# Service difficulty reports: Boeing 737-2B7 A list on [Boeing 737-2B7](https://openairdocs.org/model/boeing-737-2b7.md). Newest first. General aviation reporting is voluntary. Page 1 of 28 · 1,360 reports - [SDR EE4Y2020121511965](https://openairdocs.org/sdr/EE4Y2020121511965.md): Floor Support · cracked · Dec 15, 2020 · N288AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > UPPER FUSELAGE, MAIN CABIN FROM BS 312 TO BS 328 AT LBL 48", INTERCOSTAL WITH CRACK. IT WAS REPAIRED, AS PER B737-400 SRM INSTRUCTIONS REF JOB: A1J185 NRI: 2-41. - [SDR EE4Y2020121511964](https://openairdocs.org/sdr/EE4Y2020121511964.md): Shear Tie · corroded · Dec 15, 2020 · N288AU · Boeing 7372B7 · Fuselage Internal Mounting Structure > LOWER FUSELAGE, AFT CARGO COMPARTMENT AT BS 967 BETWEEN STRINGER 25RH AND STRINGER 26RH, SHEAR TIE WITH CORROSION. NOTE: IT WAS REPAIRED, AS PER B737-400 SRM INSTRUCTIONS REF JOB: A1J185 NRI: 1-77. - [SDR EE4Y2020121511963](https://openairdocs.org/sdr/EE4Y2020121511963.md): Shear Tie · corroded · Dec 15, 2020 · N288AU · Boeing 7372B7 · Fuselage Internal Mounting Structure > LOWER FUSELAGE, FORWARD CARGO COMPARTMENT, AT BS 520 BETWEEN STRINGER 27LH AND STRINGER 28LH. SHEAR TIE FRAME WITH CORROSION. NOTE: IT WAS REPAIRED, AS PER B737-400 SRM INSTRUCTIONS REF JOB: A1J185 NRI: 1-25. - [SDR EE4Y2020121511962](https://openairdocs.org/sdr/EE4Y2020121511962.md): Shear Tie · corroded · Dec 15, 2020 · N288AU · Boeing 7372B7 · Fuselage Internal Mounting Structure > LOWER FUSELAGE, FORWARD CARGO COMPARTMENT, AT BS 520 BETWEEN STRINGER 27RH AND STRINGER 28RH, SHEAR TIE FRAME WITH CORROSION. NOTE: IT WAS REPAIRED, AS PER B737-400 SRM INSTRUCTIONS REF: JOB: A1J185 NRI: 1-23. - [SDR EE4Y2020121511961](https://openairdocs.org/sdr/EE4Y2020121511961.md): Intercostal · cracked · Dec 15, 2020 · N288AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > LOWER FUSELAGE, FORWARD CARGO COMPARTMENT AT BS 500F BETWEEN STRINGER 25RH AND STRINGER 26RH, INTERCOSTAL ANGLE WITH CRACK. NOTE: IT WAS REPAIRED, AS PER B737-400 SRM INTRUCTION (REF: JOB: A1J185 NRI: 1-21). - [SDR USAASB01322](https://openairdocs.org/sdr/USAASB01322.md): Battery · discharged · Nov 22, 2001 · N282AU · Boeing 7372B7 · Emergency Lighting > TPA - THE EMERGENCY EXIT LIGHT ABOVE THE FORWARD ENTRY DOOR WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. (M) - [SDR USAASB01321](https://openairdocs.org/sdr/USAASB01321.md): Wire · broken · Nov 20, 2001 · N268AU · Boeing 7372B7 · Light System Wiring > PVD - THE EMERGENCY LIGHT AT SEAT 12 WAS INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE. (M) - [SDR USAASB01316](https://openairdocs.org/sdr/USAASB01316.md): Light · inoperative · Nov 17, 2001 · N278AU · Boeing 7372B7 · Emergency Lighting > LGA - COCKPIT EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT ASSEMBLY. (M) - [SDR USAASB01312](https://openairdocs.org/sdr/USAASB01312.md): Battery · discharged · Nov 15, 2001 · N282AU · Boeing 7372B7 · Emergency Lighting > LGA - MAINTENANCE FOUND THE FORWARD SERVICE DOOR AND FORWARD ENTRY DOOR EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERIES. OPERATIONAL CHECK GOOD. (M) - [SDR USAASB01300](https://openairdocs.org/sdr/USAASB01300.md): Battery · discharged · Oct 18, 2001 · N279AU · Boeing 7372B7 · Emergency Lighting > LGA - THE EMERGENCY LIGHT ABOVE THE R2 SERVICE DOOR WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. (M) - [SDR USAASB01298](https://openairdocs.org/sdr/USAASB01298.md): Battery Pack · discharged · Oct 18, 2001 · N279AU · Boeing 7372B7 · Emergency Lighting > LGA - THE LEFT OVERWING EMERGENCY LIGHT WAS DIM. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK. (M) - [SDR 2001F00636](https://openairdocs.org/sdr/2001F00636.md): Battery Pack · discharged · Oct 10, 2001 · N277AU · Boeing 7372B7 · Emergency Lighting > BWI - MAINTENANCE FOUND THE FORWARD ENTRY DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK (P/N 61-0478-9) AND POWER SUPPLY (P/N 6013211). OPERATIONAL CHECK GOOD. REF USAASB01293. (M) - [SDR USAASB01293](https://openairdocs.org/sdr/USAASB01293.md): Battery Pack · discharged · Oct 10, 2001 · N277AU · Boeing 7372B7 · Emergency Lighting > BWI - MAINTENANCE FOUND THE FORWARD ENTRY DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK (P/N 61-0478-9) AND POWER SUPPLY (P/N 6013211). OPERATIONAL CHECK GOOD. (M) - [SDR USAASB01283](https://openairdocs.org/sdr/USAASB01283.md): Battery · discharged · Oct 6, 2001 · N279AU · Boeing 7372B7 · Emergency Lighting > PVD - THE EMERGENCY LIGHT ABOVE THE AFT RIGHT SERVICE DOOR WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. (M) - [SDR USAASB01280](https://openairdocs.org/sdr/USAASB01280.md): Battery · discharged · Oct 3, 2001 · N279AU · Boeing 7372B7 · Emergency Lighting > TPA - THE EMERGENCY LIGHT ABOVE THE AFT RIGHT SERVICE DOOR WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. (M) - [SDR USAASB01272](https://openairdocs.org/sdr/USAASB01272.md): Light · inoperative · Sep 27, 2001 · N270AU · Boeing 7372B7 · Emergency Lighting > BWI - THE LEFT AFT EMERGENCY EXIT DOOR LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT ASSEMBLY. (M) - [SDR USAASB01267](https://openairdocs.org/sdr/USAASB01267.md): Battery · discharged · Sep 24, 2001 · N270AU · Boeing 7372B7 · Emergency Lighting > BWI - THE EMERGENCY EXIT LIGHT ABOVE THE MAIN ENTRY DOOR WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. (M) - [SDR USAA011287](https://openairdocs.org/sdr/USAA011287.md): Frame · cracked · Sep 20, 2001 · N283AU · Boeing 7372B7 · Fuselage Main, Frame > CLT - FOUND OUTER CHORD CRACKED 1 INCH, BS 178 WL 207 RBL 25. INSTALLED NEW RIGHT CHORD SEGMENTS AND SPLICE PARTS PER EO 5300V157. (M) - [SDR USAASB01260](https://openairdocs.org/sdr/USAASB01260.md): Light · missing · Sep 15, 2001 · N266AU · Boeing 7372B7 · Emergency Lighting > LGA - THE LOW LEVEL EMERGENCY LIGHT AT SEAT ROW 16 WAS MISSING. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) - [SDR USAA011234](https://openairdocs.org/sdr/USAA011234.md): Intercostal · cracked · Sep 12, 2001 · N275AU · Boeing 7372B7 · Fuselage Structure (General) > CLT - FOUND INTERCOSTAL 1.5 INCH, BS 180 WL 195 RBL 26. REMOVED AND REPLACED INTERCOSTAL PER EO 5300V157. (M) - [SDR USAA011233](https://openairdocs.org/sdr/USAA011233.md): Web · cracked · Sep 12, 2001 · N275AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > CLT - FOUND FLOOR WEB CRACKED.25 INCH, WL 207 BS 180 RBL 26. REMOVED AND REPLACED FLOOR WEB PER EO 5300V157. (M) - [SDR USAA011226](https://openairdocs.org/sdr/USAA011226.md): Intercostal · cracked · Sep 10, 2001 · N275AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > CLT - FOUND INTERCOSTAL CRACKED 1.5 INCH, BS 180 WL 195 LBL 26. INSTALLED DOUBLER PER EO NR 5300V157. (M) - [SDR USAA011225](https://openairdocs.org/sdr/USAA011225.md): Web · cracked · Sep 10, 2001 · N275AU · Boeing 7372B7 · Fuselage Main, Structure > CLT - FOUND WEB CRACKED.75 INCH, BS 178, RBL 10, WL 234. INSTALLED REPAIR DOUBLER PER EA 85403. (M) - [SDR USAA011224](https://openairdocs.org/sdr/USAA011224.md): Web · cracked · Sep 10, 2001 · N275AU · Boeing 7372B7 · Fuselage Structure (General) > CLT - FOUND WEB CRACKED.75 INCH, BS 178, LBL 10, WL 234. REPAIR DOUBLER INSTALLED PER EA 85403. (M) - [SDR USAA011221](https://openairdocs.org/sdr/USAA011221.md): Frame · cracked · Sep 10, 2001 · N275AU · Boeing 7372B7 · Fuselage Main, Frame > CLT - FOUND CHORD CRACKED 1.75 INCH, BS 178 BULKHEAD, WL 207, LEFT SIDE CHORD. SPLICED IN NEW SECTION OF CHORD. (M) - [SDR USAA011220](https://openairdocs.org/sdr/USAA011220.md): Frame · cracked · Sep 10, 2001 · N275AU · Boeing 7372B7 · Fuselage Main, Frame > CLT - FOUND CHORD CRACKED.09 INCH, BS 178 BULKHEAD, WL 207, RIGHT SIDE CHORD. SPLICED IN NEW SECTION OF CHORD PER EO NR 5300V157. (M) - [SDR USAASB01247](https://openairdocs.org/sdr/USAASB01247.md): Socket · damaged · Sep 5, 2001 · N279AU · Boeing 7372B7 · Emergency Lighting > BWI - THE LEFT AFT OVERWING EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT REFLECTOR AND LAMP SOCKET ASSEMBLY. (M) - [SDR USAA011166](https://openairdocs.org/sdr/USAA011166.md): Frame · cracked · Aug 29, 2001 · N273AU · Boeing 7372B7 · Fuselage Main, Frame > CLT - FOUND CHORD CRACKED.5 INCH, IN RADIUS OF LEFT SIDE CHORD BS 178 AT WL 196 AND WL 207. SPLICED IN ANGLE AND DOUBLER STRAP PER EO 5300V157. (M) - [SDR USAA011165](https://openairdocs.org/sdr/USAA011165.md): Web · cracked · Aug 29, 2001 · N273AU · Boeing 7372B7 · Fuselage Main, Plate/Skin > CLT - FOUND WEB CRACKED 1 INCH, BS 179, WL 207, RBL 24. REMOVED AND REPLACED PART WITH NR 65-45833U40. (M) - [SDR USAA011164](https://openairdocs.org/sdr/USAA011164.md): Web · cracked · Aug 29, 2001 · N273AU · Boeing 7372B7 · Fuselage Main, Structure > CLT - FOUND WEB CRACKED FIVE PLACES.25 INCH EACH, BS 178, WL 234, LBL 10. INSTALLED DOUBLER ON WEB, CRACK CUT OUT OF WEB PER EO 5300V153 AND SRM 53-10-08 FIG 209. (M) - [SDR USAA011163](https://openairdocs.org/sdr/USAA011163.md): Frame · cracked · Aug 29, 2001 · N273AU · Boeing 7372B7 · Fuselage Main, Frame > CLT - FOUND SIDE CHORD CRACKED.5 INCH, BS 178 BULKHEAD, WL 207 AND WL 196, LEFT SIDE CHORD. INSTALLED NEW CHORD SECTION AND SPLICE PARTS. (M) - [SDR USAA011162](https://openairdocs.org/sdr/USAA011162.md): Stiffener · cracked · Aug 29, 2001 · N273AU · Boeing 7372B7 · Fuselage Miscellaneous Structure > CLT - FOUND VERTICAL CHORD CRACKED.5 INCH AND.9 INCH, BS 178 BULKHEAD LBL 5-7 VERTICAL CHORD, WL 184. INSTALLED REPAIR DOUBLER PER EO NR 5300V155. (M) - [SDR USAA011161](https://openairdocs.org/sdr/USAA011161.md): Web · cracked · Aug 29, 2001 · N273AU · Boeing 7372B7 · Fuselage Structure (General) > CLT - FOUND WEB CRACKED.5 INCH, BS 178 BULKHEAD WL 2.8, LBL 11.7. CUT OUT DAMAGE FABRICATED FILLER AND DOUBLER PER EA 85310 AND SRM 53-10-08 FIG 211. (M) - [SDR USAA011160](https://openairdocs.org/sdr/USAA011160.md): Bulkhead · cracked · Aug 29, 2001 · N273AU · Boeing 7372B7 · Fuselage Main, Bulkhead > CLT - FOUND WEB PRESSURE CRACKED.06 AND.08 INCH, BS 178 BULKHEAD WEB, LBL.5 AND RBL.5, WL 188. CUT OUT CRACKS AND INSTALLED DOUBLER PER EA 85310. (M) - [SDR USAA011159](https://openairdocs.org/sdr/USAA011159.md): Web · cracked · Aug 29, 2001 · N273AU · Boeing 7372B7 · Fuselage Structure (General) > CLT - FOUND WEB CRACKED.6 INCHES, BS 178, WL 188 AT RBL.5 AND LBL.5 INCH. INSTALLED WEB REPAIR PER EA 85310, EO 5300V152. (M) - [SDR USAASB01240](https://openairdocs.org/sdr/USAASB01240.md): Battery · inoperative · Aug 23, 2001 · N288AU · Boeing 7372B7 · Emergency Lighting > BWI - THE AFT ENTRY/SERVICE DOOR EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M) - [SDR USAASB01220](https://openairdocs.org/sdr/USAASB01220.md): Battery Pack · inoperative · Aug 2, 2001 · N278AU · Boeing 7372B7 · Emergency Lighting > TPA - DURING OVERNIGHT CHECK, MAINTENANCE FOUND BOTH AFT EXTERIOR ESCAPE SLIDE EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK IN THE AFT CARGO COMPARTMENT, RIGHT SIDE. OPERATIONAL CHECK NORMAL. (M) - [SDR USAASB01207](https://openairdocs.org/sdr/USAASB01207.md): Battery Pack · discharged · Jul 18, 2001 · N274AU · Boeing 7372B7 · Emergency Lighting > TPA - AFT LEFT AND RIGHT EVACUATION SLIDE EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACKS. (M) - [SDR P2EA01132](https://openairdocs.org/sdr/P2EA01132.md): Autothrust Sys · inoperative · Jul 18, 2001 · N128NJ · Boeing 7372B7 · Auto Throttle System > FLT 8140 - MCI - AUTO THROTTLE INOPERATIVE, DEFERRED PER MEL 22-04, CONTROL NR M128719, PER MX CONTROL MCGRATH. (M) - [SDR USAASB01206](https://openairdocs.org/sdr/USAASB01206.md): Light · failed · Jul 17, 2001 · N283AU · Boeing 7372B7 · Emergency Lighting > ALB - THE AFT SERVICE DOOR EMERGENCY EXIT SIGN WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT ASSEMBLY. (M) - [SDR P2EA01126](https://openairdocs.org/sdr/P2EA01126.md): Skin · cracked · Jul 13, 2001 · N128NJ · Boeing 7372B7 · Trailing Edge Flaps > SJO - DURING C-CHECK, FOUND LEFT OUTBOARD MID FLAP AT FORE FLAP CENTER TRACK CAVITY, SKIN WITH CRACK. REPAIRED LEFT WING OUTBOARD MID FLAP, CENTER TRACK CAVITY SKIN SECTION DUE TO CRACK IAW COOPESA EO NR COO-3-57-332-01. (M) - [SDR USAASB01194](https://openairdocs.org/sdr/USAASB01194.md): Battery · inoperative · Jul 7, 2001 · N274AU · Boeing 7372B7 · Emergency Lighting > BWI - THE LEFT EXTERIOR OVERWING EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. (M) - [SDR USAA010865](https://openairdocs.org/sdr/USAA010865.md): Skin · cracked · Jul 7, 2001 · N269AU · Boeing 7372B7 · Fuselage Structure (General) > CLT - FOUND FUSELAGE SKIN CRACKED, AFT END OF AIRSTAIR HANDLE CUTOUT. INSTALLED REPAIR DOUBLER PER TYPICAL REPAIR 53-30-03. (M) - [SDR P2EA01127](https://openairdocs.org/sdr/P2EA01127.md): Skin · damaged · Jul 6, 2001 · N128NJ · Boeing 7372B7 · Leading Edge Devices > SJO - DURING C-CHECK, FOUND LEFT WING, OUTBOARD FORE FLAP (P/N 65-46431-251, S/N BN424) UPPER SURFACE WITH BUDGED SKIN, DELAMINATION AND DENTS. LEFT WING, OUTBOARD FORE FLAP (P/N 65-46431-251, S/N BN424), NEW PART INSTALLED (P/N 65-46431-243, S/N BN188). (M - [SDR P2EA01116](https://openairdocs.org/sdr/P2EA01116.md): Skin · delaminated · Jul 6, 2001 · N128NJ · Boeing 7372B7 · Leading Edge Devices > SJO - DURING C-CHECK, LEFT WING, OUTBOARD FORE FLAP (P/N 65-46431-251, S/N BN424) UPPER SURFACE WITH BULGED SKIN, DELAMINATION AND DENTS. (M) - [SDR P2EA01123](https://openairdocs.org/sdr/P2EA01123.md): Spoiler · delaminated · Jul 5, 2001 · N128NJ · Boeing 7372B7 · Spoilers > SJO - DURING C-CHECK, FOUND RIGHT WING SPOILER NR 6 (P/N 65-46451-61A, S/N MA6427) DELAMINATED. RIGHT WING SPOILER NR 6 REPAIRED DUE TO DELAMINATION. (M) - [SDR P2EA01115](https://openairdocs.org/sdr/P2EA01115.md): Spoiler · delaminated · Jul 5, 2001 · N128NJ · Boeing 7372B7 · Spoilers > SJO - DURING C-CHECK, RIGHT WING, SPOILER NR 6 (P/N 65-46451-61A, S/N MA6427) DELAMINATED. (M) - [SDR P2EA01117](https://openairdocs.org/sdr/P2EA01117.md): Skin · dented · Jul 3, 2001 · N128NJ · Boeing 7372B7 · Fuselage Main, Plate/Skin > SJO - DURING C-CHECK, FUSELAGE BS 1026 BETWEEN STRINGER 27 LEFT AND 27 RIGHT SKIN WITH DENT OUT OF LIMITS. FUSELAGE SKIN SECTION REPAIRED FROM BS 1016 TO BS 1033, BETWEEN STRINGERS 26 LEFT AND 26 RIGHT DUE TO DENT IAW SRM 53-30-3, FIG 28. (M) - [SDR P2EA01118](https://openairdocs.org/sdr/P2EA01118.md): Skin · dented · Jul 3, 2001 · N128NJ · Boeing 7372B7 · Fuselage Main, Plate/Skin > SJO - DURING C-CHECK, FUSELAGE FROM BS 847-867 BETWEEN STRINGER 26 LEFT AND 27 LEFT SKIN WITH DENTS OUT OF LIMITS. (M) - [SDR P2EA01114](https://openairdocs.org/sdr/P2EA01114.md): Skin · dented · Jul 3, 2001 · N128NJ · Boeing 7372B7 · Fuselage Main, Plate/Skin > SJO - DURING C-CHECK, FUSELAGE FROM BS 847 TO BS 867 BETWEEN STRINGER 26L AND 26R HAS SKIN WITH DENTS OUT OF LIMITS. (M) Next page: https://openairdocs.org/model/boeing-737-2b7/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 = '7372B7' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/model/boeing-737-2b7/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.