# Service difficulty reports: Boeing 737-2M6C

A list on [Boeing 737-2M6C](https://openairdocs.org/model/boeing-737-2m6c.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 3 · 144 reports

- [SDR TSAA0632027](https://openairdocs.org/sdr/TSAA0632027.md): Circuit Card · malfunctioned · Mar 29, 2006 · N805AL · Boeing 7372M6C · Landing Gear System Wiring
  > FERRY FLIGHT 320 HNL-MHV - AFTER TAKEOFF AND GEAR UP, CREW HAD UNSAFE LANDING GEAR INDICATION. CREW LOWERED THE LANDING GEAR AND RETURNED TO HNL WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE A-13 CARD IN THE LANDING GEAR ACCESSORY UNIT AND F
- [SDR TSAA0532049](https://openairdocs.org/sdr/TSAA0532049.md): Brake · inoperative · Oct 18, 2005 · N805AL · Boeing 7372M6C · Landing Gear Brake System
  > PILOTS OBSERVED BOTH ANTI-SKID LIGHTS CAME ON IN FLIGHT ONLY WHEN THE LANDING GEAR IS IN THE (OFF) POSITION; LANDED WITH NO DIFFICULTIES. REMOVED AND REPLACED PARKING BRAKE SHUTOFF VALVE ASSEMBLY. MAINTENANCE ALSO FOUND A BAD NR 4 TRANSDUCER AND CURRENTLY WA
- [SDR TSAA0426077](https://openairdocs.org/sdr/TSAA0426077.md): Connector · damaged · Nov 15, 2004 · N805AL · Boeing 7372M6C · Fire Protection System Wiring
  > FLT 942, HNL-KOA: (NON-ETOPS) AFTER ENGINES WERE STARTED, THE NR 2 ENGINE FIRE WARNING SWITCH AND BELL CAME ON. FOLLOWED THE QRH AND SHUT DOWN THE ENGINE. REPLACED THE HERMETIC CONNECTORS ON THE NR 2 ENGINE LOWER FIRE DETECTION LOOP. ACCOMPLISHED HIGH POWER
- [SDR TSAA0427072](https://openairdocs.org/sdr/TSAA0427072.md): Warning Light · illuminated · Sep 20, 2004 · N805AL · Boeing 7372M6C · Central Warning
  > NON-ETOPS CARGO FLIGHT 909, HNL-LIH, ON CLIMB-OUT PASSING 2000-3000 FT, THE FEEL DIFFERENTIAL PRESSURE LIGHT CAME ON. RETURNED TO HNL. BLEW OUT ELEVATOR PITOT TUBES, PITOT TUBES CLEAR. AIRCRAFT RETURNED TO SERVICE.
- [SDR TSAA0429071](https://openairdocs.org/sdr/TSAA0429071.md): Hydraulic System · contaminated · Sep 20, 2004 · N805AL · Boeing 7372M6C · Hydraulic System, Main
  > NON-ETOPS CARGO FLIGHT 909, HNL-LIH: ON CLIMB-OUT PASSING 1500 FT THE FEEL DIFFERENTIAL PRESSURE LIGHT ILLUMINATED. RETURNED TO HNL. REPLACED THE B HYDRAULIC SYSTEM RETURN FILTER AND CASE DRAIN FILTERS DUE TO CONTAMINATION, OPS CHECK GOOD. REPLACED THE A SY
- [SDR TSAA0427042](https://openairdocs.org/sdr/TSAA0427042.md): Control Cable · out of adjust · May 29, 2004 · N805AL · Boeing 7372M6C · Trailing Edge Flap Control System
  > AT 34,000 FT DURING CRUISE THE L/E FLAP TRANSIT LIGHT CAME ON, AUTO-PILOT KICKED OFF AND ON DESCENT THE CONFIGURATION HORN CAME ON. RETURNED TO HNL. ADJUST FLAP CABLE WFA & WFB TENSION IAW AMM 27-51-01 AS ADDRESSED BY BOEING SERVICE LETTER 27-040. OPS CHECK
- [SDR TSAA0453023](https://openairdocs.org/sdr/TSAA0453023.md): Door Frame · cracked · Jan 20, 2004 · N805AL · Boeing 7372M6C · Fuselage Main, Structure
  > FOUND CRACK ON LOWER INBOARD CORNER OF FORWARD CARGO DOOR FRAME. TRIMMED OUT DAMAGED AREA. VERIFIED CRACK REMOVED USING HFEC INSPECTION. FABRICATED A REPAIR ANGLE, ALODINED, AND PRIMED. INSTLALED REPAIR PARTS. REPAIR COMPLETED IAW ECO 1763. AIRCRAFT RETU
- [SDR TSAA0330154](https://openairdocs.org/sdr/TSAA0330154.md): Shutoff Valve · defective · Jun 25, 2003 · N805AL · Boeing 7372M6C · Air Intake Anti/De-Ice System
  > FLT 952 - HNL-ITO, NR 2 ENGINE COWL ENGINE ICE LIGHT REMAINS ON IN TRANSITION (BRIGHT BLUE). RETURNED TO HNL FOR UNEVENTFUL LANDING. REMOVED AND REPLACED THE NR 2 ENIGNE COWL VALVE. OPS CHECKED GOOD IAW AMM 75-11-0. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0333113](https://openairdocs.org/sdr/TSAA0333113.md): Battery Pack · inoperative · May 3, 2003 · N805AL · Boeing 7372M6C · Emergency Lighting
  > REPLACED FORWARD ENTRY EMERGENCY EXIT LIGHT BATTERY PACK DUE TO INOPERATIVE. OP CHECK OK. AIRCAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0379039](https://openairdocs.org/sdr/TSAA0379039.md): Switch · inoperative · Feb 23, 2003 · N805AL · Boeing 7372M6C · Turbine Engine Oil System
  > DURING CLIMB, THE NR 1 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED. THE NR 1 ENGINE WAS SHUTDOWN IAW THE QRH. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED IN HNL WITH NO FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE OIL BYPASS SWITCH
- [SDR TSAA0353016](https://openairdocs.org/sdr/TSAA0353016.md): Skin · corroded · Feb 4, 2003 · N805AL · Boeing 7372M6C · Fuselage Main, Plate/Skin
  > TRIMMED OUT DAMAGE SKIN AT BS 918 ABOVE STRINGER 25R. HFEC INSPECTED THE EDGE OF THE TRIM. ENLARGED TRIM BY.04 INCH INSURANCE CUT. NDT INSPECTED THE OUTER ROW OF FASTENER HOLES COMMON TO REMOVED EXISTING LAP REPAIR USING ROTARY AND SURFACE PROBLE INSPECTIO
- [SDR TSAA0353007](https://openairdocs.org/sdr/TSAA0353007.md): Skin · corroded · Feb 4, 2003 · N805AL · Boeing 7372M6C · Fuselage Main, Plate/Skin
  > REMOVED DAMAGED SKIN AND STRINGERS 26L, 27L, AND 27R BETWEEN BS 908 AND BS 1016. REPLACED SKIN PANEL PER PRODUCTION DRAWINGS 65-45776-55 AND 65-45776-56. INSTALLED PRODUCTION PANEL USING FASTENERS IDENTIFIED IN DRAWINGS. FINISHED ALL BARE ALUMINUM WITH ALODI
- [SDR TSAA0353017](https://openairdocs.org/sdr/TSAA0353017.md): Skin · corroded · Feb 4, 2003 · N805AL · Boeing 7372M6C · Fuselage Main, Plate/Skin
  > TRIMMED OUT DAMAGE SKIN AT BS 947.5 ABOVE STRINGER 25L. HFEC INSPECTED THE EDGE OF THE TRIM. ENLARGED TRIM BY.040 INCH INSURANCE CUT. NDT INSPECTED THE OUTE ROW OF FASTENER HOLES COMMON TO REMOVED EXISTING REPAIR USING.030 NOTCH ROTARY AND SURFACE PROBE I
- [SDR TSAA0353011](https://openairdocs.org/sdr/TSAA0353011.md): Stringer · corroded · Jan 30, 2003 · N805AL · Boeing 7372M6C · Fuselage Main, Longeron/Stringer
  > TRIMMED OUT DAMAGE STRINGER SECTION. FABRICATED A.090 INCH THICK J AND U-CHANNEL FROM 7075-T6. ALODINED AND APPLIED TWO COATS PRIMER TO ALL BARE ALUMINUM. INSTALLED REPAIR PARTS USING FASTENERS IDENTIFIED IN FIGURE 2. SEALED FAYING SURFACE WITH BMS 5-95 SE
- [SDR TSAA0353004](https://openairdocs.org/sdr/TSAA0353004.md): Stringer · cracked · Jan 30, 2003 · N805AL · Boeing 7372M6C · Fuselage Main, Longeron/Stringer
  > EXTERIOR 1 INCH FUSELAGE CRACK AT BS 375 AT STRINGER 15L. TRIMMED OUT DAMAGE. HFEC INSPECTED THE EDGE OF THE TRIM. ENLARGED TRIMMED AREA BY.040 INCH INSURANCE CUT. HFEC ROTARY AND SURFACE PROBLE INSPECTED FASTENER HOLES ALONG STRINGER 15R UNDER THE REPAIR
- [SDR TSAA0353003](https://openairdocs.org/sdr/TSAA0353003.md): Skin · cracked · Jan 29, 2003 · N805AL · Boeing 7372M6C · Fuselage Main, Plate/Skin
  > EXTERIOR 1 INCH CRACK BETWEEN BS 440 AND BS 460 AT BL 0. TRIMMED OUT DAMAGED AREA ON LOWER LOBE ANTENNA CUT OUT. PERFORMED NDT INSPECTION OF CUTOUT, SKIN AND SATELLITE HOLES USING HFEC, NO DEFECTS NOTED. FABRICATED A.063 INCH THICK FILLER AND.071 INCH THI
- [SDR TSAA0353005](https://openairdocs.org/sdr/TSAA0353005.md): Stringer · cracked · Jan 20, 2003 · N805AL · Boeing 7372M6C · Fuselage Main, Longeron/Stringer
  > TWO RIVETS SHOW CRACK INDICATIONS USING LFEC AT BS 227.8 STRINGER 27R. REMOVED ADJACENT FASTENERS AND STRINGER. USING HFEC CONFIRMED NO CRACK INDICATION USING ROTARY PROBE IAW BOEING TELEX ALO-HNL-03-0031H. (M)
- [SDR TSAA0226197](https://openairdocs.org/sdr/TSAA0226197.md): Pitot Tube · obstructed · Sep 22, 2002 · N805AL · Boeing 7372M6C · Pitot/Static System
  > FLT 930 - HNL-OGG - DURING THE CLIMB-OUT OF HNL, THE FIRST OFFICERS AIR SPEED INDICATOR WAS INDICATING 40 KNOTS SLOWER THAN THE CAPTAIN'S INDICATOR. THE AIRCRAFT RETURNED TO AND LANDED AT HNL WITH NO FURTHER INCIDENT. MAINTENANCE PERSONNEL REMOVED FOD FROM T
- [SDR TSAA0251185](https://openairdocs.org/sdr/TSAA0251185.md): Frame · cracked · Aug 13, 2002 · N805AL · Boeing 7372M6C · Fuselage Main, Structure
  > CRACK LOCATED AT BS 807, S-14L. CUT AND REMOVED DAMAGED AREA, VERIFIED CRACK REMOVAL UTILIZING HFEC METHOD NO DEFECTS NOTED, FABRICATED AND INSTALLED REPAIR ANGLES AND FILLER FROM.063 IN 2075-T6 IAW APPROVED FASTENERS WENT WITH BMS 5-95 SEALANT PER TABLE I A
- [SDR TSAA0251190](https://openairdocs.org/sdr/TSAA0251190.md): Frame · cracked · Aug 13, 2002 · N805AL · Boeing 7372M6C · Fuselage Main, Frame
  > TEAR STRAP FASTENER HOLE CRACK AT BS 777, S-20L. REMOVED FASTENER AND VERIFIED CRACK UTILIZING HFEC ROTARY HOLE PROBE METHOD IAW WITH NDT, REMOVED DAMAGED AREA AND HFEC INSPECTION COMPLETED NO DEFECTS NOTED. FABRICATED AND INSTALLED.032 IN 2024-T3 CLAD REPA
- [SDR TSAA0251189](https://openairdocs.org/sdr/TSAA0251189.md): Stiffener · cracked · Aug 13, 2002 · N805AL · Boeing 7372M6C · Wing Miscellaneous Structure
  > LT WING FRONT SPAR STIFFENER CRACK AT FSS 473.31 AND FSS 475.55. REMOVED, FABRICATED AND INSTALLED STIFFENERS. NEW STIFFENERS FABRICATED FROM 7178-T6511 EXTRUSION AND NEW SHIMS FABRICATED FROM 2024-T3, APPLIED ALODINE AND BMS 10-11 TYPE 1 PRIMER AND BMS 10-1
- [SDR TSAA0251188](https://openairdocs.org/sdr/TSAA0251188.md): Window Frame · cracked · Aug 13, 2002 · N805AL · Boeing 7372M6C · Fuselage Main, Structure
  > RT SIDE WINDOW FRAME CORNER FASTENER HOLE CRACK AT BS 727B. VERIFIED CRACK ON WINDOW FRAME ASSY BY UTILIZING HFEC ROTAR PROBE METHOD, REAMED WINDOW FRAME FASTENER HOLE UNTIL REMOVAL OF CRACK. VERIFIED CRACK REMOVAL BY HFEC ROTARY METHOD, ENLARGED AND INSTALL
- [SDR TSAA0251187](https://openairdocs.org/sdr/TSAA0251187.md): Window Frame · cracked · Aug 13, 2002 · N805AL · Boeing 7372M6C · Fuselage Main, Structure
  > RT SIDE WINDOW FRAME CORNER FASTENER HOLE CRACK AT BS 380. CRACK ON WINDOW FRAME ASSY BY UTILIZING HFEC ROTARY PROBE METHOD, REAMED WINDOW FRAME FASTENER HOLE UNTIL REMOVAL OF CRACK, CRACK REMOVAL BY HFEC ROTARY METHOD, ENLARGED, INSTALLED FREEZE PLUG TO FAST
- [SDR TSAA0251186](https://openairdocs.org/sdr/TSAA0251186.md): Skin · cracked · Aug 13, 2002 · N805AL · Boeing 7372M6C · Fuselage Main, Plate/Skin
  > RT BS 1129 AND BS 1138 FUSELAGE SKIN CRACKS LOCATED AT S5R AND S12R. TRIMMED OUT CRACKS MAINTAINING A MINIMUM TRIM OUT CORNER RADIUS.050 INCHES AT A SURFACE FINISH OF 63 RMS OR SMOOTHER. PERFORMED HFEC INSPECTION AROUND TRIMOUT AREA, NO DEFECTS NOTED. FABR
- [SDR TSAA0253144](https://openairdocs.org/sdr/TSAA0253144.md): Frame · cracked · Jun 1, 2002 · N805AL · Boeing 7372M6C · Fuselage Main, Frame
  > REPAIRED RIGHT OUTBOARD CHORD AT BS727, S18A DUE TO FASTENER HOLE CRACK. UTILIZED HIGH FREQUENCY EDDY CURRENT AND ULTRASONIC METHODS. REMOVED AND INSTALLED CHORD ASSEMBLY, REASSEMBLED AND INSTALLED ALL COMPONENTS AND FASTENERS, APPLIED BMS 5-95, TYPE I SEALA
- [SDR TSAA0251145](https://openairdocs.org/sdr/TSAA0251145.md): Skin · cracked · May 20, 2002 · N805AL · Boeing 7372M6C · Fuselage Main, Plate/Skin
  > REPAIRED FUSELAGE SKIN CRACK AT BS 727B, S-17. CUT OUT DAMAGED AREA AND PERFORMED HFEC INSPECTION AROUND CUT OUT, PERFORMED INSURANCE CUT OF.040 INCH, FABRICATED AND INSTALLED REPAIR DOUBLER AND TEAR STRAP. AIRCRAFT RETURNED TO SERVICE.
- [SDR TSAA0251140](https://openairdocs.org/sdr/TSAA0251140.md): Frame · cracked · May 20, 2002 · N805AL · Boeing 7372M6C · Fuselage Main, Frame
  > FOUND CRACK ON THE FRAME AT BS 480 ABOVE STRINGER 17R. CUT OUT AND REMOVED DAMAGED PORTION OF FORMED SECTION. VERIFIED CUTOUT WITH HFEC. DETERMINED FROM TABLES III, IV, AND V, THE NUMBER OF FASTENERS AND FASTENER ROWS REQUIRED. FABRICATED REPAIR PARTS FROM
- [SDR TSAA0233117](https://openairdocs.org/sdr/TSAA0233117.md): Battery Pack · discharged · Apr 24, 2002 · N805AL · Boeing 7372M6C · Emergency Lighting
  > REPLACED LEFT OVERWING EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0253105](https://openairdocs.org/sdr/TSAA0253105.md): Skin · cracked · Apr 6, 2002 · N805AL · Boeing 7372M6C · Fuselage Main, Plate/Skin
  > FOUND 3 INCH CRACK ON THE FUSELAGE SKIN AT BS 887 ALONG STRINGER 24R. CUT OUT DAMAGED PORTION OF SKIN. VERIFIED CRACK REMOVED USING HFEC. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-30-3 FIGURE 1. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0253059](https://openairdocs.org/sdr/TSAA0253059.md): Skin · corroded · Mar 1, 2002 · N805AL · Boeing 7372M6C · Vertical Stabilizer, Plate/Skin
  > FOUND SKIN BULGE ON RIGHT SIDE VERTICAL FIN RIGHT SPAR AT FWL 112.356. FABRICATED REPAIR ANGLE, EXTERNAL DOUBLER, TWO FS 173.10 IN SPAR RIB CLIPS, REPLACEMENT FIN REAR SPAR WEB, SOLID SINGLE GUSSET, SKIN TRIM POUT FILLER AND FLAT FILLERS IAW FIGURES 2A THROUG
- [SDR TSAA0253060](https://openairdocs.org/sdr/TSAA0253060.md): Spar · cracked · Mar 1, 2002 · N805AL · Boeing 7372M6C · Vertical Stabilizer, Spar/Rib
  > FOUND CRACK IN THE VERTICAL STABILIZER IN SPAR WEB ON THE VERTICAL STABILIZER. TRIMMED OUT CRACK IAW FIGURE 2. FABRICATED A REPAIR DOUBLER AND A FILLER AS SHOWN IN FIGURE 2. INSTALLED REPAIR PARTS AND VERIFIED 8110-3 RECEIVED IAW ECO 3276. AIRCRAFT RETURNE
- [SDR TSAA0255025](https://openairdocs.org/sdr/TSAA0255025.md): Spar · nicked · Jan 14, 2002 · N805AL · Boeing 7372M6C · Horizontal Stabilizer, Spar/Rib
  > FOUND NICKS ON CENTER SECTION REAR SPAR UPPER FORWARD SIDE FITTING. REMOVED NICKS/DAMAGED MATERIAL TO A MAXIMUM OF.01 INCH AND TAPERED. APPLIED A CHEMICAL CONVERSION COATING AND REFINISHED THE REWORKED SURFACE IAW SRM 55-10-1 FIGURE 6, DETAIL IX. AIRCRAFT
- [SDR TSAA0255024](https://openairdocs.org/sdr/TSAA0255024.md): Attach Fitting · gouged · Jan 14, 2002 · N805AL · Boeing 7372M6C · Horizontal Stabilizer, Attach Fittings
  > FOUND GOUGE MARKS ON LEFT HORIZONTAL STABILIZER CENTER SECTION LUG, UPPER FORWARD FITTING. REMOVED GOUGE / DAMAGED MATERIAL TO A MINIMUM WIDTH OF.10 INCH AND RADIUS OF 1 INCH AND TAPERED. APPLIED A CHEMICAL CONVERSION COATING AND REFINISHED THE REWORKED SUR
- [SDR TSAA0133165](https://openairdocs.org/sdr/TSAA0133165.md): Battery Pack · inoperative · Dec 1, 2001 · N805AL · Boeing 7372M6C · Emergency Lighting
  > REPLACED NR 5 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OP CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0126118](https://openairdocs.org/sdr/TSAA0126118.md): Fire Warning · false activation · Sep 16, 2001 · N805AL · Boeing 7372M6C · Fire Detection
  > FLT - 117 - HNL-LIH - ON SHORT FINAL LANDING IN LIHUE, HI, THE APU WAS STARTED AND FOLLOWED BY AN ILLUMINATION OF THE APU FIRE WARNING HANDLE, THE SOUNDING OF THE FIRE WARNING BELL, AND ILLUMINATION OF THE GLARE SHIELD FIRE WARNING LIGHTS. THE APU FIRE HANDLE
- [SDR TSAA0153077](https://openairdocs.org/sdr/TSAA0153077.md): Spar · corroded · Jun 18, 2001 · N805AL · Boeing 7372M6C · Fuselage Structure (General)
  > FOUND CORROSION DURING HEAVY CHECK AT RIGHT WING FRONT SPAR LOWER CHORD FORWARD FLANGE LOWER SURFACE AT FSS 476.0 THROUGH FSS 481.7. (M)
- [SDR TSAA0153075](https://openairdocs.org/sdr/TSAA0153075.md): Bear Strap · corroded · Jun 15, 2001 · N805AL · Boeing 7372M6C · Fuselage Main, Plate/Skin
  > DISCOVERED CORROSION AT FORWARD CARGO DOOR BEAR STRAP (AFT UPPER CORNER). (M)
- [SDR TSAA0153076](https://openairdocs.org/sdr/TSAA0153076.md): Skin · cracked · Jun 15, 2001 · N805AL · Boeing 7372M6C · Wing, Plate/Skin
  > FOUND.62 INCH CRACK DURING HEAVY CHECK AT RIGHT UPPER WING SKIN AFT EDGE BETWEEN WBL 157 AND WBL 183.4. (M)
- [SDR TSAA0133022](https://openairdocs.org/sdr/TSAA0133022.md): Battery Pack · discharged · Feb 22, 2001 · N805AL · Boeing 7372M6C · Emergency Lighting
  > REPLACED NR 1 FLOOR EMERGENCY LIGHT BATTERY PACK FOR BEING LOW. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0133016](https://openairdocs.org/sdr/TSAA0133016.md): Battery Pack · discharged · Feb 16, 2001 · N805AL · Boeing 7372M6C · Emergency Lighting
  > REPLAED NR 2 FLOOR EMERGENCY LIGHT BATTERY PACK FOR BEING LOW. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0153012](https://openairdocs.org/sdr/TSAA0153012.md): Frame · cracked · Feb 9, 2001 · N805AL · Boeing 7372M6C · Fuselage Main, Frame
  > FOUND IDENTIFIED CRACK AT BS 727, STRINGER 18L UPPER CHORD BY UTILIZING HFEC METHOD. (M)
- [SDR TSAA0033243](https://openairdocs.org/sdr/TSAA0033243.md): Battery Pack · inoperative · Dec 14, 2000 · N805AL · Boeing 7372M6C · Emergency Lighting
  > REPLACED NR 4 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE, OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0033224](https://openairdocs.org/sdr/TSAA0033224.md): Battery Pack · discharged · Oct 27, 2000 · N805AL · Boeing 7372M6C · Emergency Lighting
  > REPLACED NR 2 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0053219](https://openairdocs.org/sdr/TSAA0053219.md): Frame · cracked · Sep 12, 2000 · N805AL · Boeing 7372M6C · Fuselage Main, Frame
  > PREVENTIVE MODIFICATION INCORPORATED INCONJUNCTION WITH CRACK REPAIR AT BS 480 INNER FRAME FLANGE. REPAIR INCLUDED TRIM OUT OF CRACK, HFEC INSPECTION OF TRIM OUT. INSTALLED.040 INCH 7075-T6 FILLER AND INSTALLATION OF.050 INCH DOUBLER. IAW AD 2000-04-08, S
- [SDR 20001012AP002](https://openairdocs.org/sdr/20001012AP002.md): Seal · worn · Jun 28, 2000 · N805AL · Boeing 7372M6C · Pneumatic Distribution System
  > FLT 286 - OGG-ITO - FLIGHT CREW EXPERIENCED A LEFT WING BODY OVERHEAT LIGHT ON. LIGHT WENT OUT AFTER LEFT BLEED SWITCH WAS TURNED OFF AND ISOLATION VALVE CLOSED. CREW RETURNED TO OGG AFTER CONFERRING WITH DISPATCH THAT THER WAS NO MAINTENANCE SUPPORT AVAILAB
- [SDR TSAA0026160](https://openairdocs.org/sdr/TSAA0026160.md): Clamp · worn · Jun 28, 2000 · N805AL · Boeing 7372M6C · Pneumatic Distribution System
  > FLT - 286 - OGG-ITO - FLIGHT CREW EXPERIENCED A LEFT WING-BODY OVERHEAT LIGHT ON. LIGHT WETN OUT AFTER LEFT BLEED SWITCH WAS TURNED OFF AND ISOLATION VALVE CLOSED. CREW RETURNED TO OGG AFTER CONFERRING WITH DISPATCH THAT THERE WAS NO MAINTENANCE SUPPORT AVAI
- [SDR TSAA0033154](https://openairdocs.org/sdr/TSAA0033154.md): Battery Pack · inoperative · Jun 24, 2000 · N805AL · Boeing 7372M6C · Emergency Lighting
  > REPLACED NR 3 AND NR 6 FLOOR EMERGENCY LIGHT BATTERY POWER PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0033153](https://openairdocs.org/sdr/TSAA0033153.md): Battery Pack · inoperative · Jun 23, 2000 · N805AL · Boeing 7372M6C · Emergency Lighting
  > REPLACED FORWARD SERVICE DOOR EMERGENCY EXIT IDENTIFIER POWER PACK. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0053127](https://openairdocs.org/sdr/TSAA0053127.md): Stringer · cracked · Apr 26, 2000 · N805AL · Boeing 7372M6C · Fuselage Main, Longeron/Stringer
  > REPAIRED 1.75 INCH CRACK AT STRINGER 16L APPROX 4 INCHES AFT OF BS 727 AND 2 INCH CRACK AT STRINGER 17L APPROX 7 INCHES AFT OF BS 727 CONFIRMED BY USING HIGH FREQUENCY EDDY CURRENT METHOD. REPAIRED BY USING ONE DOUBLER FOR BOTH CRACKS IAW SRM 53-30-3. AIRCRA
- [SDR TSAA0033122](https://openairdocs.org/sdr/TSAA0033122.md): Battery Pack · inoperative · Apr 24, 2000 · N805AL · Boeing 7372M6C · Emergency Lighting
  > REPLACED FORWARD OVERHEAD EXIT IDENTIFIER BATTERY. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Next page: https://openairdocs.org/model/boeing-737-2m6c/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 aircraft_model_key = '7372M6C'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-737-2m6c/reports

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