# Service difficulty reports: Boeing 737-2S3

A list on [Boeing 737-2S3](https://openairdocs.org/model/boeing-737-2s3.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 57 reports

- [SDR DL73E011337](https://openairdocs.org/sdr/DL73E011337.md): Battery Pack · discharged · Aug 13, 2001 · N369DL · Boeing 7372S3 · Emergency Lighting
  > ON INSPECTION FOUND FWD, MID, AND AFT OVERHEAD EMERGENCY EXIT LIGHTS INOP IN CABIN. REPLACED FWD BATTERY PACK, MID RT BATTERY PACK AND CHARGER ASSY AND AFT BATTERY PACK AND CHARGER ASSY. OPN OF ALL EMERGENCY LIGHTS NOW NORMAL.
- [SDR DL73E011336](https://openairdocs.org/sdr/DL73E011336.md): Battery Pack · discharged · Aug 13, 2001 · N369DL · Boeing 7372S3 · Emergency Lighting
  > ON INSPECTION FOUND OVERWING EMERGENCY EXIT LIGHTS INOP IN CABIN. REPLACED MID LEFT BATTERY PACK PER MM. OPN NORMAL.
- [SDR DL73E011295](https://openairdocs.org/sdr/DL73E011295.md): Battery · discharged · Aug 6, 2001 · N367DL · Boeing 7372S3 · Emergency Lighting
  > ON INSPECTION FOUND AFT LEFT OVER DOOR EMERGENCY EXIT SIGN INOP. REPLACED BATTERIES PER MM. OPN NORMAL
- [SDR DL73E011285](https://openairdocs.org/sdr/DL73E011285.md): Battery Pack · discharged · Jul 4, 2001 · N369DL · Boeing 7372S3 · Emergency Lighting
  > ON INSPECTION FOUND EMERGENCY LIGHTS IN CEILING OF CABIN, ALL POSITIONS INOP. BOTH CABIN OVERWING EMERGENCY LIGHTS INOP ALSO. REPLACED FWD, MID AND AFT LEFT BATTERY PACKS PER MM. CKS NORMAL.
- [SDR DL73E010864](https://openairdocs.org/sdr/DL73E010864.md): Indicator · failed · May 29, 2001 · N367DL · Boeing 7372S3 · Visual Omnirange (VOR) System
  > NR 1 INST XMFR C/B POPPED ON PRE-DEPARTURE. REPLACED CAPTS RMI DUE TO OFF FLAG IN VIEW.
- [SDR DL73E010557](https://openairdocs.org/sdr/DL73E010557.md): Frame · cracked · Apr 4, 2001 · N367DL · Boeing 7372S3 · Fuselage Main, Frame
  > CRACKS WERE FOUND IN THE FS 178 BULKHEAD LT AND RT SIDE CHORDS. ADDITIONALLY, TWO CRACKS WERE FOUND IN THE CENTER WEB AT LBL 12/WL 218 AND RBL 12/WL 234. THE WEB WAS REPAIRED PER SRM 53-10-11, FIG. 1 AND THE CHORDS WERE REPLACED PER ERA 397408-14AD. THE D
- [SDR DL73E010555](https://openairdocs.org/sdr/DL73E010555.md): Skin · cracked · Apr 4, 2001 · N367DL · Boeing 7372S3 · Fuselage Main, Plate/Skin
  > TWO CRACKS WERE FOUND IN THE FUSELAGE SKIN NEAR FS 727B, STR 17 RT AND 727A, STR 18 RT. THE CRACKS WERE CUT OUT AND AN EXTERNAL DOUBLER WAS INSTALLED PER B737-200 SRM 53-30-3, FIG6. THE DAMAGE WAS FOUND AT HMV.
- [SDR DL73E010554](https://openairdocs.org/sdr/DL73E010554.md): Skin · cracked · Apr 4, 2001 · N367DL · Boeing 7372S3 · Fuselage Main, Plate/Skin
  > A CRACK WAS FOUND IN THE LOWER HINGE CUTOUT OF THE AFT GALLEY DOOR. THE CRACK WAS COMMON TO THE SKIN, BONDED DOUBLER AND THE BEAR STRAP. THE CRACK WAS CUT OUT AND A DOUBLER / TRIPLER INSTALLED AT HMV.
- [SDR DL73E010518](https://openairdocs.org/sdr/DL73E010518.md): Floorbeam · cracked · Mar 30, 2001 · N367DL · Boeing 7372S3 · Fuselage Main, Floor Beam
  > DURING ACCOMPLISHMENT OF INSPECTION PER S/B 737-57-1210. A CRACK WAS FOUND IN THE PANEL ATTACH HOLE AT FS 660. THE CRACK WAS CUT OUT AND THE AREA REPAIRED BY S/B 737-57-1210.THE DAMAGE WAS FOUND AT HMV.
- [SDR DL73E010499](https://openairdocs.org/sdr/DL73E010499.md): Skin · cracked · Mar 27, 2001 · N367DL · Boeing 7372S3 · Fuselage Main, Plate/Skin
  > A CRACK WAS FOUND IN THE FUSELAGE SKIN AT FS 727B AND STR 16L. THE CRACK WAS CUT OUT AND REPAIRED PER SRM 53-30-3. THE DAMAGE WAS FOUND AT HMV.
- [SDR DL73E010466](https://openairdocs.org/sdr/DL73E010466.md): Frame · cracked · Mar 22, 2001 · N367DL · Boeing 7372S3 · Fuselage Main, Frame
  > A CRACK WAS FOUND IN THE WEB OF THE FS 795 FRAME BETWEEN STR 23R AND 24R. THE CRACK WAS CUT OUT AND REPAIRED PER SRM 51-40-3, FIGURE 1. THE DAMAGE WAS FOUND AT HMV.
- [SDR DL73E010049](https://openairdocs.org/sdr/DL73E010049.md): Flap Track · corroded · Jan 8, 2001 · N369DL · Boeing 7372S3 · Trailing Edge Flaps
  > INSPECTION OF THE INBD FLAP TRACK OF THE OUTBD FLAP ON THE LT WING REVEALED EXTENSIVE PITTING CORROSION. THE FLAP TRACK WAS REMOVED AND DISCARDED. A NEW FLAP TRACK WAS INSTALLED PER ER/A 379729-14AD.
- [SDR DL73E001969](https://openairdocs.org/sdr/DL73E001969.md): Intercostal · cracked · Oct 10, 2000 · N369DL · Boeing 7372S3 · Fuselage Miscellaneous Structure
  > ROUTINE INSPECTIONS OF THE FWD GALLEY DOOR (R1) SURROUND STRUCTURE PER AD 98-22-10, REVEALED A CRACK IN THE LOWER INTERCOSTAL OF THE AFT DOOR FRAME. THE CRACK IS TYPICAL OF BAC S/B 737-53A1108. THE CRACKED INTERCOSTAL WAS REMOVED AND AN IMPROVED VERSION
- [SDR DL73E001723](https://openairdocs.org/sdr/DL73E001723.md): Support Fitting · corroded · Sep 6, 2000 · N367DL · Boeing 7372S3 · Main Landing Gear Attach Section
  > THE LUG BORE OF THE FS 685 LT MLG SIDE SUPPORT FITTING WAS FOUND WITH CORROSION. THE CORROSION WAS REMOVED BY OVERSIZING THE LUG BORE. AN OVERSIZE BUSHING WAS INSTALLED. THE REPAIR WAS ACCOMPLISHED PER ER/A 378436-14.
- [SDR DL73E001722](https://openairdocs.org/sdr/DL73E001722.md): Beam · tool damage · Sep 6, 2000 · N367DL · Boeing 7372S3 · Wing Spar
  > THE AFT TRUNNION BORE OF THE LT WING MLG SUPPORT BEAM SUFFERED TOOLING DAMAGE IN THE HOLE BORE. THE BORE WAS OVERSIZED TO REMOVE THE TOOLING DAMAGE, ROTO PEENED, AND AN OVERSIZE BUSHGING INSTALLED. THE REPAIR WAS ACCOMPLISHED PER ER/A 378444-14.
- [SDR DL73E001670](https://openairdocs.org/sdr/DL73E001670.md): Link · corroded · Aug 23, 2000 · N367DL · Boeing 7372S3 · Landing Gear Retraction/Extension System
  > MLG TRUNNION LINK PITTED AND RUSTY RUST COMING OUT OF MATING SURFACES OF TRUNNION LINK ASSY AND TRUNNION PIN I/B OF MLG ACTUATOR. RIGHT MLG TRUNNION LINK PITTED/CORRODED ON I/B AND O/B FACES. RT MLG UPPER STRUT TRUNNION LUG CORROSION. RT MLG UPPER STRUT CYL
- [SDR DL73E001623](https://openairdocs.org/sdr/DL73E001623.md): Pcu · malfunctioned · Aug 19, 2000 · N367DL · Boeing 7372S3 · Rudder Control System
  > NOTICED A SHARP ABRUPT YAW INPUT SHORTLY AFTER NOSE WHEEL LIFT OFF. NO ABNORMAL WINDS OR AIRCRAFT WAKE EXISTING. YAW WAS SIGNIFICIANT, NO INPUTS NOTED IN RUDDER PEDALS BY PILOT FLYING. CHECKED YAW DAMP FOR FAULTS, NONE. REPLACED RUDDER PCU PER M/M RII. C
- [SDR DL73E001600](https://openairdocs.org/sdr/DL73E001600.md): Actuator · malfunctioned · Aug 19, 2000 · N367DL · Boeing 7372S3 · Rudder Actuator
  > NOTICED A SHARP ABRUPT YAW INPUT SHORTLY AFTER NOSE WHEEL LIFTOFF. NO ABNORMAL WINDS OR AIRCRAFT WAKE EXISTING. YAW WAS SIGNIFICANT NO INPUTS NOTED IN RUDDER PEDALS BY PILOT FLYING. REPLACING RUDDER PACK.
- [SDR DL73E001331](https://openairdocs.org/sdr/DL73E001331.md): Transmission · seized · Jul 14, 2000 · N369DL · Boeing 7372S3 · Trailing Edge Flap Control System
  > FLAPS LOCKED OUT ON APPROACH TO CAE. CREW DID GO-AROUND. FOUND FLAP TRANSMISSION SEIZED. REPLACED FLAP TRANSMISSION AND JACK SCREW ASSY, CHECKS GOOD.
- [SDR DL73E001071](https://openairdocs.org/sdr/DL73E001071.md): Engine · fod · May 31, 2000 · N369DL · Boeing 7372S3 · Engine (Turbine/Turboprop)
  > ON TAKEOFF, HEARD LOUD BANG. SUSPECT BIRD STRIKES. FOUND NR 2 ENG 1ST STAGE FAN BLADE FOD. REPLACING FAN.
- [SDR DL73E000880](https://openairdocs.org/sdr/DL73E000880.md): Skin · cracked · May 2, 2000 · N369DL · Boeing 7372S3 · Fuselage Main, Plate/Skin
  > A 2 INCH CRACK WAS FOUND EMANATING FROM UNDER A WING TO BODY FAIRING AT FS 727A+3 AND STRINGER 17L. AN EXISTING REPAIR WAS NEAR THE CRACK. THE PREVIOUS REPAIR WAS REMOVED AND THE NEW CRACK AND EXISTING REPAIR CUTOUT WERE COMBINED INTO A 20 X 11 INCH CUTOUT.
- [SDR DL73E000862](https://openairdocs.org/sdr/DL73E000862.md): Floorbeam · cracked · Apr 28, 2000 · N369DL · Boeing 7372S3 · Fuselage Main, Floor Beam
  > THE RBL 45.5 FLOOR LONGITUDINAL FLOORBEAM OVER THE MLG WHEEL WELL WAS FOUND WITH A 12 INCH CRACK IN THE BEAM WEB BETWEEN FS 633 & 645. THE CRACKED SECTION OF WEB WAS CUT AND REMOVED. A NEW SECTION OF WEB WAS SPLICED IN WITH TWO ALUMINUM SPLICE DOUBLERS
- [SDR DL73E992535](https://openairdocs.org/sdr/DL73E992535.md): damaged · Nov 16, 1999 · N369DL · Boeing 7372S3 · Flight Control System
  > RT WING OUTBOARD FLAP JACKSCREW DAMAGED. REPLACED NR 8 JACKSCREW TRANSMISSION ASSY.
- [SDR DL73E991786](https://openairdocs.org/sdr/DL73E991786.md): Light · inop · Aug 10, 1999 · N367DL · Boeing 7372S3 · Emergency Lighting
  > EMERGENCY LTS INOP LT AND RT FWD ENTRY DOOR ON OUTSIDE OF AIRCRAFT REF WDM 33-51-01. REPLACED M571. OPS NORMAL.
- [SDR DL73E991724](https://openairdocs.org/sdr/DL73E991724.md): Radar Tr Unit · inop · Aug 1, 1999 · N369DL · Boeing 7372S3 · Weather Radar System
  > WX RADAR ANT FLASHING ON SCREEN. NO RADAR AVAILABLE. REPLACED WX RARAR TRANSCEIVER.
- [SDR DL73E991322](https://openairdocs.org/sdr/DL73E991322.md): Skin · cracked · Jun 11, 1999 · N367DL · Boeing 7372S3 · Service Doors
  > DURING THE INSP OF THE R1 DOOR UPPER CORNERS SEVERAL CRACKS WERE FOUND IN THE SKIN ASSY AND BEARSTRAP. REPAIRED PER ERA 367544-14, REV A.
- [SDR DL73E990846](https://openairdocs.org/sdr/DL73E990846.md): Connector · loose · Apr 16, 1999 · N367DL · Boeing 7372S3 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS ALONG AISLE AND LOWER DOORS COME ON AND GO OFF ON THEIR OWN. FOUND WIRE LOOSE ON AFT FLT ATTENDANT PANEL EMERGENCY SWITCH. TIGHTENED CONNECTOR ON SWITCH. LIGHTS OPS CHK NML.
- [SDR DL73E990287](https://openairdocs.org/sdr/DL73E990287.md): Generator · failed · Feb 13, 1999 · N369DL · Boeing 7372S3 · AC Generator-Alternator
  > NR 1 ENG GEN FAILED SHORTLY AFTER T/O. THERE WAS NO INDICATION ON THE OVERHEAD ELECT PANEL THAT THE GENERATOR HAD FAILED. REPLACED GCU.
- [SDR DL73E990133](https://openairdocs.org/sdr/DL73E990133.md): Battery · discharged · Jan 21, 1999 · N367DL · Boeing 7372S3 · Emergency Lighting
  > EMERGENCY EXIT LIGHT BATTERIES DEAD DUE TO GND POWER LOSS. REPLACED EMERGENCY EXIT BATTERIES AND BASE ASSY.
- [SDR DL73E982420](https://openairdocs.org/sdr/DL73E982420.md): Battery Pack · discharged · Nov 23, 1998 · N369DL · Boeing 7372S3 · Emergency Lighting
  > ONE SECTION OF EMERGENCY LIGHTS REMAINED ON DURING FLT. REPLACED EMERG BATTERY PACK, OPS CK OK.
- [SDR DL73E982302](https://openairdocs.org/sdr/DL73E982302.md): Skin · cracked · Nov 6, 1998 · N367DL · Boeing 7372S3 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN WAS FOUND WITH A 1.875 INCH CRACK BELOW THE L1 DOOR AT APPROX FS 335. THE CRACK IS TYPICAL OF BAC S/B 737-53-1083. THE CRACK WAS STOP DRILLED AND REPAIRED WITH AN INTERIM DOUBLER REPAIR PER THE S/B. THE REPAIR WILL BE REPLACED WITH A PERMA
- [SDR DL73E982303](https://openairdocs.org/sdr/DL73E982303.md): Skin · cracked · Nov 4, 1998 · N369DL · Boeing 7372S3 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN, DOUBLER AND BEAR STRAP WERE FOUND WITH A 1 INCH TYPICAL CRACK IN THE LOWER FWD CORNER OF THE R2 DOOR CUTOUT. THE CRACK WAS REPAIRED PER B737 SRM 53-30-3, FIG 24 EXCEPT BLIND FASTENERS WERE AUTHORIZED ON A TIME-LIMITED BASIS. THE REPAIR WAS
- [SDR DL73E982128](https://openairdocs.org/sdr/DL73E982128.md): Floorbeam · cracked · Oct 12, 1998 · N367DL · Boeing 7372S3 · Fuselage Main, Floor Beam
  > THE UPPER CAP OF THE RBL 24.82 OVERWING PASSENGER FLOORBEAM WAS FOUND WITH A.5 INCH CRACK EMANATING FROM A CUTOUT FOR A SEAT TRACK ATTACH POINT. THE CRACK WAS STOP DRILLED AND REPAIRED WITH AN ALUMINUM REPAIR DOUBLER AND TRIPLER PER ER/A 365847-14, REV B.
- [SDR DL73E982127](https://openairdocs.org/sdr/DL73E982127.md): Skin · cracked · Oct 12, 1998 · N367DL · Boeing 7372S3 · Fuselage Main, Plate/Skin
  > THE UPPER HINGE CUTOUT OF THE L1 DOOR OPENING WAS FOUND WITH A TYPICAL CRACK IN THE SKIN AND BONDED DOUBLER. THE CRACK WAS ROUTED OUT AND REPAIRED WITH AN EXTERNAL STEEL DOUBLER PER THE B737 SRM 53-30-3 FIG 21. THE REPAIR WAS DOCUMENTED PER ER/A 365839-14, R
- [SDR DL73E981948](https://openairdocs.org/sdr/DL73E981948.md): Circuit Breaker · tripped · Sep 20, 1998 · N369DL · Boeing 7372S3 · Landing Gear Retraction/Extension System
  > AIR TURNBACK DUE TO LANDING GEAR LEVER WOULDN'T MOVE TO UP POS ON T/O. ABNORMAL PROCEDURES RUN TO RAISE LANDING GEAR. LAND GEAR EXT NORMAL ON RETURN. RESET LEVER LATCH C/B. CYCLED LAND GEAR LEVER, ALL IND NORMAL. REPLACED LEVER LATCH C/B. CYCLED L/G LEVER
- [SDR DL73E981894](https://openairdocs.org/sdr/DL73E981894.md): Audio Acc Unit · failed · Sep 12, 1998 · N367DL · Boeing 7372S3 · Audio Integrating System
  > COMM RADIO FAILURE IN FLIGHT OCCURED 5 MIN AFTER T/O. RADIOS RESTORED AFTER APU STARTED AND TRANSFERED NR 2 BUS TO APU. RAN ENGS ALL COMRADIOS CK GOOD. INSPECTED STATIC WICKS AND ANTS. ALL OK. REPLACED AUDIO ACC UNIT. ALL RADIO FUNCTIONS NORMAL.
- [SDR DL73E981449](https://openairdocs.org/sdr/DL73E981449.md): Clip · cracked · Jul 9, 1998 · N367DL · Boeing 7372S3 · Fuselage Miscellaneous Structure
  > A SKIN AND STRINGER REPAIR WERE ACCOMPLISHED AT FS 597 STR 2L. THE FRAME-TO-STRINGER CLIP INSPECTION REQUIRED PER BAC S/B 737-53-1085 (AD 93-08-04) WAS ACCOMPLISHED AT THIS LOCATION AND RESULTED IN FINDING A CRACKED CLIP. A NEW CLIP HAD TO BE MODIFIED TO ALL
- [SDR DL73E981447](https://openairdocs.org/sdr/DL73E981447.md): Clips · cracked · Jul 8, 1998 · N367DL · Boeing 7372S3 · Fuselage Miscellaneous Structure
  > WHILE ACCOMPLISHING REPLACEMENT OF CRACKED FRAME-TO-STRINGER CLIPS PER BAC S/B 737-53-1085 (AD 93-08-04), MTC. WAS UNABLETO INSTALL THE REQUIRED RIVETS. THE RIVETS WERE SUBSTITUTED WITH STEEL HI-LOKS PER ER/A 365196-14AD, REV A.
- [SDR DL73E980955](https://openairdocs.org/sdr/DL73E980955.md): Skin · punctured · Apr 30, 1998 · N369DL · Boeing 7372S3 · Fuselage Main, Plate/Skin
  > A 1.5 X 1.5 PUNCTURE WAS FOUND IN THE FUSELAGE SKIN JUST AFT OF STA 460 BELOW THE STRINGER 25R SKIN LAP SPLICE. THE PUNCTURE WAS TRIMMED TO A SMOOTH CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER AND AN ADDITIONAL DOUBLER TO OVERLAP THE SKIN LAP SPLICE
- [SDR DL73E980935](https://openairdocs.org/sdr/DL73E980935.md): Bolt · loose · Apr 29, 1998 · N369DL · Boeing 7372S3 · Trailing Edge Flaps
  > DURING AD MANDATED INSPECTION, THE OUTBD BOLT ON THE NR 3 FLAP OUTBD TRACK AFT ATTACH FITTING WAS FOUND LOOSE. THE CONDITION WAS CORRECTED BY INSTALLING THE TRACK MODIFICATION PER BAC S/B 737-57A1130. THE MODIFICATION WAS DOCUMENTED PER ER/A 364643-14AD.
- [SDR DL73E980720](https://openairdocs.org/sdr/DL73E980720.md): Anti-Ice · odor · Apr 2, 1998 · N369DL · Boeing 7372S3 · Engine Anti-Icing System
  > AT 25,000, AN ELECTRICAL SMELL WAS NOTED IN ENTIRE AIRCRAFT WHEN ENGINE ANTI-ICE WAS TURNED ON. SMELL WENT AWAY WHEN ENGINE ANTI-ICE TURNED OFF. RAN ENGINES AND PACKS, INSPECTED FOR SOURCE, NO TROUBLE FOUND.
- [SDR DL73E980037](https://openairdocs.org/sdr/DL73E980037.md): Skin · cracked · Jan 6, 1998 · N367DL · Boeing 7372S3 · Fuselage Main, Plate/Skin
  > FUSELAGE/SKIN, FS 727A-727B, S-16R-17R, REPAIRED FOR SKIN CRACKS. THE FUSELAGE SKIN BETWEEN FS 727A AND 727B AND BETWEEN STRINGER 16R AND 17R WAS FOUND WITH A 3.25 LONG CRACK AND A 2.25 LONG CRACK. THE CRACKS WERE CUT OUT AND A REPAIR DOUBLER WAS INSTALLED P
- [SDR DL73E971682](https://openairdocs.org/sdr/DL73E971682.md): Skin · cut · Aug 22, 1997 · N369DL · Boeing 7372S3 · Fuselage Main, Plate/Skin
  > WHILE ACCOMPLISHING THE REPLACEMENT OF STA 727 FRAME CHORD PER E.O. 3-68646-3AD, THE FUSELAGE SKIN BETWEEN ST 727 BULKHEAD AND STA 727+10 WAS CUT IN ORDER TO PROVIDE ACCESS FOR THE CHORD REPLACEMENT. WHEN CUTTING THE SKIN, MX ALSO CUT THE INTERNAL BONDED WAFF
- [SDR DL73E971681](https://openairdocs.org/sdr/DL73E971681.md): Frame · cracked · Aug 22, 1997 · N369DL · Boeing 7372S3 · Fuselage Main, Frame
  > THE FS 727 BULKHEAD O/B CHORD AT STR 18A WAS FOUND CRACKED AND IS BEING REPLACED PER BACO DWG 65C33722, AS REQUIRED BY DAL EO 3-68646-3AD, WHICH ACCOMPLISHES S/B 737-53-1088. BETWEEN STR S-24 AND S-27, BACB30FP* FASTENERS, SAME SIZE AS REQUIRED BY BP, WERE IN
- [SDR DL73E971680](https://openairdocs.org/sdr/DL73E971680.md): Frame · cracked · Aug 22, 1997 · N369DL · Boeing 7372S3 · Fuselage Main, Frame
  > WHILE ACCOMP INSPECTIONS REQUIRED BY AD 95-12-17, A TYPICAL CRACK WAS FOUND IN THE BS 727 FRAME, OUTBOARD CHORD AT STR 18A, LHS. THE CHORD WILL BE REPLACED PER S/B 737-53-1088 AND A PREVENTATIVE MODIFICATION WILL BE ACCOMP PER S/B 737-53A1166. THE S/B REQUIR
- [SDR DL73E970856](https://openairdocs.org/sdr/DL73E970856.md): Light · inop · May 5, 1997 · N369DL · Boeing 7372S3 · Emergency Lighting
  > ON L/O, FOUND EMERGENCY EXIT LIGHT ABOVE 2L DOOR INOP. REPLACED LIGHT ASSEMBLY.
- [SDR DL73E970290](https://openairdocs.org/sdr/DL73E970290.md): Intercostal · cracked · Feb 12, 1997 · N367DL · Boeing 7372S3 · Fuselage Miscellaneous Structure
  > THE R-1 DOOR FRAME INTERCOSTALS AT STR 8A,10A, 11A WERE FOUND CRACKED IN THE TYPICAL MANNER SHOWN IN S/B 737-53A1108, REV 5. THIS ER/A ACCOMPLISHED A REPAIR AT THIS LOCATION WITH THE LISTED S/B AND AD 88-03-03. REPETITIVE INSPECTIONS PER EO 3-55852-12AD MUS
- [SDR DL73E970200](https://openairdocs.org/sdr/DL73E970200.md): Uplock Sensor · malfunctioned · Feb 1, 1997 · N367DL · Boeing 7372S3 · Landing Gear Position and Warning
  > LEFT GEAR RED ON RETRACTION. RETURNED TO CVG. CORRECTIVE ACTION NECESSARY TO DO GEAR SWING. CHECKING UPLOCK. REPLACED UPLOCK SENSOR. CHECKS OK.
- [SDR DL73E962787](https://openairdocs.org/sdr/DL73E962787.md): Pwr Supply · inoperative · Dec 30, 1996 · N367DL · Boeing 7372S3 · Emergency Lighting
  > BOTH LT AND RT LOWER EMERG DOOR EXIT IDENTIFIERS INOP. REPLACED EMERG LIGHT PWR SUPPLY PACK M9027, OPS GOOD PER MM.
- [SDR DL73E962403](https://openairdocs.org/sdr/DL73E962403.md): Transmitter · inoperative · Oct 28, 1996 · N367DL · Boeing 7372S3 · Trailing Flap Position Indicating System
  > FLAPS FAILED TO EXTEND. REPLACED LT FLAP POS TRANSMITTER AND INDICATOR, OPER CK OK.

Next page: https://openairdocs.org/model/boeing-737-2s3/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 = '7372S3'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-737-2s3/reports

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