# Service difficulty reports: Boeing 737-36M

A list on [Boeing 737-36M](https://openairdocs.org/model/boeing-737-36m.md).

Newest first. General aviation reporting is voluntary.

- [SDR PIDA200500011](https://openairdocs.org/sdr/PIDA200500011.md): Attach Angle · cracked · Apr 19, 2005 · N374PA · Boeing 73736M · Fuselage Miscellaneous Structure
  > UPPER ATTACH ANGLE ON INTERCOSTAL AT BL 0 BETWEEN BS 380 AND BS 400 AT WL 208 IS CRACKED. REPLACED ANGLE PER SRM 51-10-02.
- [SDR PIDA200500006](https://openairdocs.org/sdr/PIDA200500006.md): Frame · cracked · Apr 19, 2005 · N374PA · Boeing 73736M · Fuselage Main, Frame
  > TWO CRACKS AT RIVET HOLE IN BS 867 FRAME AT STR 9 RT. REPAIRED PER SRM 53-00-07.
- [SDR PIDA200500004](https://openairdocs.org/sdr/PIDA200500004.md): Frame · cracked · Apr 19, 2005 · N374PA · Boeing 73736M · Fuselage Main, Frame
  > TWO CRACKS IN BS 787 FRAME AT RIVET HOLE AT STR 9RT. REPAIRED PER SRM 53-00-07.
- [SDR PIDA200500013](https://openairdocs.org/sdr/PIDA200500013.md): Intercostal · cracked · Apr 19, 2005 · N374PA · Boeing 73736M · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT BS 540 CRACKED AT I/B AFT ATTACH FASTENER AT RBL 1. REPLACED INTERCOSTAL PER DWG 65-52894 AND SRM 51-10-2.
- [SDR PIDA200500008](https://openairdocs.org/sdr/PIDA200500008.md): Frame · cracked · Apr 19, 2005 · N374PA · Boeing 73736M · Fuselage Main, Frame
  > TWO CRACKS IN BS 827 FRAME AT STR 9 LT. REPAIRED PER SRM 53-00-07.
- [SDR PIDA200500007](https://openairdocs.org/sdr/PIDA200500007.md): Frame · cracked · Apr 19, 2005 · N374PA · Boeing 73736M · Fuselage Main, Frame
  > TWO CRACKS IN BS 787 FRAME AT STR 9 LT. REPAIRED PER SRM 53-00-07.
- [SDR PIDA200500009](https://openairdocs.org/sdr/PIDA200500009.md): Frame · cracked · Apr 19, 2005 · N374PA · Boeing 73736M · Fuselage Main, Frame
  > TWO CRACKS IN BS 867 FRAME AT STR 9LT. REPAIRED PER SRM 53-00-07.
- [SDR PIDA200500012](https://openairdocs.org/sdr/PIDA200500012.md): Channel · cracked · Apr 19, 2005 · N374PA · Boeing 73736M · Fuselage, Equipment Attach Fittings
  > CRACK IN LOWER RADIUS AT AFT END OF THE LEFT MOUNT HAT CHANNEL FOR THE RADAR TR UNIT. REPAIRED HAT CHANNEL PER SRM 51-70-12.
- [SDR PIDA200500010](https://openairdocs.org/sdr/PIDA200500010.md): Web · cracked · Apr 19, 2005 · N374PA · Boeing 73736M · Fuselage Miscellaneous Structure
  > FOUR CRACKS IN WEB PANEL AT LBL 4 BETWEEN BS 967 AND BS 986. REPAIRED PER DWG 65-46816 AND SRM 51-10-2.
- [SDR PIDA200500015](https://openairdocs.org/sdr/PIDA200500015.md): Support Angle · cracked · Apr 19, 2005 · N374PA · Boeing 73736M · Wing, Control Surface Attach Fittings
  > NUMBER 5 SPOILER O/B HINGE I/B SUPPORT ANGLE CRACKED. REPLACED SUPPORT ANGLE PER SRM 51-10-2.
- [SDR PIDA200500003](https://openairdocs.org/sdr/PIDA200500003.md): Floorbeam · corroded · Apr 19, 2005 · N374PA · Boeing 73736M · Fuselage Main, Floor Beam
  > CORROSION AT CLIP NUT HOLE AT LBL 27 ON FLOORBEAM AT BS 312. REPAIRED PER SRM 53-10-51.
- [SDR PIDA200500014](https://openairdocs.org/sdr/PIDA200500014.md): Support Angle · cracked · Apr 19, 2005 · N374PA · Boeing 73736M · Wing, Control Surface Attach Fittings
  > NUMBER 5 SPOILER I/B ATTACH BRACKET SUPPORT ANGLES CRACKED. REPLACED ANGLES PER SRM 51-10-2.
- [SDR PIDA200500005](https://openairdocs.org/sdr/PIDA200500005.md): Frame · cracked · Apr 19, 2005 · N374PA · Boeing 73736M · Fuselage Main, Frame
  > TWO CRACKS IN BS 827 FRAME AT STR 9RT. REPAIRED PER SRM 53-00-07.
- [SDR PIDA200500002](https://openairdocs.org/sdr/PIDA200500002.md): Skin Panel · damaged · Apr 19, 2005 · N374PA · Boeing 73736M · Fuselage Main, Plate/Skin
  > IMPACT DAMAGE (DENT) AT BS 483 SKIN PANEL BETWEEN STR 21 LT AND STR 22 LT. REPAIRED PER SRM 53-00-01 FIG 229.
- [SDR PIDA200500001](https://openairdocs.org/sdr/PIDA200500001.md): Skin · damaged · Apr 19, 2005 · N374PA · Boeing 73736M · Fuselage Main, Plate/Skin
  > IMPACT DAMAGE TO THE FUSELAGE SKIN, FORWARD ENTRANCE DOORWAY BEARSTRAP AND BS 294.5 BULKHEAD SHEAR TIE AND WEB BETWEEN STR 19LT AND STR 20LT. REPAIRED PER EA 53-074.
- [SDR 374PA0012](https://openairdocs.org/sdr/374PA0012.md): Circuit Breaker · failed · Sep 3, 2004 · N374PA · Boeing 73736M · Autopilot System
  > AUTO PILOT DISENGAGES BY ITSELF AND AURAL WARNING CIRCUIT BREAKER KEEPS POPPING OUT AFFECTING AUTO PILOT DISCONNECT HORN. REPLACED AURAL WARNING CIRCUIT BREAKER PER MM 31-26-00 AND OPS CHECKED. PERFORMED SELF TEST OF AUTO PILOT SYSTEM PER MM 22-02-10 AND 22-
- [SDR 374PA0013](https://openairdocs.org/sdr/374PA0013.md): Line · loose · Sep 2, 2004 · N374PA · Boeing 73736M · Compressor Bleed Valve
  > RIGHT ENGINE DOESN'T SPOOL UP. ADJUSTED GROUND IDLE PER MM. ADJUSTED SPECIFIC GRAVITY PER MM. TIGHTENED LINE AT BLEED REGULATOR. BOTH ENGINES OPERATE NORMAL PER MM.
- [SDR 374PA0011](https://openairdocs.org/sdr/374PA0011.md): Skin · dented · May 17, 2004 · N374PA · Boeing 73736M · Fuselage Main, Plate/Skin
  > DENT AT RIGHT SIDE OF AIRCRAFT AT BS 312 AND STR 20. REPAIRED PER SRM 53-00-01 AND EA 53-121.
- [SDR 374PA0010](https://openairdocs.org/sdr/374PA0010.md): Skin · dented · May 17, 2004 · N374PA · Boeing 73736M · Fuselage Main, Plate/Skin
  > DENT IN FUSELAGE SKIN AFT OF L1 DOOR AT STA 400 BETWEEN STR 17 LT AND STR 18 LT. REPAIRED AREA PER SRM 53-00-01 AND EA 53-120.
- [SDR 374PA0009](https://openairdocs.org/sdr/374PA0009.md): Threshold · cracked · May 17, 2004 · N374PA · Boeing 73736M · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR CENTER SECTION OF THRESHOLD CRACKED. WELDED PER BAC 5975.
- [SDR 374PA0008](https://openairdocs.org/sdr/374PA0008.md): Angle · corroded · May 17, 2004 · N374PA · Boeing 73736M · Fuselage Miscellaneous Structure
  > CORROSION ON LT TRANSITION ANGLE IN AFT CARGO BIN FROM BS 727E TO AFT END. FABRICATED AND INSTALLED REPLACEMENT TRANSITION ANGLE IAW SRM 53-60-53.
- [SDR 374PA0007](https://openairdocs.org/sdr/374PA0007.md): Bolt · loose · Mar 3, 2004 · N374PA · Boeing 73736M · Fasteners
  > FOUND FIVE BOLTS LOOSE DURING INSPECTION OF RUDDER FLANGE BOLTS PER PARA (A) & (B) OF AD 2003-26-01 AND BOEING SB 737-55A1087. REPLACED HARDWARE AT LOCATIONS F1, F2, F3, F4, F10 PER BOEING SERVICE BULLETIN.
- [SDR 374PA0006](https://openairdocs.org/sdr/374PA0006.md): Warning Horn · false activation · Jan 24, 2004 · N374PA · Boeing 73736M · Leading Edge Slat Position Indicating System
  > WARNING HORN ON TAKEOFF ROLL. NO LEADING EDGE FLAP/SLAT INDICATION. RESET LEADING EDGE POSITION INDICATOR CIRCUIT BREAKER. SYSTEM OPS CHECKS GOOD PER MM 27-88-00.
- [SDR 374PA0005](https://openairdocs.org/sdr/374PA0005.md): Skin · damaged · Nov 21, 2003 · N374PA · Boeing 73736M · Fuselage Main, Plate/Skin
  > FUSELAGE DAMAGED LEFT SIDE FROM BS 907 TO BS 927 AT STR 16 LT, AT BS 907 BETWEEN STR 21 LT AND 22 LT AND FRAME SHEAR TIE DAMAGED AT BS 908 BETWEEN STR 21 LT AND STR 22 LT. REPAIRED DAMAGE PER EA NOS 53-327, 53-331, AND 53-332.
- [SDR 374PA0004](https://openairdocs.org/sdr/374PA0004.md): Lamp · inoperative · Nov 2, 2003 · N374PA · Boeing 73736M · Emergency Lighting
  > RT EMERGENCY OVERWING EXIT SIGN LOCATOR LIGHT INOPERATIVE. RE-LAMPED LOCATOR LIGHT IAW MM 33-51-11. OPS CHECKS NORMAL.
- [SDR 374PA0003](https://openairdocs.org/sdr/374PA0003.md): Coupler · failed · Aug 9, 2003 · N374PA · Boeing 73736M · Autopilot System
  > YAW DAMPER OFF LIGHT ILLUMINATED (YAW DAMPER DC CIRCUIT BREAKER POPPED). REPLACED YAW DAMPER COUPLER PER MM 22-13-00. OPS CHECKS GOOD.
- [SDR 374PA0002](https://openairdocs.org/sdr/374PA0002.md): Battery · discharged · Jan 12, 2003 · N374PA · Boeing 73736M · Emergency Equipment
  > FWD FLIGHT ATTENDANT JUMPSEAT OUTBOARD EMERGENCY FLASHLIGHT LED WILL NOT FLASH. ITEM DEFERRED PER MEL 25-12, CONTROL NR 0112001. 1/15/2003. R & R BATTERY POWER UNIT AS REQUIRED. OPS CHECK NORMAL. CLEARED MEL 25-12, CONTROL NR 0112001
- [SDR 374PA0001A](https://openairdocs.org/sdr/374PA0001A.md): Sensor · failed · Oct 4, 2002 · N374PA · Boeing 73736M · Leading Edge Slat Control System
  > TAKEOFF WARNING HORN ACTIVATED DURING T/O ROLL, OBSERVED LE FLAPS TRANSIT LIGHT ILLUMINATED, PERFORMED RTO. FOUND NR 1 KRUGER FLAP POSITION SENSOR BAD. R&R PROXIMITY SENSOR PER MM 27-88-11, OPS CHECKED. GOOD.
- [SDR 374PA0001](https://openairdocs.org/sdr/374PA0001.md): Sensor · Oct 4, 2002 · N374PA · Boeing 73736M · Leading Edge Slat Control System
  > Takeoff warning horn activated during T/O roll, observed LE flaps transit light illuminated, performed RTO. R&R #1&2 tires and brakes, R&R #3&4 brakes per 32-41 & 32-45; insp anti-skid system per 32-42-00 OK; performed T/O warning test per AD 88-22-09 OK; bra

## 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 = '73736M'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-737-36m/reports

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