# Service difficulty reports: Boeing 737-2P6

A list on [Boeing 737-2P6](https://openairdocs.org/model/boeing-737-2p6.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 4 · 200 reports

- [SDR TSAA0777056](https://openairdocs.org/sdr/TSAA0777056.md): Connector · misinstalled · Oct 15, 2007 · N835AL · Boeing 7372P6 · Engine Indicating System Wiring
  > NON-ETOPS FLIGHT 278 HNL-KOA, ON TAKEOFF AFTER THROTTLE ADVANCE, THE CREW NOTED THE NR 1 EPR AT 2.22 AND THE NR 2 EPR AT 1.74. THE CREW ABORTED THE TAKEOFF AT 100 KTS INDICATED AIRSPEED. THE CREW RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE FO
- [SDR TSAA0773051](https://openairdocs.org/sdr/TSAA0773051.md): Fuel Control · failed · Sep 20, 2007 · N835AL · Boeing 7372P6 · Fuel Control/Turbine Engines
  > NON-ETOPS FLIGHT 90 HNL-KOA, ON TAKEOFF ROLL, THE CREW NOTED THE NR 2 EGT CLIMBING FASTER THAN THE NR 1 EGT. ABORTED THE TAKEOFF AT 100 KTS INDICATED AIRSPEED DUE TO NR 2 ENGINE HIGH EGT. THE CREW RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE C
- [SDR TSAA0629097](https://openairdocs.org/sdr/TSAA0629097.md): Transmitter · failed · Nov 7, 2006 · N835AL · Boeing 7372P6 · Hydraulic Indicating System
  > NON-ETOPS FLT 68 HNL-ITO: DURING CLIMB, THE CREW NOTED THAT THE HYDRAULIC A-SYSTEM PRESSURE GAUGE READ 800 PSI. THE CREW RETURNED TO FIELD AND LANDED IN WITHOUT FURTHER INCIDENT. MAINTENANCE PLACED THE HYDRAULIC A-SYSTEM PRESSURE INDICATION ON MEL 29-3-1. AIR
- [SDR TSAA0632091](https://openairdocs.org/sdr/TSAA0632091.md): Light · inoperative · Oct 24, 2006 · N835AL · Boeing 7372P6 · Landing Gear Position and Warning
  > FLT 244 HNL-OGG - DURING APPROACH, CREW NOTED THE LEFT LANDING GEAR GREEN LIGHT WOULD NOT ILLUMINATE WITH THE LANDING GEAR LEVER SELECTED IN THE DOWN POSITION. THE CREW CYCLED THE LANDING GEAR WHICH STILL RESULTED IN NO INDICATION. A GO-AROUND WAS PERFORMED
- [SDR TSAA0632072](https://openairdocs.org/sdr/TSAA0632072.md): Light · inoperative · Aug 19, 2006 · N835AL · Boeing 7372P6 · Landing Gear Position and Warning
  > NON-ETOPS FLT 226 LIH-HNL: DURING TAKEOFF, CREW NOTED RED NOSE GEAR WARNING LIGHT NOT ILLUMINATED. THE CREW RE-LAMPED THE NOSE GEAR WARNING LIGHT. AIRCRAFT LANDED IN HNL WITHOUT FURTHER INCIDENT. MAINTENANCE NOTED NOSE GEAR RED WARNING LIGHT OPERATIVE. AIR
- [SDR TSAA0632071](https://openairdocs.org/sdr/TSAA0632071.md): Light · inoperative · Aug 19, 2006 · N835AL · Boeing 7372P6 · Landing Gear Position and Warning
  > ON APPROACH, CREW NOTED GREEN NOSE GEAR DOWN LIGHT NOT ILLUMINATED. THE CREW PERFORMED A GO-AROUND AND RE-LAMPED THE NOSE GEAR DOWN LIGHT. AIRCRAFT LANDED IN LIH WITHOUT FURTHER INCIDENT. MAINTENANCE NOTED NOSE GEAR DOWN LIGHT OPERATIVE. AIRCRAFT WAS RETUR
- [SDR TSAA0621038](https://openairdocs.org/sdr/TSAA0621038.md): Line · misinstalled · May 20, 2006 · N1PC · Boeing 7372P6 · Pneumatic Distribution System
  > PACK TRIP OFF AFTER T/O. BURNING RUBBER SMELL AND PRESSURE BUMP ON T/O AND LANDING. REMOVED & REPLACED RIGHT A/C BAY FLOW CONTROL VALVE, OPS AND LEAK CHECK OK. ACTION DID NOT FIX PROBLEM. REMOVED & REPLACED NR 2 ENGINE PNEUMATIC SHUT-OFF VALVE, OPS & LEAK
- [SDR TSAA0672037](https://openairdocs.org/sdr/TSAA0672037.md): Engine · malfunctioned · May 12, 2006 · N1PC · Boeing 7372P6 · Engine (Turbine/Turboprop)
  > ON DESCENT THE CREW ADVANCED THE THROTTLES AND HEARD 3 LOAD BANG SOUNDS FROM THE NR 1 ENGINE. THERE WERE NO ABNORMAL ENGINE INDICATIONS. CREW RETARDED THROTTLES SLIGHTLY AND THE SOUNDS DISSIPATED AND DID NOT RETURN. CREW LANDED IN KOA WITHOUT FURTHER INCIDE
- [SDR TSAA0632036](https://openairdocs.org/sdr/TSAA0632036.md): Strut · low · May 11, 2006 · N1PC · Boeing 7372P6 · Main Landing Gear Strut/Axle/Truck
  > DURING CRUISE THE CREW NOTED THAT THE RIGHT MAIN GEAR INDICATION LIGHTS ILLUMINATED BOTH GREEN AND RED (UNSAFE CONDITION). THE CREW MOVED THE LANDING GEAR SELECTOR FROM THE OFF POSITION TO UP POSITION AND THE GEAR INDICATION RETURNED TO GREEN ONLY. THE CREW
- [SDR F3LA200200384](https://openairdocs.org/sdr/F3LA200200384.md): Stud · loose · Nov 1, 2002 · N1PC · Boeing 7372P6 · Turbine Engine Oil System
  > DURING CLIMBOUT, THE FLIGHT CREW REPORTED THE NUMBER ONE ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED AND OIL QUANTITY WAS SHOWN AT ZERO. THE AIRCRAFT RETURNED TO ITS DEPARTURE AIRPORT. MAINTENANCE FOUND A LOOSE STUD ON THE MAIN OIL FILTER. THE STUD HOLE WAS H
- [SDR F3LA200200253](https://openairdocs.org/sdr/F3LA200200253.md): Skin · cracked · Aug 28, 2002 · N272 · Boeing 7372P6 · Leading Edge Devices
  > DURING C-2 CHECK, INSPECTION REPORTED LT WING NR 1 SLAT LOWER SKIN CRACKED AT LAST ROW OF RIVETS, OUTBOARD OF MAIN TRACK. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PER SRM 57-43-01.
- [SDR F3LA200200195](https://openairdocs.org/sdr/F3LA200200195.md): Structure · corroded · Jul 5, 2002 · N272 · Boeing 7372P6 · Rudder Miscellaneous Structure
  > DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON RUDDER BULLNOSE BY NR 3 HINGE. REPLACED CORRODED AREA OF RUDDER BULLNOSE PER SRM 51-40-02 AND BOEING DRAWING 65-53740.
- [SDR F3LA200200194](https://openairdocs.org/sdr/F3LA200200194.md): Strap · corroded · Jul 5, 2002 · N272 · Boeing 7372P6 · Fuselage Miscellaneous Structure
  > DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON STRAP AT BS 857, RBL 18. REPLACED STRAP PER SRM 51-30-5 AND 51-30-2.
- [SDR F3LA200200193](https://openairdocs.org/sdr/F3LA200200193.md): Sill · cracked · Jul 5, 2002 · N272 · Boeing 7372P6 · Fuselage Miscellaneous Structure
  > DURING C-2 CHECK, INSPECTION REPORTED R1 DOOR LOWER SILL WEB CRACKED AT FWD DRAIN HOLE. REMOVED DAMAGED WEB, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER PER SRM 51-40-02 AND SOPM 20-41-02.
- [SDR F3LA200200192](https://openairdocs.org/sdr/F3LA200200192.md): Sill · corroded · Jul 5, 2002 · N272 · Boeing 7372P6 · Fuselage Miscellaneous Structure
  > DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON R1 DOOR MOP SEAL AND THRESHOLD SUPPORT. REMOVED CORROSION PER SRM 53-10-01 AND INSTALLED NEW MOP SEAL PER SRM 51-30-02.
- [SDR F3LA200200191](https://openairdocs.org/sdr/F3LA200200191.md): Angle · corroded · Jul 5, 2002 · N272 · Boeing 7372P6 · Fuselage Miscellaneous Structure
  > DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON FLOOR ANGLE INBD OF R1 GUTTER AT BS 336, RBL 54. FABRICATED AND INSTALLED REPLACEMENT SUPPORT ANGLES PER BOEING DRAWING 65C15677 AND SRM 51-30-2.
- [SDR F3LA200200188](https://openairdocs.org/sdr/F3LA200200188.md): Seat Track · corroded · Jul 4, 2002 · N272 · Boeing 7372P6 · Fuselage, Seat/Cargo Attach Fittings
  > DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON TWO SEAT TRACKS BETWEEN BS 947 AND BS 967, RBL 11.50. FABRICATED AND INSTALLED REPLACEMENT SEAT TRACK PER SRM 51-30-02.
- [SDR F3LA200200187](https://openairdocs.org/sdr/F3LA200200187.md): Seat Track · corroded · Jul 3, 2002 · N272 · Boeing 7372P6 · Fuselage, Seat/Cargo Attach Fittings
  > DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON TOP OF SEAT TRACK BETWEEN BS 947 AND BS 967, RBL 36.5. FABRICATED AND INSTALLED REPLACEMENT SEAT TRACK PER SRM 51-30-2.
- [SDR F3LA200200185](https://openairdocs.org/sdr/F3LA200200185.md): Seat Track · corroded · Jul 2, 2002 · N272 · Boeing 7372P6 · Fuselage, Seat/Cargo Attach Fittings
  > DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON CARGO FLOOR TRACK, STA 797 TO 809, RBL 14. REPLACED CARGO FLOOR TRACK PER SRM 51-30-02.
- [SDR F3LA200200182](https://openairdocs.org/sdr/F3LA200200182.md): Floorbeam · corroded · Jul 2, 2002 · N272 · Boeing 7372P6 · Fuselage Main, Floor Beam
  > DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON TOP OF FLOORBEAM AT STA 987.5, RBL 36 TO RBL 40. REPLACED FLOORBEAM PER SRM 53-10-9, FIG 3.
- [SDR F3LA200200181](https://openairdocs.org/sdr/F3LA200200181.md): Floorbeam · corroded · Jul 2, 2002 · N272 · Boeing 7372P6 · Fuselage Main, Floor Beam
  > DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON TOP OF FLOORBEAM AT STA. 947.5, RBL 38 TO RBL 43.75. REPAIRED FLOOR BEAM PER SRM 53-10-9.
- [SDR F3LA200200189](https://openairdocs.org/sdr/F3LA200200189.md): Floor Support · corroded · Jul 1, 2002 · N272 · Boeing 7372P6 · Fuselage Miscellaneous Structure
  > DURING C-2 CHECK, INSPECTION REPORTED SURFACE CORROSION ON FLOOR SUPPORT BETWEEN BS 947 AND BS 967, FROM RBL 11.50 TO RBL 36.50. FABRICATED AND INSTALLED REPLACEMENT FLOOR SUPPORT PER SRM 51-30-02 AND EA 53-737-173.
- [SDR F3LA200200186](https://openairdocs.org/sdr/F3LA200200186.md): Floorbeam · corroded · Jul 1, 2002 · N272 · Boeing 7372P6 · Fuselage Main, Floor Beam
  > DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON TOP OF FLOOR BEAM AT STA. 947.5, RBL 38. REPAIRED FLOOR BEAM PER SRM 53-10-9.
- [SDR F3LA200200184](https://openairdocs.org/sdr/F3LA200200184.md): Sill · corroded · Jul 1, 2002 · N272 · Boeing 7372P6 · Fuselage Miscellaneous Structure
  > DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON AFT CARGO DOOR OPENING LOWER WEB SILL. REPLACED CARGO WEB SILL PER SRM 51-30-2.
- [SDR F3LA200200183](https://openairdocs.org/sdr/F3LA200200183.md): Floor Support · corroded · Jul 1, 2002 · N272 · Boeing 7372P6 · Fuselage Miscellaneous Structure
  > DURING C-2 CHECK, INSPECTION REPORTED FLOOR SUPPORT CORRODED BETWEEN STA 967 TO 987.5, RBL 20. FABRICATED AND INSTALLED REPLACEMENT FLOOR SUPPORT PER EA 53-737-173 AND SRM 51-30-2.
- [SDR F3LA200200179](https://openairdocs.org/sdr/F3LA200200179.md): Sill · corroded · Jul 1, 2002 · N272 · Boeing 7372P6 · Fuselage Miscellaneous Structure
  > DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON R1 DOOR MOP SILL AND THRESHOLD SUPPORT. REMOVED CORROSION ON MOP SILL AND FOUND TO BE OUT OF LIMITS PER SRM 53-10-01. REPLACED MOP SILL PER SRM 51-30-02.
- [SDR F3LA200200180](https://openairdocs.org/sdr/F3LA200200180.md): Sill · corroded · Jul 1, 2002 · N272 · Boeing 7372P6 · Fuselage Miscellaneous Structure
  > DURING C-2 CHECK, INSPECTION REPORTED R1 DOOR LOWER SILL WEB CRACKED AT FWD DRAIN HOLE. REMOVED DAMAGED WEB, FABRICATED REPAIR DOUBLER AND FILLER PER SRM 51-40-02, AND INSTALLED REPAIR PARTS PER SRM 51-40-02.
- [SDR F3LA200200178](https://openairdocs.org/sdr/F3LA200200178.md): Floor Support · corroded · Jul 1, 2002 · N272 · Boeing 7372P6 · Fuselage Miscellaneous Structure
  > DURING C-2 CHECK, INSPECTION REPORTED SURFACE CORROSION ON FLOOR SUPPORT BETWEEN STA 967 AND 987.5, LBL 18. FABRICATED AND INSTALLED REPLACEMENT FLOOR SUPPORT PER EA 53-737-173 AND SRM 51-30-02 AND SRM 53-10-02.
- [SDR F3LA200200177](https://openairdocs.org/sdr/F3LA200200177.md): Floor Support · corroded · Jul 1, 2002 · N272 · Boeing 7372P6 · Fuselage Miscellaneous Structure
  > DURING C-2 CHECK, INSPECTION REPORTED SURFACE CORROSION ON FLOOR SUPPORT BETWEEN STA 987.5 AND 1006, BL 0. FABRICATED AND INSTALLED REPLACEMENT FLOOR SUPPORT PER EA 53-737-173 AND SRM 51-30-02 AND SRM 53-10-2.
- [SDR F3LA200200176](https://openairdocs.org/sdr/F3LA200200176.md): Gusset · gouged · Jun 29, 2002 · N272 · Boeing 7372P6 · Engine Cowling System
  > DURING C-2 CHECK, INSPECTION REPORTED MULTIPLE GOUGES IN NR 1 ENGINE OTBD COWLING LOWER CHORD AND GUSSET AT SECOND LATCH FITTING FROM FWD SIDE OF COWL. REMOVED DAMAGED AREA AND FABRICATED REPAIR DOUBLER PER SRM 51-40-3 AND 54-10-2. DOUBLER CHANGED THICKNESS
- [SDR F3LA200200175](https://openairdocs.org/sdr/F3LA200200175.md): Skin · dented · Jun 25, 2002 · N272 · Boeing 7372P6 · Cargo/Baggage Doors
  > DURING C-2 CHECK, INSPECTION REPORTED DENT IN AFT CARGO DOOR AT TOP OF DOOR. CUT OUT DAMAGE PER SRM 52-00-3. REMOVED STIFFENER PER SRM 51-30-02. FABRICATED DOUBLER PER SRM 52-00-03. INSTALLED REPAIR DOUBLER AND STIFFENER PER SRM 52-00-3 AND SRM 51-30-2.
- [SDR F3LA200200174](https://openairdocs.org/sdr/F3LA200200174.md): Intercostal · corroded · Jun 25, 2002 · N272 · Boeing 7372P6 · Fuselage Miscellaneous Structure
  > DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON INTERCOSTAL AT STA 500A TO 500B, RBL 25. FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL PER BOEING DRAWING 69-41473, SRM 51-30-2 AND SOPM 20-41-02.
- [SDR F3LA200200173](https://openairdocs.org/sdr/F3LA200200173.md): Cargo Track · corroded · Jun 25, 2002 · N272 · Boeing 7372P6 · Fuselage, Seat/Cargo Attach Fittings
  > DURING C-2 CHECK, INSPECTION REPORTED CORROSION ON CARGO TRACK TIE DOWN SOCKET AT STA 947, LBL 17. REMOVED SECTION OF CARGO TRACK IN AFT BAY AT LBL 17 FROM STA 917 TO STA 947. SPLICED IN NEW SECTION OF CARGO TRACK PER SRM 51-30-02, 53-40-5 AND SOPM 20-41-02.
- [SDR F3LA200200164](https://openairdocs.org/sdr/F3LA200200164.md): Skin · delaminated · Jun 5, 2002 · N272 · Boeing 7372P6 · Elevator, Plate/Skin
  > ON WALKAROUND, FLIGHT CREW REPORTED LT ELEVATOR DELAMINATED ON TRAILING EDGE. REPAIRED PER SRM 51-40-9, PARAGRAPH 4 AND EA 55-737-063.
- [SDR F3LA200200118](https://openairdocs.org/sdr/F3LA200200118.md): Light · inoperative · Mar 23, 2002 · N272 · Boeing 7372P6 · Emergency Lighting
  > MAINTENANCE REPORTED EMERGENCY PATH LIGHTING AT ROW 1 INOPERATIVE AND EXPOSED WIRES NEAR ROW 16. REPLACED AISLE PATH LIGHT SOCKET AND LENS AT ROW 1 AND REPAIRING WIRING AT ROW 16. SYSTEM CHECKED OKAY.
- [SDR F3LA200100112](https://openairdocs.org/sdr/F3LA200100112.md): Engine · out of rig · Oct 4, 2001 · N272 · Boeing 7372P6 · Engine (Turbine/Turboprop)
  > ABORTED TAKEOFF. FLIGHT CREW REPORTED NR 2 ENGINE WOULD ONLY PRODUCE 2.0 EPR OF THE REQUIRED 2.05. PUSHED RT THROTTLE ALMOST TO FWD STOP WITH NO FURTHER THRUST. ABORTED TAKEOFF AT 90 KNOTS. PERFORMED ENGINE RUN AND FOUND ALL PARAMETERS FOR NR 2 ENGINE LOWE
- [SDR F3LA200100096](https://openairdocs.org/sdr/F3LA200100096.md): Battery Pack · discharged · Jul 16, 2001 · N272 · Boeing 7372P6 · Emergency Lighting
  > PRIOR TO DEPARTURE, MAINTENANCE REPORTED BOTH EMERGENCY OVERWING EXIT LIGHTS INOPERATIVE. MAINTENANCE IS IN THE PROCESS OF TROUBLESHOOTING THE SYSTEM. AN ADDENDUM WILL BE ISSUED WHEN REPAIR IS ACCOMPLISHED. ADDENDUM: REPLACED FORWARD AND CENTER BATTERY PAC
- [SDR F3LA200100076](https://openairdocs.org/sdr/F3LA200100076.md): Fitting · loose · Jun 4, 2001 · N272 · Boeing 7372P6 · Engine Pressure Ratio (EPR)
  > REJECTED TAKEOFF. FLIGHT CREW REPORTED NR 2 ENGINE EGT EXCEEDED RED RADIAL. AN ADDENDUM WILL BE ISSUED WHEN CAUSE OF FAILURE AND CORRECTIVE ACTION IS KNOWN. ADDENDUM: PERFORMED EPR SYSTEM TEST AND FOUND NR 2 ENGINE PT7 FITTING LOOSE. TIGHTENED PT7 FITTING
- [SDR F3LA200100054](https://openairdocs.org/sdr/F3LA200100054.md): Power Supply · discharged · Apr 23, 2001 · N272 · Boeing 7372P6 · Emergency Lighting
  > PRIOR TO DEPARTURE, FLIGHT CREW REPORTED EMERGENCY AISLE PATH LIGHTING IN FWD CABIN INOPERATIVE. REPLACED FWD EMERGENCY AISLE PATH LIGHTING POWER SUPPLY.
- [SDR F3LA200100051](https://openairdocs.org/sdr/F3LA200100051.md): Angle · cracked · Mar 30, 2001 · N272 · Boeing 7372P6 · Rudder Structure
  > DURING C-1 CHECK, INSPECTION REPORTED CRACK IN ANGLE, VERTICAL STABILIZER AT APPROXIMATELY RUDDER STA 86.59. MAINTENANCE FABRICATED AND INSTALLED REPAIR ANGLES PER SRM 51-40-4.
- [SDR F3LA200100047](https://openairdocs.org/sdr/F3LA200100047.md): Skin · dented · Mar 20, 2001 · N272 · Boeing 7372P6 · Fuselage Main, Plate/Skin
  > DURING C1 CHECK, INSPECTION REPORTED 2 DENTS ON RIGHT FUSELAGE SKIN AT STA 1016, STR 20R. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED FILLER, REPAIRED DOUBLER, AND INSTALLED.
- [SDR F3LA200100045](https://openairdocs.org/sdr/F3LA200100045.md): Door · corroded · Mar 15, 2001 · N272 · Boeing 7372P6 · Electrical/Electronic Compartment Doors
  > DURING C-1 CHECK, INSPECTION REPORTED RT UPPER FWD CORNER OF E&E DOOR CORRODED. MAINTENANCE REMOVED CORROSION AND PERFORMED A WEB REPAIR PER SRM 51-40-02.
- [SDR F3LA200000275](https://openairdocs.org/sdr/F3LA200000275.md): Engine · stalled · Dec 26, 2000 · N272 · Boeing 7372P6 · Turbine Engine Compressor Section
  > REJECTED TAKEOFF. FLIGHT CREW REPORTED HEARING TWO "BANGS" WHICH WAS THOUGHT TO BE A COMPRESSOR STALL AND ABORTED TAKEOFF AT 50 KNOTS WITHOUT INCIDENT. CREW COULD NOT DETERMINE WHICH ENGINE WAS AFFECTED AS THERE WERE NO ENGINE INDICATION FLUCTUATIONS. MAINT
- [SDR F3LA200000273](https://openairdocs.org/sdr/F3LA200000273.md): Strut · collapsed · Dec 17, 2000 · N272 · Boeing 7372P6 · Main Landing Gear Strut/Axle/Truck
  > AIR TURNBACK. FLIGHT CREW REPORTED LT. MAIN LANDING GEAR UNSAFE LIGHT WOULD NOT EXTINGUISH WITH GEAR HANDLE IN "UP" POSITION. RED UNSAFE AND GREEN GEAR LIGHT ILLUMINATED WITH GEAR HANDLE IN "OFF" POSITION. AIRCRAFT RETURNED TO DEN AND LANDED WITHOUT INCIDEN
- [SDR F3LA00239](https://openairdocs.org/sdr/F3LA00239.md): Girt Bar · wrong part · Sep 12, 2000 · N1PC · Boeing 7372P6 · Emergency Equipment
  > FLT 430 - BLOCK TURN BACK, FLIGHT CREW REPORTED LEFT AFT EVACUATION SLIDE GIRT BAR WOULD NOT LOCK IN PLACE. MAINTENANCE INSTALLED CORRECT GIRT BAR PER MM 25-61-6311, PARA 5, STEP F4. (M)
- [SDR F3LA00114](https://openairdocs.org/sdr/F3LA00114.md): Light · inoperative · May 31, 2000 · N1PC · Boeing 7372P6 · Emergency Lighting
  > DEN - DURING SERVICE CHECK, MAINTENANCE REPORTED EMERGENCY FLOOR PROXIMITY LIGHT PATH STRIP INOPERATIVE AND TRACK DAMAGED AT ROW 1 THROUGH ROW 3. MAINTENANCE REPAIRED WIRING AND REPLACED LIGHT TRACK PER MM 33-50-00. (M)
- [SDR F3LA00093](https://openairdocs.org/sdr/F3LA00093.md): Line · leaking · May 17, 2000 · N1PC · Boeing 7372P6 · Hydraulic System, Main
  > LAS - FLT 778 - AIR TURN BACK. FLIGHT CREW REPORTED B-SYSTEM HYDRAULIC FAILURE. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED LEAKING HYDRAULIC LINE TO THE RUDDER PCU. (X)
- [SDR F3LA99157](https://openairdocs.org/sdr/F3LA99157.md): Skin · corroded · Nov 22, 1999 · N1PC · Boeing 7372P6 · Horizontal Stabilizer, Plate/Skin
  > DEN - DURING C-7 CHECK INSPECTION, REPORTED FORWARD TIP OF RIGHT STABILIZER CORRODED. MAINTENANCE FABRICATED REPLACEMENT PARTS AND REPAIRED PER EA NR 55-737-010. (M)
- [SDR F3LA99164](https://openairdocs.org/sdr/F3LA99164.md): Stringer · corroded · Nov 21, 1999 · N1PC · Boeing 7372P6 · Fuselage Main, Longeron/Stringer
  > DEN - DURING C-7 CHECK, INSPECTION REPORTED CORROSION ON STRINGER 26R, BS 987 TO BS 987.5. MAINTENANCE FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 53-10-3. (M)
- [SDR F3LA99137](https://openairdocs.org/sdr/F3LA99137.md): Angle · corroded · Nov 12, 1999 · N1PC · Boeing 7372P6 · Fuselage Miscellaneous Structure
  > DEN - DURING C-7 CHECK, INSPECTION REPORTED RIGHT FORWARD SERVICE DOOR INBOARD THRESHOLD SUPPORT ANGLE CORRODED. MAINTENANCE FABRICATED AND REPAIRED RIGHT FORWARD SERVICE DOOR INBOARD THRESHOLD SUPPORT ANGLE PER SRM 51-40-3. (M)

Next page: https://openairdocs.org/model/boeing-737-2p6/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 = '7372P6'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-737-2p6/reports

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