# Service difficulty reports: N672MC, cancelled Feb 27, 2013

A list on [N672MC, cancelled Feb 27, 2013](https://openairdocs.org/deregistered/N672MC-2013-02-27.md).

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

- [SDR HALA0000247](https://openairdocs.org/sdr/HALA0000247.md): Spring · broken · Aug 4, 2000 · N672MC · Doug DC951 · Landing Gear Steering System
  > FLT 153 - HNL - HEARD LOUD BANG/THUMP FROM NOSE WHEEL WELL AREA. RETURNED TO HNL WHERE AND UNEVETFUL LANDING WAS MADE. FOUND RIGHT NLG BUNGEE SPRING BROKEN. REPLACED SPRING PER MM 32-21-3. INSPECTED NLG WHEEL WELL, CONDITION AND SECURITY CHECK OK. OK FOR
- [SDR HALA0000239](https://openairdocs.org/sdr/HALA0000239.md): Pulley · broken · Jul 23, 2000 · N672MC · Doug DC951 · Leading Edge Slat Control System
  > HNL - FLT 347 - ON APPROACH AT FLAPS 5 DEGREES SELECTION, 'SLAT DISAGREEMENT' LIGHT CAME ON. PERFORMED SLAT DISAGREEMENT PROCEDURE AND LANDED IN KOA. ON DEPARTURE OUT AT APPROX 180 KNOTS AT FLAPS 15, BLUE SLAT LIGHT WENT OUT AND 'SLAT DISAGREE' ANNUNCIATOR
- [SDR HALA0000159](https://openairdocs.org/sdr/HALA0000159.md): Computer · failed · Jun 4, 2000 · N672MC · Doug DC951 · Autopilot Computer
  > FLT 197 - HNL - AIRCRAFT MADE UNCOMMANDED ROLL TO RIGHT AT TOP OF DESCENT WITH AUTOPILOT ENGAGED. TURN KNOB IS WINGS LEVEL DETENT NAV SELECTOR IN TURN KNOB MODE. ALSO, VOR COURSE WAS COMING ALIVE AT SAME TIME, ALTHOUGH NAV/LOC WAS NOT SELECTED. REPLACED ROL
- [SDR HALA0000062](https://openairdocs.org/sdr/HALA0000062.md): Screw · loose · Mar 2, 2000 · N672MC · Doug DC951 · Stabilizer Control System
  > HNL - FLT 362 - PRIMARY PITCH TRIM FAILED ON CLIMB-OUT, OVERTEMP. SWAPPED TO A/C 59. MAINTENANCE TIGHTENED LOOSE SCREW ON PRIMARY TRIM BRAKE SWITCH. OPERATIONAL CHECK OK. (M)
- [SDR HALA0000005](https://openairdocs.org/sdr/HALA0000005.md): Blade · cracked · Jan 1, 2000 · N672MC · Doug DC951 · Turbine Engine Compressor Section
  > HNL - FLT 181 - NR 1 ENGINE HAD COMPRESSOR STALL UPON THROTTLE ADVANCE FOR PARKING. FOUND NR 10 COMPRESSURE BLADE CRACK AT C-1 FAN HUB. REMOVED NR 1 ENGINE ASSY PER HAL M144. (X)
- [SDR HALA000004](https://openairdocs.org/sdr/HALA000004.md): Connector · failed · Dec 30, 1999 · N672MC · Doug DC951 · Fire Detection
  > HNL - MAINTENANCE ENTRY: NR 2 ENGINE FIRE B-LOOP INOPERABLE. OK TO CONTINUE PER MEL 26-1-1. MPCW ON OVERNIGHT REPLACED NR 2 ENGINE B-LOOP PYLON ELEMENT CONNECTOR. OPS CHECK OK. (X)
- [SDR HALA9900245](https://openairdocs.org/sdr/HALA9900245.md): Sensor · malfunctioned · Nov 24, 1999 · N672MC · Doug DC951 · Cabin Pressure Control System
  > HNL - FLT 515 - CABIN PRESSURE CONTROL, ON TAKEOFF, CABIN DESCENDS 1800 FEET/MINUTE (PEGS OUT). THEN CLIMBS 500 FEET/MINUTE. THEN OSCILATES IN CLIMB 200-800 FEET/MINUTE. ON DESCENT, CABIN CLIMBS 500 FEET/MINUTE, THEN DOWN 1,000 FEET/MINUTE. REPLACED DIFFERE
- [SDR HALA0000172](https://openairdocs.org/sdr/HALA0000172.md): Actuator · failed · Aug 29, 1999 · N672MC · Doug DC951 · Landing Gear Retraction/Extension System
  > FLT 162 - HNL - NOSE LANDING GEAR WOULD NOT EXTEND. CYCLED THREE TIMES. PULLED ALTERNATE GEAR EXTENSION LEVER, NOSE GEAR EXTENDED WITH NORMAL INDICATIONS. STOWED ALT LEVER. CHECKED NOSE GEAR COND AND SERVICE CHECK OK. REPLACED NOSE GEAR BUNGEE CYL PER MM
- [SDR HALA9900158](https://openairdocs.org/sdr/HALA9900158.md): Proximity Box · malfunctioned · Aug 6, 1999 · N672MC · Doug DC951 · Landing Gear Position and Warning
  > HNL - FLT 103 - NOSE GEAR UNSAFE LIGHT WOULD NOT EXTINGUISH WITH GEAR UP POSITION. LOCK DOWN OK. LIGHT GOES OUT WITH GEAR DOWN. REPLACED NOSE GEAR SENSOR AND CONDUIT. REPLACED PROXIMITY SWITCH BOX. SWUNG GEAR SEVERAL TIMES. OPS CHECK OK. (X)
- [SDR HALA9900117](https://openairdocs.org/sdr/HALA9900117.md): Connector · failed · May 20, 1999 · N672MC · Doug DC951 · Leading Edge Slat Position Indicating System
  > HNL - FLT 208 - SLAT DISAGREE LIGHT STAYS ON WHEN SLATS ARE EXTENDED. REPLACED NR 6 PIN ON RIGHT EXTEND SWITCH CANNON PLUG. OPS CHECK ON GROUND GOOD. (M)
- [SDR HALA9900106](https://openairdocs.org/sdr/HALA9900106.md): Altimeter · malfunctioned · May 2, 1999 · N672MC · Doug DC951 · Altimeter, Barometric/Encoder
  > HNL - DURING CLIMB, EXPERIENCED LARGER AND LARGER A/S DEVIATIONS FROM RIGHT AND LEFT A/S INDICATORS, TCAS FAIL FLAG AND ALTITUDE VARIATIONS, LOSS OF MODE C AND R ALTIMETER WENT INTO BARO MODE. REPLACED FIRST OFFICERS ALTIMETER FOR EXCESSIVE LEAK STATIC SYSTEM
- [SDR HALA9900021](https://openairdocs.org/sdr/HALA9900021.md): Acm · malfunctioned · Jan 18, 1999 · N672MC · Doug DC951 · Cabin Cooling System
  > HNL - FLT 202 - TAIL COMPARTMENT HIGH TEMP LIGHT ON. ISOLATED TO RT PACK. REPLACED RT ACM, OPS AND LEAK CHECK OK. (M)
- [SDR HALA9900020](https://openairdocs.org/sdr/HALA9900020.md): Motor · failed · Jan 17, 1999 · N672MC · Doug DC951 · Stabilizer Control System
  > HNL - FLT 103 - PRIMARY STAB TRIM INOPERATIVE. WILL NOT MOVE WITH SUITCASE HANDLE OR EITHER CNTL WHEEL SWITCHES. ALT TRIM APPEARS TO BE NORMAL. (M)
- [SDR HALA9800393](https://openairdocs.org/sdr/HALA9800393.md): Handle · not secured · Nov 20, 1998 · N672MC · Doug DC951 · Electrical/Electronic Compartment Doors
  > FLT 195 - HNL - VIBRATION STARTED IN CRUISE AND IS MOST NOTICED IN STEERING TILLER. FOUND E/E COMPARTMENT DOOR HANDLE NOT PROPERLY SECURED. RESECURED E/E, COMPARTMENT DOOR. INSPECTED NOSE GEAR CONDITION AND SECURITY FOUND FLIGHT BRAKES ARE WORN. REPLACED F
- [SDR HALA9800332](https://openairdocs.org/sdr/HALA9800332.md): Accumulator · malfunctioned · Sep 23, 1998 · N672MC · Doug DC951 · Hydraulic Power Accumulator, Main
  > FLT 167 - HNL - WITH AUX HYD PUJP OFF AND SELECTING RIGHT ENGINE HYD SYSTEM PRESSURE DROPS RAPIDLY TO BELOW 1500 PSI, THEN SLOWLY CONTINUES DOWN. INSPECTED RIGHT HYD SYSTEM ACCUMULATOR OPS AND LEAK CHECK GOOD. FOUND RIGHT HYD SYSTEM ACCUMULATOR CORRODED. (M
- [SDR HALA9800283](https://openairdocs.org/sdr/HALA9800283.md): Battery · discharged · Aug 15, 1998 · N672MC · Doug DC951 · Emergency Lighting
  > HNL - CABIN FLOOR EMERGENCY LIGHTS INOP. REMOVED AND REPLACED CABIN FLOOR EMERGENCY LIGHT BATTER POWER SUPPLY, OPS CHECK GOOD. (M)
- [SDR HALA9800118](https://openairdocs.org/sdr/HALA9800118.md): Light · inoperative · May 4, 1998 · N672MC · Doug DC951 · Emergency Lighting
  > SBA - TEST FLIGHT - EMERGENCY LIGHTS ABOVE JUMP SEAT ARE INOPERATIVE. RE-LAMPED AND OPS CHECK OK IAW MM 33-50-00. (X)
- [SDR HALA9800117](https://openairdocs.org/sdr/HALA9800117.md): Bracket · out of adjust · May 4, 1998 · N672MC · Doug DC951 · Landing Gear Position and Warning
  > SBA - TEST FLIGHT - (LOG PAGE 18N00688). NLG UNSAFE LIGHT STAYS ON WITH GEAR RETRACTED. ADJUSTED NOSE LANDING GEAR POSITION INDICATION BRACKETS AND TESTED GOOD IAW MM 32-60-0, PAGE 201 TO PAGE 203. (X)
- [SDR HALA9800108](https://openairdocs.org/sdr/HALA9800108.md): Hat Channel · corrosion · Apr 15, 1998 · N672MC · Doug DC951 · Fuselage Main, Bulkhead
  > STATION 1292 RT AFT FACE CANTED BLKHD 3RD STIFFENER (HAT CHANNEL) UP IN VENT BOX AREA LEVEL 2 CORROSION. REMOVED HAT CHANNEL FABRICATED REPLACEMENT HAT CHANNEL PER SRM 51-10-2, INSTALLED PER SRM 51-30-2. (M)
- [SDR HALA9800107](https://openairdocs.org/sdr/HALA9800107.md): Pan · crack · Apr 15, 1998 · N672MC · Doug DC951 · Cargo/Baggage Doors
  > FORWARD CARGO DOOR OUTER PAN RADIUS HAS 1 INCH CRACK BOTTOM END OF DOOR. LOCATED AND FABRICATED 7 DOUBLER STOP DRILLED CRACK AND PRIMED PER SRM 51-10-3, 52-03 FIG 8 SHT 2, AND INSTALLED PER 51-30-2. (M)
- [SDR HALA9800106](https://openairdocs.org/sdr/HALA9800106.md): Tip Fairing · corroded · Apr 15, 1998 · N672MC · Doug DC951 · Vertical Stabilizer
  > VERT STABILIZER AFT TIP FAIRING AREA LOWER WEB, DIRECTLY ABOVE TOP OF RUDDER) HAS CORROSION AT SEVERAL SIGHTS, FORWARD MOST AREA 10 INCH BY 8 INCH, LOCATION 2V113 FROM 8 INCH AFT OF AFT SPAR TO 48 INCHES AFT OF SPAR. REMOVED, FABRICATED, REPLACED WEB SECTIO N
- [SDR HALA9800104](https://openairdocs.org/sdr/HALA9800104.md): Splice · corrosion · Apr 15, 1998 · N672MC · Doug DC951 · Fuselage Main, Plate/Skin
  > EVIDENCE OF CORROSION EMINATING FROM SKIN JOINT, FS 1258 PRODUCTION SPLICE RT 6 INCH BELOW PYLON TRAILING EDGE FAIRING SUPPORT. REMOVED CORROSION AND TREATED PER SRM 51-10-3. REMOVED AND REPLACED FASTENERS AS REQUIRED PER SRM 51-30-2. REMOVED AND REPLACED I
- [SDR HALA9800103](https://openairdocs.org/sdr/HALA9800103.md): Beam · cracked · Apr 15, 1998 · N672MC · Doug DC951 · Fuselage Miscellaneous Structure
  > NOSE LANDING GEAR W/W, LEFT STATION 49 LOWER BEAM IS STRUCTURE ATTACHING UPPER FASTENER AREA IS CRACKED APPROX 5/8 INCH LONG. CRACKED STOP DRILLED IAW DOUBLER AND ANGLE 'L' TREATED SRM 57-05-FIG 110, 51-10-02 AND INSTALLED REPAIR DOUBLER AND 'L' ANGLE SRM 57-
- [SDR HALA9800110](https://openairdocs.org/sdr/HALA9800110.md): Angle · cracked · Apr 7, 1998 · N672MC · Doug DC951 · Fuselage Miscellaneous Structure
  > RIGHT AND LEFT LOWER KEEL BEAM ANGLES TO FRAME ATTACH BRACKET FS 700 - FS 705 HAVE 3 INCH CRACKS RUNNING HORIZONTALLY. REMOVED AND REPLACED LEFT AND RIGHT KEEL BEAM ANGLES PER SRM 51-30-5. TOTAL TIME: 45,975 HOURS. TOTAL CYCLES: 71,775. REF: OPERATOR CON
- [SDR 98ZZZX1972](https://openairdocs.org/sdr/98ZZZX1972.md): Angle · cracked · Apr 7, 1998 · N672MC · Doug DC951 · Fuselage Miscellaneous Structure
  > RIGHT AND LEFT LOWER KEEL BEAM ANGLES TO FRAME ATTACH BRACKET FS 700 - FS 705 HAVE 3 INCH CRACKS RUNNING HORIZONTALLY. REMOVED AND REPLACED LEFT AND RIGHT KEEL BEAM ANGLES PER SRM 51-30-5. TOTAL TIME: 45,975 HOURS. TOTAL CYCLES: 71,775. REF: OPERATOR CON
- [SDR HALA97198](https://openairdocs.org/sdr/HALA97198.md): Actuator · leaking · Jan 17, 1997 · N672MC · Doug DC951 · Leading Edge Slat Actuator
  > HNL - FLT 158 - SLAT DISAGREEMENT LIGHT CAME ON UPON FLAP SELECTION FOR LANDING IN KOA. RECYCLED SLATS AND FLAPS. LIGHT CAME BACK ON AGAIN WITH SLAT EXTENTION. REPLACED LEFT WING SLAT EXTEND SWITCH AND LEFT WING TOP SLAT ACT CYL PER MM 27-80-5. LEAK CHECK
- [SDR HALA96125](https://openairdocs.org/sdr/HALA96125.md): Striker Plate · worn · Aug 24, 1996 · N672MC · Doug DC951 · Landing Gear Position and Warning
  > HNL - FLT 376 - AFTER TAKEOFF, LEFT GEAR UNSAFE LIGHT CAME ON. FOUND STRIKER PLATE WORN. REPLACED STRIKER PLATE. PERFORMED ALTERNATE UPLATCH CHECK ON DOOR PER MM 32-31-4. OPS CHECKED OK. (M)
- [SDR HALA9636](https://openairdocs.org/sdr/HALA9636.md): Control Box · inop · Apr 4, 1996 · N672MC · Doug DC951 · Drag Control System
  > HNL - FLT 509 - SPOILERS WOULD NOT ARM FOR LANDING. WORKED OK MANUAL. REPLACED SPOILER ACTUATOR CONTROL BOX. OPS CHECKED OK. (M)
- [SDR HALA95132](https://openairdocs.org/sdr/HALA95132.md): Angle · cracked · Oct 2, 1995 · N672MC · Doug DC951 · Nacelle/Pylon Structure
  > HNL - IN C-CHECK, RIGHT PYLON TO FUSELAGE TOP ATTACH ANGLE HAS A CRACK APPROX 1.5 INCHES LONG BELOW AFT PRESSURE BULKHEAD TEE CAP. REPLACED PYLON ANGLE. REPLACED FASTENERS IN VERTICAL LEG THROUGH FUSELAGE PER SRM 54-04. INSTALLED HORIZONTAL LEG FASTENERS PE
- [SDR HALA95125](https://openairdocs.org/sdr/HALA95125.md): Floor Beam · corroded · Sep 21, 1995 · N672MC · Doug DC951 · Fuselage Main, Floor Beam
  > HNL - IN C-CHECK, FOUND HEAVY CORROSION ON MID SECTION OF E/E COMPARTMENT AFT FLOOR BEAM, L-1 HEAVY LOCAL. REMOVED DAMAGED SECTION. INSTALLED FILLER AND REPAIR ANGLES PER SRM 53-01. (M)
- [SDR HALA95126](https://openairdocs.org/sdr/HALA95126.md): Former · cracked · Sep 20, 1995 · N672MC · Doug DC951 · Fuselage Miscellaneous Structure
  > HNL - IN C-CHECK, FOUND FORMER CRACKED, 2 PLACES BETWEEN LONGERONS 29L AND 30 AT STATION 579. INSTALLED NESTED DOUBLER PER SRM 53-01. (M)
- [SDR HALA95124](https://openairdocs.org/sdr/HALA95124.md): Former · cracked · Sep 20, 1995 · N672MC · Doug DC951 · Fuselage Miscellaneous Structure
  > HNL - IN C-CHECK, FOUND FORMER CRACKED, 2 PLACES BETWEEN LONGERONS 29R AND 30 AT STATION 541. INSTALLED NESTED DOUBLER PER SRM 53-01. (M)
- [SDR HAL95081](https://openairdocs.org/sdr/HAL95081.md): Eel Battery · discharged · Jun 26, 1995 · N672MC · Doug DC951 · Emergency Lighting
  > INFORMATION FROM M-71 LOG PAGE 142700-2. AFT EMERGENCY FLOOR LIGHTS INOPERABLE. REPLACED AFT EMERGENCY FLOOR LIGHT BATTERIES. OPERATIONAL CHECK GOOD. (X)
- [SDR HAL95001](https://openairdocs.org/sdr/HAL95001.md): Bracket · cracked · Jan 3, 1995 · N672MC · Doug DC951 · Trailing Edge Flaps
  > HNL - ITEM FROM M-71, NR 138547-1. DURING SERVICE CHECK, FOUND A CRACK IN INBOARD FLAP HINGE (BRACKET ASSY) ON THE RIGHT WING. VERIFIED CRACK WITH EDDY CURRENT. FOUND SMALL CRACK INDICATION AT THE LUG ON THE CASTING THAT IS THE ATTACH POINT FOR THE RETRACT

## 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 = 'N672MC' AND deregistration_id = 'N672MC-2013-02-27'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N672MC-2013-02-27/reports

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