /ELECTRICAL SMELL IN AFT LAV/GALLEY FOLLOWED POM. PULLED C/B SMELL DISIPATED. FOUND SOURCE TO BE AFT LAV WATER HEATER
- [SDR DL73K010587](https://openairdocs.org/sdr/DL73K010587.md): Stringer · corroded · Apr 10, 2001 · N316DL · Boeing 737232 · Fuselage Main, Longeron/Stringer
  > CORROSION WAS FOUND ON STR 26 RT AT APPROXIMATLEY FS 500+12. THE AFTMOST END OF THE STRINGER WAS CUT OFF AND A NEW SECTION WAS SPLICED IN. THE CORROSION WAS FOUND AT HMV.
- [SDR DL73K010584](https://openairdocs.org/sdr/DL73K010584.md): Frame · corroded · Apr 9, 2001 · N316DL · Boeing 737232 · Fuselage Main, Frame
  > LOWER LOBE FRAME AT FS 500 WAS FOUND CORRODED AT THE INBD FLANGE BETWEEN STR 25R/26R. THE FLANGE WAS CUT OUT AND A REPAIR ANGLE INSTALLED. THE DAMAGE WAS FOUND AT HMV.
- [SDR DL73K010583](https://openairdocs.org/sdr/DL73K010583.md): Bulkhead · corroded · Apr 9, 2001 · N316DL · Boeing 737232 · Fuselage Main, Bulkhead
  > CORROSION WAS FOUND ON THE BS 1016 PRESSURE BULKHEAD WEB AT BL 0. REPAIR WAS ACCOMPLISHED PER S/B 737-53A1075. THE DAMAGE WAS FOUND DURING HMV.
- [SDR DL73K010582](https://openairdocs.org/sdr/DL73K010582.md): Skin · corroded · Apr 9, 2001 · N316DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > CORROSION WAS FOUND IN THE FUSELAGE SKIN AND BEAR STRAP AT FS 490 BETWEEN STR 27R/28R. THE DAMAGE WAS CUT OUT AND A REPAIR DOUBLER INSTALLED. THE DAMAGE WAS FOUND AT HMV.
- [SDR DL73K010556](https://openairdocs.org/sdr/DL73K010556.md): Frame · cracked · Apr 4, 2001 · N316DL · Boeing 737232 · Fuselage Main, Frame
  > A CRACK WAS FOUND IN THE FS 492 FRAME AT STR 24 RT IN THE FLANGE. THE LENGTH OF THE CRACK IS 2.05 INCHES. THE CRACK WAS CUTOUT AND A REPAIR WAS INSTALLED PER SRM 51-40-3. THE DAMAGE WAS FOUND AT HMV.
- [SDR DL73K010535](https://openairdocs.org/sdr/DL73K010535.md): Strap · cracked · Apr 2, 2001 · N316DL · Boeing 737232 · Fuselage, Stabilizer Attach Fittings
  > CRACKS WERE FOUND AT THE CUTOUT IN THE FUSELAGE FOR THE HORIZONTAL STABILIZER SIMILIAR TO THE TYPICAL CRACKS OF S/B 737-53-1134. CRACKS WERE FOUND IN THE LT & RT STINGER 12 STRAP, FS 1140, AND THE LT & RT FS 1138 FRAME STRAPS. THE DAMAGE WAS REPAIRED PER SR
- [SDR DL73K010534](https://openairdocs.org/sdr/DL73K010534.md): Fitting · corroded · Apr 2, 2001 · N316DL · Boeing 737232 · Horizontal Stabilizer, Attach Fittings
  > CORROSION WAS FOUND ON THE LT AND RT HORIZONTAL STABILIZER ATTACH FITTINGS ON BOTH THE BORES AND FACES. THE CORROSION WAS REMOVED AND NEW BUSHINGS INSTALLED PER 397372-14 AT HMV.
- [SDR DL73K010533](https://openairdocs.org/sdr/DL73K010533.md): Fitting · corroded · Apr 2, 2001 · N316DL · Boeing 737232 · Fuselage, Stabilizer Attach Fittings
  > CORROSION WAS FOUND IN THE BORE AND FACES OF THE LT AND RT FUSELAGE CLEVIS LUGS FOR THE HORIZONTAL STABILIZER. THE CORROSION WAS REMOVED AND NEW BUSHINGS WERE INSTALLED PER ERA 397371-14AD AT HMV.
- [SDR DL73K010532](https://openairdocs.org/sdr/DL73K010532.md): Fitting · corroded · Apr 2, 2001 · N316DL · Boeing 737232 · Fuselage, Landing Gear Attach Fittings
  > THE LT MLG STRUT SUPPORT FITTING FRAME INSTALLATION HAD CORROSION LOCATED IN THE BORE. THE FITTING IS LOCATED AT FS 695, LBL 68.5 AND WL 188.5. THE CORROSION WAS REMOVED AND A REPAIR SLEEVE INSTALLED. THE DAMAGE WAS FOUND AT HMV.
- [SDR DL73K010519](https://openairdocs.org/sdr/DL73K010519.md): Attach Fitting · corroded · Mar 30, 2001 · N316DL · Boeing 737232 · Fuselage, Landing Gear Attach Fittings
  > THE LT MLG STRUT SUPPORT FITTING FRAME AT FS 685 HAD CORROSION AT THE SIDE STRUT ATTACH LUG LOCATED AT LBL 68.5 AND WL 188.5. CORROSION WAS FOUND IN THE BORE AND BOTH FACES. CORROSION WAS REMOVED AND A REPAIR SLEEVE INSTALLED.THE DAMAGE WAS FOUND AT HMV.
- [SDR DL73K010500](https://openairdocs.org/sdr/DL73K010500.md): Fitting · corroded · Mar 27, 2001 · N316DL · Boeing 737232 · Wing, Landing Gear Attach Fittings
  > CORROSION WAS FOUND IN A FASTENER HOLE OF THE UPPER ROW COMMON TO THE REAR SPAR UPPER CAP OF THE MLG SUPPORT BEAM O/B AFT FITTING. ANOTHER FASTENER HOLE WAS MISDRILLED WHILE REPLACING THE AFT FITTING. THE FASTENER HOLES WERE OVERSIZED AND BUSHED PER ERA 3973
- [SDR DL73K010460](https://openairdocs.org/sdr/DL73K010460.md): Bearing · worn · Mar 17, 2001 · N316DL · Boeing 737232 · Horizontal Stabilizer Structure
  > WHILE PERFORMING JIC5957 FOUND PIVOT BEARING PLAY TO BE OUT OF LIMITS. IN THE PROCCESS OF REMOVING BEARING HOUSING FOUND SAFETY WIRE BROKEN AND KEEPER BACKED OFF APROX 1/4 INCH
- [SDR DL73K002529](https://openairdocs.org/sdr/DL73K002529.md): Accessory Unit · failed · Dec 25, 2000 · N316DL · Boeing 737232 · Landing Gear Position and Warning
  > AT TOP OF DESCENT - ISOLATION VALVE LIGHT ILLUMINATED - THEN AFTER PLACING GEAR DOWN HAD NO GEAR LIGHTS RED OR GREEN. VISUALY CHECKED GEAR DOWN AND FOUND GEAR LIGHT C/B OUT. REPLACED LANDING GEAR ACCESSORY UNIT PER M/M
- [SDR DL73K001144](https://openairdocs.org/sdr/DL73K001144.md): Beam · cracked · Jun 13, 2000 · N316DL · Boeing 737232 · Fuselage Main, Structure
  > A CRACK WAS FOUND IN THE RT S18A SHEAR BEAM WEB AT BS 727. SUBJECT CRACK IS TYPICAL OF THOSE DEPICTED IN S/B 737-53-1066. THE CRACK IS LOCATED AT THE AFT, I/B MOST FASTENER LOCATION. THE SUBJECT SB IS NOT EFFECTIVE FOR AC 316. DAMAGE REPAIRED PER ERA 377513
- [SDR DL73K000586](https://openairdocs.org/sdr/DL73K000586.md): Wire · pinched · Mar 27, 2000 · N316DL · Boeing 737232 · Light System Wiring
  > ON L/O, FOUND AISLE EMERGENCY EXIT LIGHTS INOP FWD OF WING. REPAIRED WIRING.
- [SDR DL73K991508](https://openairdocs.org/sdr/DL73K991508.md): Battery Pack · discharged · Jul 3, 1999 · N316DL · Boeing 737232 · Emergency Lighting
  > EMERGENCY LIGHTS AT ROWS 4, 6, 8 ABC OVERHEAD FAILED TO LIGHT ON TEST. REPLACED BATTERY PACK.
- [SDR DL73K991445](https://openairdocs.org/sdr/DL73K991445.md): Coffeemaker · failed · Jun 27, 1999 · N316DL · Boeing 737232 · Buffet/Galleys
  > AFT GALLEY NR 2 COFFEEMAKER WHEN TURNED ON CAUSES SMELL OF HOT ELEC WIRES. INSPECTED CANNON PLUG, CKS OK. REPLACED COFFEEMAKER.
- [SDR DL73K990514](https://openairdocs.org/sdr/DL73K990514.md): Lights · odor · Mar 11, 1999 · N316DL · Boeing 737232 · Passenger Compartment Lighting
  > 2L AFT GALLEY HAS ELECTRIC SMELL WHEN GALLEY LIGHTS ON. INSP AFT GALLEY FLUORESCENT LIGHTS AND WIRING, NO SIGNS OF BURNED WIRING. DEACTIVATED THRESHOLD AND WORK LIGHTS IN AFT GALLEY C/B PULLED AND COLLARD BEHIND CAPTS SEAT.
- [SDR DL73K990504](https://openairdocs.org/sdr/DL73K990504.md): Coffeemaker · malfunctioned · Mar 10, 1999 · N316DL · Boeing 737232 · Buffet/Galleys
  > DISCONTINUED TAKEOFF DUE TO ELECTRICAL ODOR IN AFT GALLEY. F/A REPORTED C/B PANEL WARM TO TOUCH. TURNED OFF GALLEY PWR AND RETURNED TO GATE. INSPECTED AFT GALLEY C/B PANEL AND WIRING, REPLACED BOTH COFFEEMAKERS AS A PRECAUTION. ALSO, CLEANED COFFEE RESIDUE
- [SDR DL73K982593](https://openairdocs.org/sdr/DL73K982593.md): Floorbeam · cracked · Dec 16, 1998 · N316DL · Boeing 737232 · Fuselage Main, Floor Beam
  > FUSELAGE OVERWING FLOORBEAM, UPPER CAP BL 0 FS 66, REPAIR FOR CRACKED CAP. THE OVERWING FLOORBEAM AT BL 0 WAS FOUND WITH A SEVERED UPPER CAP AT FS 662 WITH AN ADDITIONAL CRACK IN THE CAP AT FS 666. THE UPPER CAP WAS REPAIRED PER THE GUIDELINES OF BAC S/B
- [SDR DL73K982268](https://openairdocs.org/sdr/DL73K982268.md): Hinge · cracked · Nov 3, 1998 · N316DL · Boeing 737232 · Galley Doors
  > THE LOWER GATE HINGE ON THE R1 DOOR WAS FOUND CRACKED. THE CRACKED HINGE WAS REMOVED AND REPLACED PER THE REQUIREMENTS OF BAC S/B 737-52A1124. THE REPAIR WAS DOCUMENTED PER ER/A 366007-14AD.
- [SDR DL73K982264](https://openairdocs.org/sdr/DL73K982264.md): Skin · cracked · Nov 2, 1998 · N316DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN AT FS 740 WAS FOUND WITH A 1.25 INCH LONG CRACK BELOW STRINGER 18R. THE CRACK WAS REPAIRED PER THE B737-200 SRM 53-30-3 FIG 1. THE REPAIR DOUBLER EXTENDS UNDER THE WING TO BODY FAIRING, SO INFRINGES ON SSI F-41. THE REPAIR HAS BEEN DOCUMEN
- [SDR DL73K981793](https://openairdocs.org/sdr/DL73K981793.md): Power Supply · inoperative · Aug 29, 1998 · N316DL · Boeing 737232 · Emergency Lighting
  > MID PATH LIGHTS INOP. REPLACED POWER SUPPLY.
- [SDR DL73K981358](https://openairdocs.org/sdr/DL73K981358.md): Skin · cracked · Jun 27, 1998 · N316DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > THE SKIN ASSY AT THE LOWER FWD CORNER OF THE AFT ENTRY DOOR WAS FOUND WITH A TYPICAL CRACK THROUGH THE SKIN, DOUBLER, AND BEAR STRAP. THE CRACK WAS REPAIRED PER B737 SRM 53-30-3 FIG 24 EXCEPT BLIND FASTENERS WERE AUTHORIZED ON A TEMPORARY BASIS. THE REPAIR W
- [SDR DL73K980843](https://openairdocs.org/sdr/DL73K980843.md): Fuse · blown · Apr 18, 1998 · N316DL · Boeing 737232 · Emergency Lighting
  > ON SERVICE CK DURING TEST OF EMERGENCY LIGHT SYTEM, FOUND AFT SECTION OF SEAT LIGHTS INOP. FOUND BLOWN FUSE ON PWR SUPPLY CKD FOR SHORTS, NONE FOUND. REPLACED PWR SUPPLY LIGHTS, CK NORMAL.
- [SDR DL73K970929](https://openairdocs.org/sdr/DL73K970929.md): Floorbeam · corroded · May 15, 1997 · N316DL · Boeing 737232 · Fuselage Main, Floor Beam
  > FLOORBEAM T-CAP FS 328 CORRODED AT LBL 27 AND FROM RBL12 TO RT SIDE OF FUSELAGE, C53-107-02. REMOVED ALL HARDWARE FROM DAMAGED BEAM SECTION. COMPLETED REMOVING DAMAGED SECTION. DRILLED REPAIR PARTS AND BEGAN INSTALLING REPAIR AND REPLACEMENT T-CAP PER M/M 5
- [SDR DL73K970902](https://openairdocs.org/sdr/DL73K970902.md): Floorbeam · corroded · May 5, 1997 · N316DL · Boeing 737232 · Fuselage Main, Floor Beam
  > AT MIDVISIT, THE FLOORBEAM T-CAP WAS FOUND TO BE CORRODED SEVERAL PLACES, LBL 7 TO RBL O/B END. THE CORROSION WAS REMOVED PER SRM 51-10-6, ALL OUT OF LIMITS EXCEPT RBL 48. DAMAGED SECTION REMOVED AND REPAIR PARTS AND REPLACED T-CAP, DRILLED AND INSTALLED PER
- [SDR DL73K970231](https://openairdocs.org/sdr/DL73K970231.md): Solenoid · failed · Feb 6, 1997 · N316DL · Boeing 737232 · Passenger Oxygen System
  > ON OXYGEN SYSTEM TEST ROW 14ABC OXYGEN DOOR DID NOT OPEN. REPLACED DOOR LATCH ACTUATOR SOLENOID.
- [SDR DL73K962459](https://openairdocs.org/sdr/DL73K962459.md): Bulkhead · cracked · Oct 16, 1996 · N316DL · Boeing 737232 · Fuselage Main, Bulkhead
  > STATION 178 BULKHEAD WAS FOUND CRACKED IN SEVERAL LOCATIONS. DAMAGE CUTOUTS ARE 1 INCH X 2 INCH AT RBL 4, WL 200 AND WL 203, AND LBL 4, WL 200, AND A 1 INCH BY 1 INCH AT RBL 7 WL 200. IN ADDITION TO THE WEB CRACKS, THE VERTICAL CHORD HAS A.50 INCH CRACK AT
- [SDR DL73S961054](https://openairdocs.org/sdr/DL73S961054.md): Water Separator · contaminated · May 2, 1996 · N316DL · Boeing 737232 · Humidity Control System
  > AFTER TAKEOFF, CVG UNABLE TO PRESSURIZE. OUTFLOW VALVE WAS FULL, CLOSED BOTH BLEEDS, AND LT PACK WERE ON AS WAS ISOLATION VALVE. OPEN CBS WERE ALL IN CABIN CLIMBED AND DESCENTED WITH THE A/C. REPLACED RT PACK WATER SEPARATOR BAG.
- [SDR DL73S954724](https://openairdocs.org/sdr/DL73S954724.md): Skin · cracked · Dec 16, 1995 · N316DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > THE R-2 DOOR HAS A 1.3 INCH CRACK AT THE LOWER AFT CORNER. IT WILL BE REPAIRED PER THE SRM WITH THE EXCEPTION OF BLIND FASTENER SUBSTITUTION TO FACILITATE MAINTENANCE IN MEETING THE LETTER CHECK TIME LIMIT REQUIREMENTS PER DL ERA 302921-14.
- [SDR DL73S953871](https://openairdocs.org/sdr/DL73S953871.md): Eel Bulb · failed · Oct 1, 1995 · N316DL · Boeing 737232 · Emergency Lighting
  > FOUND EMERGENCY AISLE LIGHT INOP AT 21ABC. RELAMPED, CKS GOOD.
- [SDR DL73S953870](https://openairdocs.org/sdr/DL73S953870.md): Eel Battery Pack · discharged · Oct 1, 1995 · N316DL · Boeing 737232 · Emergency Lighting
  > EMERGENCY LIGHTS ON LEFT HAND AFT DOOR ARE INOP. REPLACED BATTERY PACK, CKS GOOD.
- [SDR DL73S951971](https://openairdocs.org/sdr/DL73S951971.md): Le Skin · dented · May 1, 1995 · N316DL · Boeing 737232 · Vertical Stabilizer, Plate/Skin
  > DURING SHOP INSPECTION, VERTICAL STABILIZER LEADING EDGE PANEL WAS REPAIRED FOR A DENT AT 51 INCHES FROM THE LOWER END OF PANEL. DAMAGE WAS REPAIRED PER SRM 55-30-6.

## 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 = 'N316DL' AND deregistration_id = 'N316DL-2007-08-06'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N316DL-2007-08-06/reports

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