# Service difficulty reports: N7865A A list on [N7865A](https://openairdocs.org/aircraft/N7865A.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 4 · 199 reports - [SDR SWAA2025120140306](https://openairdocs.org/sdr/SWAA2025120140306.md): Coffeemaker · odor · Nov 26, 2025 · N7865A · Boeing 7377Q8 · Buffet/Galleys > UNKNOWN BURNING IN THE FWD GALLEY. PERFORMED INSPECTION IAW AMM 05-51-56 NO ISSUES FOUND BELIEVE COFFEE MAKER. TO BE BAD. ACFT OK FOR SERVICE. - [SDR SWAA2025082206127](https://openairdocs.org/sdr/SWAA2025082206127.md): Skin · corroded · Aug 20, 2025 · N7865A · Boeing 7377Q8 · Trailing Edge Flaps > LH INBOARD AFT FLAP HAS INTERGRANULAR CORROSION AT TRAILING EDGE APPROX. MID WAY DAMAGE IS LOCATED AT TRAILING EDGE 30.5' FROM OUTBOARD EDGE. DAMAGE IS 3.875 ' X 1.625'<[01] REMOVED AND REPLACED LH IB AFT FLAP; OPS CHECK GOOD REF. AMM 27-51-12. - [SDR SWAA2025082106137](https://openairdocs.org/sdr/SWAA2025082106137.md): Stringer Splice · corroded · Aug 20, 2025 · N7865A · Boeing 7377Q8 · Fuselage Miscellaneous Structure > AFT CARGO LEFT CENTER CATSTRIP CORRODED. REMOVED AND REPLACED CAPSTRIP PER AMM 25-52-06. - [SDR SWAA2025062083318](https://openairdocs.org/sdr/SWAA2025062083318.md): Floor Panel · cracked · Jun 18, 2025 · N7865A · Boeing 7377Q8 · Cargo Compartments > AFT CARGO FLOOR PANEL IS CRACKED AFT CARGO FLOOR PANEL IS CRACKED2945286 <[01]. REPAIRED FLOOR PANEL IN AFT CARGO COMPARTMENT PER AMM 25-52-01. A/C OK TO CONTINUE. THIS CLEARS MEL. - [SDR SWAA2025021094476](https://openairdocs.org/sdr/SWAA2025021094476.md): Bracket · loose · Feb 8, 2025 · N7865A · Boeing 7377Q8 · Emergency Equipment > FORWARD SERVICE DOOR GIRT BAR BRACKET LOOSE<[01] OK TO CONTINUE PER TLD; EA M-23-125-01839 ATTACHED
FWD SVC DOOR GIRT BRACKET SECURED WITH SAFETY WIRE
REPAIR MUST BE DONE WITH IN 10 DAYS. - [SDR SWAA2024121777019](https://openairdocs.org/sdr/SWAA2024121777019.md): Girt Bar · out of position · Dec 13, 2024 · N7865A · Boeing 7377Q8 · Emergency Equipment > FA REPORTS AFT ENTRY DOOR GIRT BAR NOT PROPERLY STOWED.<[01] STOWED AFT ENTRY DOOR GIRT BAR PER AMM 25-66-01 - [SDR SWAA2024102451189](https://openairdocs.org/sdr/SWAA2024102451189.md): Retainer · out of alignment · Oct 21, 2024 · N7865A · Boeing 7377Q8 · Emergency Equipment > AFT SERVICE DOOR ESCAPE SLIDE GIRT BAR RETAINING RING DOES NOT LOCK ONTO THE GIRT BAR.<[01] REMOVED AND REPLACED AFT SERVICE DOOR ESCAPE GIRT BAR RETAINER RING. OPS CHECK GOOD REF AMM 25-66-01 - [SDR SWAA2024052287701](https://openairdocs.org/sdr/SWAA2024052287701.md): Slide · dislodged · May 19, 2024 · N7865A · Boeing 7377Q8 · Escape Slide > REF TTG8Q00TF4HQ LP 2662364 FOR ORIGINAL WRITE UP: AFT ENTRY EMERGENCY EXIT SLIDE FELL OUT OF HOLDER WHEN PROVO ATTEMPTED TO SHUT THE DOOR<[01] REINSTALLED AFT ENTRY ESCAPE SLIDE PACK REF AMM 25-66-01 AND MT 725-61-06. - [SDR SWAA2024052287697](https://openairdocs.org/sdr/SWAA2024052287697.md): Slide · dislodged · May 19, 2024 · N7865A · Boeing 7377Q8 · Escape Slide > AFT ENTRY EMERGENCY EXIT SLIDE FELL OUT OF HOLDER WHEN PROVO ATTEMPTED TO SHUT THE DOOR REF TTG8Q00TF5B3 FOR NON-ROUTINE REFERENCING MT 725-61-06-AE (REP - EMERGENCY ESCAPE SLIDE AFT ENTRY DOOR) TTG8Q00TF4LK<[01] REINSTALLED AFT ENTRY ESCAPE SLIDE PACK. REF AM - [SDR SWAA2024022655965](https://openairdocs.org/sdr/SWAA2024022655965.md): Actuator · out of adjust · Feb 24, 2024 · N7865A · Boeing 7377Q8 · Passenger Compartment Equipment > SEAT 11D RECLINES INTO EXIT ROW<[01] ADJUSTED SEAT 11D RECLINE ACTUATOR PER AMM 25-22-00 OPS CHECKS GOOD - [SDR SWAA2024010837836](https://openairdocs.org/sdr/SWAA2024010837836.md): Cover · missing · Jan 4, 2024 · N7865A · Boeing 7377Q8 · Emergency Lighting > F/A REPORTS R/H O/W EXIT EMERGENCY EXIT LIGHT COVER MISSING<[01] REPLACED MISSING LENS PER AMM 33-51-03 - [SDR SWAA2023120825686](https://openairdocs.org/sdr/SWAA2023120825686.md): Light · inoperative · Nov 29, 2023 · N7865A · Boeing 7377Q8 · Emergency Lighting > EMERGENCY EXIT AISLE LIGHT AT SEAT ROW 16FED IS INOP.<[01] RELLAMPED EMERGENCY EXIT AISLE LIGHT AT SEAT ROW 16FED AND PERFORMED GOOD TEST IAW AMM 33-51-03-960-801.;[02] CERTIFIED ACTION 1.;[03] VERIFIED CORRECTIVE ACTIONS STEP 1 AND MEASUREMENTS TABLE. - [SDR SWAA2023121125682](https://openairdocs.org/sdr/SWAA2023121125682.md): Light · inoperative · Nov 22, 2023 · N7865A · Boeing 7377Q8 · Emergency Lighting > WIRE W3142-0456-20 FOUND DEPINNED FROM GD3664 (MARKED) WIRE LOCATED AT STA767<[01] REPINNED WIRE W3142-0456-20 TO GD3664 PER SWPM 20-90-15. PERFORMED GOOD GROUND CHECK OF WIRE W3142-0456-20 AT CONNECTOR D11338 IAW WDM 33-51-14 AND PERFORMED GOOD EMERGENCY LIGH - [SDR SWAA2023121123814](https://openairdocs.org/sdr/SWAA2023121123814.md): Bracket · cracked · Nov 22, 2023 · N7865A · Boeing 7377Q8 · Fuselage Main, Attach Fittings > BRACKET CRACKED AT BS 867 STR 3R<[01] REMOVED FLOOR PANEL 321UF PER AMM 53-21-00-000-801;[02] EDIT: ACTION ENTERED IN ERROR; WRONG TASK;[03] COMPLETED STEP 1. CARD COMPLETED;[04] VERIFIED COMPLETE STEP 3; MEASUREMENTS TABLE OK; CARD COMPLETE. - [SDR SWAA2023121121942](https://openairdocs.org/sdr/SWAA2023121121942.md): Skin · cracked · Nov 15, 2023 · N7865A · Boeing 7377Q8 · Fuselage Main, Plate/Skin > CRACK ON FUSELAGE SKIN BS907+10' JUST ABOVE STR22L COMMON TO WASTE TANK EXHAUST PORT CUTOUT<[01] THIS IS A CATEGORY B REPAIR AS PER SRM 53-70-01-2R-3.;[02] TASK COMPLETE.;[03] CORRECTION TO CORRECTIVE ACTION STEP 2 SHOULD STATE ' CRACK WAS FOUND TO BE OUT OF L - [SDR SWAA2023121121949](https://openairdocs.org/sdr/SWAA2023121121949.md): Slat · cracked · Nov 15, 2023 · N7865A · Boeing 7377Q8 · Leading Edge Devices > LEFT WING; LOWER SURFACE; L/E SLAT NOSE SKIN AT ACTUATOR RIB IS CRACKED AT FASTENER (MARKED) SLAT #3<[01] UPDATED PARTS;[02] TORQUED LEADING EDGE SLAT ACTUATOR ATTACHMENT PER AMM 27-81-21-400-801 3.H.(8).
ATS TORQUE WRENCH
CAL ID: ATS2099
CAL DUE: 09 - [SDR SWAA2023121121945](https://openairdocs.org/sdr/SWAA2023121121945.md): Support Beam · corroded · Nov 15, 2023 · N7865A · Boeing 7377Q8 · Wing Main, Frame Structure > LEFT WING TRAILING EDGE SUPPORT BEAM IS CORRODED AT FASTENERS; I/B #1 FLAP CARRIAGE; O/B #2 FLAP CARRIAGE<[01] VERIFIED MEASUREMENTS TABLE.;[02] REMOVED; REPLACED; AND INSTALLED A NEW TRAILING EDGE SUPPORT BEAM ASSEMBLY PANEL ON L/W; T/E; I/B #1 FLAP CARRIAGE; - [SDR SWAA2023121121944](https://openairdocs.org/sdr/SWAA2023121121944.md): Support Beam · corroded · Nov 15, 2023 · N7865A · Boeing 7377Q8 · Wing Main, Frame Structure > LEFT WING TRAILING EDGE SUPPORT BEAM IS CORRODED AT FASTENERS AFT OF #1 SLAT ACTUATOR; O/B #1 FLAP CARRIAGE<[01] REMOVED AND REPLACED TRAILING EDGE SUPPORT BEAM @ #1 SLAT ACTUATOR; O/B OF #1 FLAP CARRIAGE IAW SRM 51-40-02 AND AIPC 57-50-00-21.;[02] VERIFIED CO - [SDR SWAA2023121121948](https://openairdocs.org/sdr/SWAA2023121121948.md): Support Beam · corroded · Nov 15, 2023 · N7865A · Boeing 7377Q8 · Wing Main, Frame Structure > RIGHT WING TRAILING EDGE SUPPORT BEAM IS CORRODED AT FASTENER HOLES;I/B #7 FLAP CARRIAGE; O/B DEFLECTION RIB<[01] REMOVED AND REPLACED I/B #7 FLAP CARRIAGE; O/B DEFLECTION RIB TRAILING EDGE SUPPORT BEAM IAW SRM 51-40-02 AND AIPC 57-50-00-18.;[02] AMT CORRECTIO - [SDR SWAA2023121121941](https://openairdocs.org/sdr/SWAA2023121121941.md): Support Beam · corroded · Nov 15, 2023 · N7865A · Boeing 7377Q8 · Wing Main, Frame Structure > RIGHT WING TRAILING EDGE SUPPORT BEAM IS CORRODED AT FASTENER HOLES; O/B #7 FLAP CARRIAGE; I/B #8 FLAP CARRIAGE<[01] UPON FURTHER INVESTIGATION; THERE'S NO ALLOWABLE DAMAGE ON SUPPORT BEAM AND PART WILL BE A REPLACEMENT IAW SRM 51-10-02 STEP 9. REMOVED; RECEIV - [SDR SWAA2023121121410](https://openairdocs.org/sdr/SWAA2023121121410.md): Stringer · cracked · Nov 14, 2023 · N7865A · Boeing 7377Q8 · Fuselage Main, Longeron/Stringer > AREA AFT OF FWD CARGO COMPARTMENT HAS A CRACKED STR AT STR 27R; BS 520+19<[01] VERIFIED MEASUREMENT TABLE - [SDR SWAA2023121121411](https://openairdocs.org/sdr/SWAA2023121121411.md): Stringer · cracked · Nov 14, 2023 · N7865A · Boeing 7377Q8 · Fuselage Main, Longeron/Stringer > AREA AFT OF FWD CARGO COMPARTMENT HAS A SUSPECTED CRACKED STR AT STR 25R; BS 520+19<[01] VERIFIED MEASUREMENT TABLE;[02] CRACKED STRINGER WAS FOUND TO BE OUT LIMITS; REPAIRED AS PER EA 23-153-03370. THIS IS A CATEGORY A REPAIR AS DEFINED IN 737-700 SRM 51-00-0 - [SDR SWAA2023121121407](https://openairdocs.org/sdr/SWAA2023121121407.md): Stringer · cracked · Nov 14, 2023 · N7865A · Boeing 7377Q8 · Fuselage Main, Longeron/Stringer > AREA AFT OF FWD CARGO COMPARTMENT HAS A CRACKED STR AT STR 27L; BS 520+19<[01] VERIFIED MEASUREMENT FIELD - [SDR SWAA2023120821158](https://openairdocs.org/sdr/SWAA2023120821158.md): Threshold · cracked · Nov 14, 2023 · N7865A · Boeing 7377Q8 · Fuselage Miscellaneous Structure > AFT CARGO BAY AFT CORNER THRESHOLD IS CRACKED<[01] CRACK FOUND TO BE OUT OF LIMITS AS PER SRM 53-60-15-1A-1.;[02] AFT CARGO BAY AFT CORNER SCUFF PLATE REPAIRED PER SRM 53-60-15-2R-1.;[03] VERIFIED.
VERIFIED MEASUREMENTS. - [SDR SWAA2023121121029](https://openairdocs.org/sdr/SWAA2023121121029.md): Seat Track · corroded · Nov 13, 2023 · N7865A · Boeing 7377Q8 · Fuselage, Seat/Cargo Attach Fittings > CABIN SEAT TRACK HAS CORROSION IN WELL OF CROWN AT BS 847+12; RBL 25; WL 208<[01] UPDATED STEPS 1 AND 2;[02] UPDATED MEASURMENTS TABLE
USED DIAL DEPTH GAGE TOOLING ID: ATS2472
DUE DATE: 12/31/23;[03] VERIFIED;[04] EDITED MEASUREMENTS TABLE;[05] VERIFIED; - [SDR SWAA2023120821137](https://openairdocs.org/sdr/SWAA2023120821137.md): Lens · out of adjust · Nov 13, 2023 · N7865A · Boeing 7377Q8 · Emergency Lighting > PASSENGER CABIN OVERHEAD R/H BIN #6 EMERGENCY LIGHT LENS IS DIS-BONDED. (MARKED)<[01] REMOVED AND REINSTALLED EMERGENCY LIGHT LENS ON PASSENGER OVERHEAD BIN R/H #6 IAW AMM 33-51-03-960-801 STEP 3. (A) AND (C).;[02] VERIFIED CORRECTIVE ACTION AND MEASUREMENT FI - [SDR SWAA2023101711038](https://openairdocs.org/sdr/SWAA2023101711038.md): Seat · out of adjust · Oct 15, 2023 · N7865A · Boeing 7377Q8 · Passenger Compartment Equipment > EMERGENCY EXIT SEAT 11 D RECLINES<[01] ADJUSTED EMERGENCY EXIT SEAT 11D; REF AMM 25-22-00; OPS CK GOOD.
ACCOMPLISHED BY 141645 ON LOGPAGE 2504709 - [SDR SWAA2023052451334](https://openairdocs.org/sdr/SWAA2023052451334.md): Girt Bar · bent · May 23, 2023 · N7865A · Boeing 7377Q8 · Escape Slide > FWD ENTRY DOOR SLIDE BRACKET BENT WHERE GIRT BAR STORES<[01] REPOSITIONED GIRT BAR PER SIP OPS CHECK GOOD. AC OK FOR SERVICE. - [SDR SWAA2022120678863](https://openairdocs.org/sdr/SWAA2022120678863.md): Battery · inoperative · Dec 5, 2022 · N7865A · Boeing 7377Q8 · Emergency Equipment > FWD MEGAPHONE INOP / [01] REPLACED BATTERIES; OPS CHECK NORMAL; WORK DONE PER 25-64-00 OF THE AMM - [SDR SWAA2022070123839](https://openairdocs.org/sdr/SWAA2022070123839.md): Slide · out of position · Jun 28, 2022 · N7865A · Boeing 7377Q8 · Escape Slide > L1 SLIDE PACK IS PARTIALLY DROP OUT OF COMPARTMENT / [01] REINSTALLED L1 DOOR SLIDE IAW AMM 25-66-01. A/C OK FOR SERVICE - [SDR SWAA2022051808034](https://openairdocs.org/sdr/SWAA2022051808034.md): Flashlight Assy · loose · May 14, 2022 · N7865A · Boeing 7377Q8 · Passenger Compartment Equipment > FWD EMER FLASHLIGHT BASE LOOSE / [01] RESECURED BOTH FWD EMERGENCY FLASHLIGHT BASES PER SIP. - [SDR SWAA2022012461726](https://openairdocs.org/sdr/SWAA2022012461726.md): Light · inoperative · Jan 14, 2022 · N7865A · Boeing 7377Q8 · Emergency Lighting > BULLNOSE EMERGENCY EXIT LIGHT AT 6FED IS INOP; RELAMPED BULLNOSE EMERGENCY EXIT LIGHT AT 6FED AND LIGHT IS STILL INOP. ALL WORK PERFORMED AS PER AMM. 33-51-03-960-801 STEP 2.D.1. REPLACED M1674 EMERGENCY EXIT LIGHT BATTERY PACK AND PERFORMED GOOD INSTALLATIO - [SDR SWAA2022012461725](https://openairdocs.org/sdr/SWAA2022012461725.md): Light · inoperative · Jan 14, 2022 · N7865A · Boeing 7377Q8 · Emergency Lighting > FWD SERVICE DOOR EMERGENCY EXIT LIGHT INOP; / [01] RELAMPED FWD SERVICE DOOR EMERGENCY EXIT SLIDE LIGHT AND LIGHT IS STILL INOP. ALL WORK PERFORMED AS PER AMM. 33-51-04-960-801 STEP 2.F.1(A;B;D); [02] CERTIFY WORK WAS PERFORMED PER AMM 33-51-04-960-801 STEP 2 - [SDR SWAA2022012461512](https://openairdocs.org/sdr/SWAA2022012461512.md): Scuff Plate · cracked · Jan 14, 2022 · N7865A · Boeing 7377Q8 · Fuselage Miscellaneous Structure > F.E.D. AFT INNER SCUFF PLATE IS CRACKED; / [01] UPDATED PART; [02] INSTALLED AND SEALED ROBBED SCUFF PLATE AT FED AFT INNER POSITION PER AMM 53-11-01-420-801; [03] CORRECTION TO CORRECTIVE ACTION 2: REMOVED AND REPLACED SCUFF PLATE AT FED AFT INNER POSITION - [SDR SWAA2022012457091](https://openairdocs.org/sdr/SWAA2022012457091.md): Bracket · cracked · Dec 30, 2021 · N7865A · Boeing 7377Q8 · Fuselage Miscellaneous Structure > WIRE SUPPORT BRACKET CRACKED AT B.S 897 STRINGER 3 R/H; / [01] ENTRY TO CORRECT B.S DISCREPANCY IS AT B.S 867 STRINGER 3R/H; [02] REMOVED DAMAGED WIRE SUPPORT BRACKET AT B.S 867 STRINGER 3 R/H IAW B737 SRM 51-40-02. LOCATED AND DRILLED NEW WIRE SUPPORT BRACK - [SDR SWAA2022012456256](https://openairdocs.org/sdr/SWAA2022012456256.md): Fairing · delaminated · Dec 26, 2021 · N7865A · Boeing 7377Q8 · Aerodynamic Fairings > SUPPLEMENTAL INFORMATION: FAIRING 195CL HAS DELAMINATIONS OVER CORE AREA NEXT TO EDGEBAND OF PANEL SEE FAULT TTG8Q009PY4M.; / [01] IDENTIFIED PANEL MATERIAL IAW SRM 53-40-70-0I-1 FIG 2 TABLE 2 ITEM 5.
FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53- - [SDR SWAA2022012454693](https://openairdocs.org/sdr/SWAA2022012454693.md): Support Angle · corroded · Dec 18, 2021 · N7865A · Boeing 7377Q8 · Fuselage Miscellaneous Structure > CORROSION; AFT CARGO SIDEWALL LWR SUPPORT CLIP; BS 906 RBL 24; / [01] REMOVED CORROSION ON AFT CARGO SIDEWALL LOWER SUPPORT CLIP; BS 906; RBL 24; WORK AREA; W 1.0' X L 1.0'; D 0.002'; ORIGINAL THICKNESS 0.063'; REMAINING MATERIAL 0.061; FOUND TO BE IN LIMITS - [SDR SWAA2022012454177](https://openairdocs.org/sdr/SWAA2022012454177.md): Attach Bracket · cracked · Dec 16, 2021 · N7865A · Boeing 7377Q8 · Wing Miscellaneous Structure > PNEUMATIC DUCT TIE ROD SUPPORT ATTACH POINT BRACKET AT BS 540 LBL 58 IS CRACKED; / [01] REMOVAL OF PNEUMATIC DUCT TIE ROD SUPPORT ATTACH BRACKET AT B.S. 540 LBL 58 ACCOMPLISHED ON CUSTOMER CARD NUMBER TTG8Q009Y54G; [02] RECIEVED NEW PNEUMATIC DUCT TIE ROD SUP - [SDR SWAA2022012453277](https://openairdocs.org/sdr/SWAA2022012453277.md): Baffle · cracked · Dec 15, 2021 · N7865A · Boeing 7377Q8 · Fuselage Miscellaneous Structure > FWD CARGO BAY BAFFLE CRACKED BS 400-420 RBL 25 WL 165; / [01] APPLICABILITY STATEMENT NO DAMAGE ALLOWED ON SRM FOUND; REPLACE PART FOR REPAIR IAW SRM 51-10-02; [02] REMOVED BAFFLE AT FCB BS.400 TO BS.420 RBL.25 WL.165 IAW SRM 51-40-02; [03] VERIFIED CORRECTIV - [SDR SWAA2022012451345](https://openairdocs.org/sdr/SWAA2022012451345.md): Bear Strap · cracked · Dec 8, 2021 · N7865A · Boeing 7377Q8 · Fuselage Main, Plate/Skin > FOUND 1.5' CRACK AT FWD SERVICE DOOR SURROUND; BS 294 3.5' UNDER S-8R AROUND FASTENER COMMON TO THE BEAR STRAP. AREA MARKED; / VERIFIED SRM 53-10-01-2R-6 IS APPLICABLE FOR SKIN AND BEARSTRAP REPAIR AT THE FWD GALLEY DOOR..FABRICATED REPAIR PARTS DOUBLER -1 FR - [SDR SWAA2022012451326](https://openairdocs.org/sdr/SWAA2022012451326.md): Fairing · cracked · Dec 8, 2021 · N7865A · Boeing 7377Q8 · Aerodynamic Fairings > FAIRING 195CL IS CRACKED IN RADIUS AT AFT EDGE.; / REMOVED DAMAGE FROM AFT RADIUS; AFT EDGEBAND; AND UPPER EDGEBAND; ALL ON INNER SURFACE; ALL DAMAGES CONNECT; VALIDATED REPAIR PER SRM 51-70-05-2R-6; FABRICATED REPAIR PLIES OUT OF BMS 8-79 ST 120 LOT#1476632- - [SDR SWAA2022012451324](https://openairdocs.org/sdr/SWAA2022012451324.md): Channel · cracked · Dec 7, 2021 · N7865A · Boeing 7377Q8 · Fuselage Miscellaneous Structure > SUPPLEMENTAL INFORMATION: CRACK ON PASSENGER CABIN FWD ENTRY DOOR MOP SILL AT LBL 56 BS 294+9 WL 208.; / [01] REMOVED FWD ENTRY DOOR MOP SILL B.S 270-360 LBL56 WL208 PER SRM 51-40-02-0G.; [02] REMOVED INTERCOSTALS MOP SILL SUPPORT AT B.S 312-328 & B.S 328-344 - [SDR SWAA2022012451317](https://openairdocs.org/sdr/SWAA2022012451317.md): Intercostal · cracked · Dec 7, 2021 · N7865A · Boeing 7378Q8 · Fuselage Miscellaneous Structure > SUPPLEMENTAL INFORMATION: CRACK ON PASSENGER CABIN INTERCOSTAL AT LBL 46 BS 328+7 WL 208.; / [01] REMOVED AND LOCATED HOLES IN NEW INTERCOSTAL; AN INSTALLED AT BS 328+7 LBL 46 WL 208 PER SRM 51-40-02-0G-0;SRM 51-40-05-0G-0;DRAWING # 141A5400 SHT 44 REV -; [02 - [SDR SWAA2022012451316](https://openairdocs.org/sdr/SWAA2022012451316.md): Intercostal · cracked · Dec 7, 2021 · N7865A · Boeing 7377Q8 · Fuselage Miscellaneous Structure > CRACK ON PASSENGER CABIN INTERCOSTAL AT LBL 46 BS 312+8 WL 208.; / [01] COMPLETED STEPS 1 AND 2
REQUEST OK TO INSTALL; [02] CORRECTED REPAIR LOCATION AND MEASUREMENTS; [03] CORRECTED REPAIR LOCATION AND MEASUREMENTS; [04] CERTIFY; [05] VERIFIED STEPS 1 AND - [SDR SWAA2022012451066](https://openairdocs.org/sdr/SWAA2022012451066.md): Support · corroded · Dec 7, 2021 · N7865A · Boeing 7377Q8 · Fuselage Miscellaneous Structure > CORROSION ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS767 - BS727D+13 RBL20. MARKED.; / [01] REMOVED CORROSION FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS 727D+13 BS 767 RBL 20 DIMENSION;L=2.' W=1. DEPTH=.012 ORIGINAL THICKNESS.040 REMAINING THICKNESS - [SDR SWAA2022012451064](https://openairdocs.org/sdr/SWAA2022012451064.md): Stringer · cracked · Dec 7, 2021 · N7865A · Boeing 7377Q8 · Fuselage Main, Longeron/Stringer > CRACK ON FWD CARGO BAY BS 540 R/H STRINGER 23.; / [01] EVALUATED CRACK MEASUREMENTS ON FCB BS 540; STR 23RH; STRINGER DAMAGE FOUND TO BE OUT LIMITS IAW SRM 53-00-03-1A FIG 103.; [02] OUT OF SEQUENCE- VALIDATED ALLOWABLE DAMAGE 1 APPLICABILITY OF SRM SRM 53-0 - [SDR SWAA2022012451312](https://openairdocs.org/sdr/SWAA2022012451312.md): Shear Web · corroded · Dec 7, 2021 · N7865A · Boeing 7377Q8 · Fuselage Miscellaneous Structure > SUPPLEMENTAL INFORMATION: CORROSION ON PASSENGER CABIN SHEAR WEB AT BS 1016 LBL 13 WL 208.1.; / [01] REMOVED CORROSION ON PASSENGER CABIN SHEAR WEB AT BS 1016 LBL13 WL 208.1 IAW SRM 51-10-02-0G-0 STEP 4 D(2)MEASURES.8'X.5'X.008' FOUND OUT LIMITS;NO ALLOWABLE - [SDR SWAA2022012451067](https://openairdocs.org/sdr/SWAA2022012451067.md): Cargo Track · cracked · Dec 7, 2021 · N7865A · Boeing 7377Q8 · Fuselage, Seat/Cargo Attach Fittings > CRACKED TRACK AT AFT CARGO BAY BS767; BS727E RBL13 WL156. MARKED.; / EVALUATED CRACKED TRACK AT AFT CARGO BAY BS767; BS727E RBL13 WL156. DIMENSIONS L: 0.370' AND THE CRACK EXCEEDS THE DIMENSIONS IAW SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2 FIGURE 103 TOOL USED CA - [SDR SWAA2022012451065](https://openairdocs.org/sdr/SWAA2022012451065.md): Stringer · cracked · Dec 7, 2021 · N7865A · Boeing 7377Q8 · Fuselage Main, Longeron/Stringer > CRACK ON FWD CARGO BAY BS 540 R/H STRINGER 26.; / STRINGER DAMAGE FOUND TO BE OUT LIMITS IAW SRM 53-00-03-1A FIG 103.; [02] VERIFIED APPLICABILITY FOR REPAIR BETWEEN BS 500D - 540; STR- 26R IAW SRM 53-00-03-2R-1; [03] VERIFIED APPLICABILITY OF SRM 53-00-03-2R - [SDR SWAA2022012451062](https://openairdocs.org/sdr/SWAA2022012451062.md): Stringer · cracked · Dec 7, 2021 · N7865A · Boeing 7377Q8 · Fuselage Main, Longeron/Stringer > CRACK ON FWD CARGO BAY BS 540 R/H STRINGER 21.; / STRINGER DAMAGE FOUND TO BE OUT LIMITS IAW SRM 53-00-03-1A FIG 103.; [02] VERIFIED APPLICABILITY FOR REPAIR BETWEEN BS 500D - 540; STR- 21R IAW SRM 53-00-03-2R-1; [03] VERIFIED APPLICABILITY OF SRM 53-00-03-2R Next page: https://openairdocs.org/aircraft/N7865A/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 n_number = 'N7865A' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N7865A/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.