# Service difficulty reports: N7876A

A list on [N7876A](https://openairdocs.org/aircraft/N7876A.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 5 · 248 reports

- [SDR SWAA2026092150178](https://openairdocs.org/sdr/SWAA2026092150178.md): Ring · broken · Sep 15, 2026 · N7876A · Boeing 7377Q8 · Emergency Equipment
  > AFT ENTRY DOOR GIRT BAR RING BROKEN. REPLACED THE STOP RING IAW AMM 25-66-01.
- [SDR SWAA2026072720484](https://openairdocs.org/sdr/SWAA2026072720484.md): Lamp · inoperative · Jul 23, 2026 · N7876A · Boeing 7377Q8 · Emergency Lighting
  > AFT ATTENDANT STATION PANEL'S WORK LIGHT BUTTON AND EMERGENCY LIGHT BUTTON BACK LIGHTS ARE INOPERATIVE. REPLACED THE LAMPS AFT ATTENDANT STATION PANEL'S WORK LIGHT BUTTON AND EMERGENCY LIGHT BUTTON BACK LIGHTS. IAW CMM 31-15-15.
- [SDR SWAA2026071773120](https://openairdocs.org/sdr/SWAA2026071773120.md): Slide · loose · Jul 13, 2026 · N7876A · Boeing 7377Q8 · Escape Slide
  > FORWARD ENTRY DOOR SLIDE PACK LOOSE. DOOR OPENED BEFORE GIRT BAR PULLED. INSTALLED FWD ENTRY DOOR SLIDE PACK IAW MT 725--61-06. ACFT OK FOR SERVICE.
- [SDR SWAA2026062413321](https://openairdocs.org/sdr/SWAA2026062413321.md): Strap · out of alignment · Jun 4, 2026 · N7876A · Boeing 7377Q8 · Fuselage Main, Structure
  > BS 328 FRAME STRAP FROM STR 22R TO STR 20R DOES NOT MATCH WITH CONFIGURATION TASK 5311-1-17336-NG FIGURE 15 IAW EA 26-153-01522; THE CONFIGURATION IS ACCEPTABLE IAW EA 26-153-01522; THE CONFIGURATION IS ACCEPTABLE.
- [SDR SWAA2026062409347](https://openairdocs.org/sdr/SWAA2026062409347.md): Stub Frame · cracked · Jun 4, 2026 · N7876A · Boeing 7377Q8 · Fuselage Main, Structure
  > CRACK INDICATION FOUND IN OPEN FASTENER HOLE AFT POSITION AT STUB BEAM STRAPS AREA AT BS 639 RBL 45.57. CRACK DIRECTION 3 O`CLOCK LOOKING FWD FROM INBD FACE REPLACED STUB BEAM STRAPS LOCATED BS 639 RBL 45.57 IAW SRM 51-10-02 PARAGRAPH 9, SRM 51-40-02, DWG 144
- [SDR SWAA2026062409348](https://openairdocs.org/sdr/SWAA2026062409348.md): Seal · cracked · Jun 4, 2026 · N7876A · Boeing 7377Q8 · Horizontal Stabilizer Miscellaneous Structure
  > CRACKED BLADE ACCESS PANEL 343AT SEAL RT HORIZONTAL STAB. REPLACED ACCESS PANEL 343AT SEAL AND FASTENER AT RT HORIZONTAL STAB IAW SRM 51-40-02. AND SRM 51-10-02 ITEM 9.
- [SDR SWAA2026062409094](https://openairdocs.org/sdr/SWAA2026062409094.md): Plate · cracked · Jun 3, 2026 · N7876A · Boeing 7377Q8 · Wing Main, Frame Structure
  > CRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS241 AT LT WING. REPLACED FASTENERS AND CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 241 AT LT WING IAW SRM 51-40-02 AND DWG 115A2713 SHEET 3, REV A.
- [SDR SWAA2026062409092](https://openairdocs.org/sdr/SWAA2026062409092.md): Plate · cracked · Jun 3, 2026 · N7876A · Boeing 7377Q8 · Wing Main, Frame Structure
  > CRACKED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS272 AT RT WING. REPLACED CORRUGATED PLATE AND FASTENERS ON TRAILING EDGE LOCATED ORSS 272 AT RT WING IAW SRM 51-40-02.
- [SDR SWAA2026062409093](https://openairdocs.org/sdr/SWAA2026062409093.md): Plate · cracked · Jun 3, 2026 · N7876A · Boeing 7377Q8 · Wing Main, Frame Structure
  > CRACKED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS241 AT RT WING. REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS241 AT RT WING IAW SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: 115A2001; SHEET: 1; REV B.
- [SDR SWAA2026062408976](https://openairdocs.org/sdr/SWAA2026062408976.md): Fitting · damaged · Jun 3, 2026 · N7876A · Boeing 7377Q8 · Wing Main, Frame Structure
  > ELONGATED HOLE ON FITTING TRAILING EDGE LOCATED ORSS256 AT LT WING. REPLACED FITTING LOCATED ON TRAILING EDGE ORSS 256 AT LT WING IAW SRM 51-40-02-0G-0, SRM 51-10-02 ITEM 9, DWG 115A5300 SHEET 17, REV-.
- [SDR SWAA2026062409091](https://openairdocs.org/sdr/SWAA2026062409091.md): Plate · cracked · Jun 3, 2026 · N7876A · Boeing 7377Q8 · Wing Main, Frame Structure
  > CRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS272 AT LT WING. REPLACED CORRUGATED PLATE ON TRAILING EDGE LOCATED ORSS272 AT LT WING IAW SRM 51-40-02 AND DWG 115A2714; SHEET 6; REV: -. DUE TO NOT FOUND ALLOWABLE DAMAGE ON SRM 57-51-02-1A-1 ALLOWABLE DAMAGE 1
- [SDR SWAA2026062408975](https://openairdocs.org/sdr/SWAA2026062408975.md): Access Panel · damaged · Jun 3, 2026 · N7876A · Boeing 7377Q8 · Wing, Plate/Skin
  > ELONGATED HOLES ON ACCESS PANEL 561CB TRAILING EDGE AT LT WING. REPAIRED ACCESS PANEL 561CB TRAILING EDGE AT LT WING IAW SRM 51-70-04-2R-9, REPAIR 9.
- [SDR SWAA2026062408977](https://openairdocs.org/sdr/SWAA2026062408977.md): Access Panel · damaged · Jun 3, 2026 · N7876A · Boeing 7377Q8 · Wing, Plate/Skin
  > ELONGATED HOLES ON FITTING ACCESS PANEL 651GB AT RT WING. REPLACED FITTING ACCESS PANEL 651GB AT RT WING IAW SRM 51-40-02, SRM 51-10-02 ITEM 9, AND DWG 115A2714 SHEET 6 REV -.
- [SDR SWAA2026062408974](https://openairdocs.org/sdr/SWAA2026062408974.md): Access Panel · damaged · Jun 3, 2026 · N7876A · Boeing 7377Q8 · Wing, Plate/Skin
  > ELONGATED HOLES ACCESS PANEL 561BB AT LT WING. REPAIRED ACCESS PANEL 561BB AT LT WING IAW SRM 51-70-04-2R-9 REPAIR 9.
- [SDR SWAA2026062408451](https://openairdocs.org/sdr/SWAA2026062408451.md): Crossbeam · cracked · Jun 2, 2026 · N7876A · Boeing 7377Q8 · Fuselage Main, Structure
  > CRACKED BRAKE PANEL FLOOR STRUCTURE LOCATED BETWEEN BS 540 AND BL 0 TO RBL 24.75. REPLACED BRAKE PANEL AND FASTENERS ON BS 540 BETWEEN BL 0 TO RBL 24.75 IAW SRM 51-40-02 AND DRAWING 143A5240, SHEET 32, REV-.
- [SDR SWAA2026062408450](https://openairdocs.org/sdr/SWAA2026062408450.md): Angle · cracked · Jun 2, 2026 · N7876A · Boeing 7377Q8 · Fuselage Miscellaneous Structure
  > CRACKED ANGLE FLOOR STRUCTURE LOCATED BS 695 AND RBL 24.75. REPLACED ANGLE FLOOR STRUCTURE LOCATED BS 695 AND RBL 24.75 PASSENGER CABIN IAW SRM 51-40-02; DWG 111A6000, SHEET 208, REV - AND DWG 273A9110, SHEET 6, REV A.
- [SDR SWAA2026062408446](https://openairdocs.org/sdr/SWAA2026062408446.md): Bracket · cracked · Jun 1, 2026 · N7876A · Boeing 7377Q8 · Wing Miscellaneous Structure
  > CRACKED DEFLECTION CONTROL RIB TRAILING EDGE BRACKET LOCATED ORSS 272 LT WING. REPLACED DEFLECTION CONTROL RIB TRAILING EDGE BRACKET LOCATED ORSS 272 LT WING IAW SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 115A2930 SHEET 7 REV.
- [SDR SWAA2026062407749](https://openairdocs.org/sdr/SWAA2026062407749.md): Light · deteriorated · May 29, 2026 · N7876A · Boeing 7377Q8 · Emergency Lighting
  > DETERIORATED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING STRIP IN THE PASSENGER CABIN. REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING STRIP IAW AMM 33-51-15-960-801, AND DWG 33500007, REV 2.
- [SDR SWAA2025120442421](https://openairdocs.org/sdr/SWAA2025120442421.md): Stop · damaged · Dec 4, 2025 · N7876A · Boeing 7377Q8 · Emergency Equipment
  > AFT SERVICE ESCAPE SLIDE GIRT BAR RELEASE STOP DAMAGED. REPLACED AFT SERVICE ESCAPE SLIDE GIRT BAR RELEASE STOP IAW AMM 25-66-01.
- [SDR SWAA2025081805326](https://openairdocs.org/sdr/SWAA2025081805326.md): Lens · missing · Aug 16, 2025 · N7876A · Boeing 7377Q8 · Emergency Lighting
  > EMERGENCY EXIT SIGN LIGHT COVER MISSING AT ROW 11 ON CAPT SIDE. REINSTALLED EMERGENCY LIGHT LENS AT SEAT 11 ABC IAW AMM 33-51-03.
- [SDR SWAA2025060276260](https://openairdocs.org/sdr/SWAA2025060276260.md): Plug · damaged · May 29, 2025 · N7876A · Boeing 7377Q8 · Emergency Lighting
  > R1 DOOR EXIT SIGN CONNECTOR DAMAGED <[01]. R/R`D R1 DOOR EXIT SIGN D2968 PLUG IAW SWPM 20-61-28. REF WDM 33-51-12. OPS CHECKS NORMAL.
- [SDR SWAA2025032006547](https://openairdocs.org/sdr/SWAA2025032006547.md): Actuator · low pressure · Mar 18, 2025 · N7876A · Boeing 7377Q8 · Drag Control Actuator
  > AFTER FLAPS 5 HYD A SYSTEM LOW PRESSURE LIGHTS ON BOTH ENG AND ELECTRIC PUMP SHORTLY AFTER LOW PRESSURE LIGHTS ON HYD SYSTEM A CAME ON. SYS A QTY WENT TO 0. WE GOT EXTENDED VECTORS RAN QRH FOR LOSS OF SYSTEM A. RAN NON NORMAL LANDING DATA AND ALTERNATE EXTENDE
- [SDR SWAA2025032007746](https://openairdocs.org/sdr/SWAA2025032007746.md): Pump · low pressure · Mar 18, 2025 · N7876A · Boeing 7377Q8 · Hydraulic Pump, Auxiliary
  > AFTER FLAPS 5 HYD A SYSTEM LOOW PRESSURE LIGHTS ON BOTH ENG AND ELECTRIC PUMP SHORTLY AFTER LOW PRESSURE LIGHTS ON HYD SYSTEM A CAME ON. SYS A QTY WENT TO 0. WE GOT EXTENDED VECTORS RAN QRH FOR LOSS OF SYSTEM A. RAN NON NORMAL LANDING DATA AND ALTERNATE EXTEND
- [SDR SWAA2025032007747](https://openairdocs.org/sdr/SWAA2025032007747.md): Filter · low pressure · Mar 18, 2025 · N7876A · Boeing 7377Q8 · Hydraulic Filter, Auxiliary
  > AFTER FLAPS 5 HYD A SYSTEM LOW PRESSURE LIGHTS ON BOTH ENG AND ELECTRIC PUMP SHORTLY AFTER LOW PRESSURE LIGHTS ON HYD SYSTEM A CAME ON. SYS A QTY WENT TO 0. WE GOT EXTENDED VECTORS RAN QRH FOR LOSS OF SYSTEM A. RAN NON NORMAL LANDING DATA AND ALTERNATE EXTENDE
- [SDR SWAA2025032007748](https://openairdocs.org/sdr/SWAA2025032007748.md): Module · low pressure · Mar 18, 2025 · N7876A · Boeing 7377Q8 · Hydraulic Power Accumulator, Main
  > AFTER FLAPS 5 HYD A SYSTEM LOOW PRESSURE LIGHTS ON BOTH ENG AND ELECTRIC PUMP SHORTLY AFTER LOW PRESSURE LIGHTS ON HYD SYSTEM A CAME ON. SYS A QTY WENT TO 0. WE GOT EXTENDED VECTORS RAN QRH FOR LOSS OF SYSTEM A. RAN NON NORMAL LANDING DATA AND ALTERNATE EXTEND
- [SDR SWAA2025012087376](https://openairdocs.org/sdr/SWAA2025012087376.md): Sign · loose · Jan 17, 2025 · N7876A · Boeing 7377Q8 · Emergency Lighting
  > CREW REPORTS OVER WING EXIT SIGN LOOSE<[01] RESECURED EXIT SIGN AS PER SIP
- [SDR SWAA2024110555696](https://openairdocs.org/sdr/SWAA2024110555696.md): Cradle · broken · Nov 1, 2024 · N7876A · Boeing 7377Q8 · Emergency Equipment
  > FWD UPPER EMERGENCY FLASH LIGHT HOLD IS BROKEN<[01] FOUND FLASHLIGHT HOLDER IN SERVICEABLE CONDITION. R&R BROKEN FLASHLIGHT STRAP IAW AMM 25-64-00.
- [SDR SWAA2024100143056](https://openairdocs.org/sdr/SWAA2024100143056.md): Power Supply · inoperative · Sep 28, 2024 · N7876A · Boeing 7377Q8 · Emergency Lighting
  > DURING EMERGENCY LIGHT CHECK FOUND FORWARD CABIN CEILING EMERGENCY LIGHT WONT TURN ON.<[01] T/S PERFORMED PER WDM 33-51-12-6 AND FOUND POWER SUPPLY M1674 IS BAD. REPLACED POWER SUPPLY M1674 PER AMM 33-51-06 AND OPS CHECK GOOD.
- [SDR SWAA2024092038521](https://openairdocs.org/sdr/SWAA2024092038521.md): Light · inoperative · Sep 17, 2024 · N7876A · Boeing 7377Q8 · Emergency Lighting
  > EXTERNAL EMERGENCY LIGHT INOP JUST AFT OF THE FWD SERVICE DOOR.<[01] RELAMPED AND OPS CHECKED GOOD IAW MM 33-51-04.
- [SDR SWAA2024090634179](https://openairdocs.org/sdr/SWAA2024090634179.md): Light · worn · Sep 5, 2024 · N7876A · Boeing 7377Q8 · Emergency Lighting
  > PASSENGER CABIN - FWD L/H EGRESS STRIP WORN<[01] R&R PASSENGER CABIN - FWD L/H EGRESS STRIP PER AMM 33-51-15
- [SDR SWAA2024090634178](https://openairdocs.org/sdr/SWAA2024090634178.md): Battery Pack · inoperative · Sep 5, 2024 · N7876A · Boeing 7377Q8 · Emergency Lighting
  > EMX BATT PACK M02335 FAILS TO ILLUMINATE LIGHTS<[01] 01 - REMOVED AND REPLACED EMX BATTERY PACK AND POWER SUPPLY AT M02335 PER [AMM 33-51-06-960-806-NG (POWER SUPPLY - POWER SUPPLY REPLACEMENT - PERMANENT)]
- [SDR SWAA2024090634858](https://openairdocs.org/sdr/SWAA2024090634858.md): Power Supply · inoperative · Sep 5, 2024 · N7876A · Boeing 7377Q8 · Emergency Lighting
  > EMX BATT PACK M02335 FAILS TO ILLUMINATE LIGHTS<[01] 01 - REMOVED AND REPLACED EMX BATTERY PACK AND POWER SUPPLY AT M02335 PER [AMM 33-51-06-960-806-NG (POWER SUPPLY - POWER SUPPLY REPLACEMENT - PERMANENT)]
- [SDR SWAA2024071802699](https://openairdocs.org/sdr/SWAA2024071802699.md): Support Angle · cracked · Jun 17, 2024 · N7876A · Boeing 7377Q8 · Fuselage Miscellaneous Structure
  > CRACK SUPPORT ANGLE LOCATED IN WEATHER RADAR TRASCEIVER MOUNT RH SIDE AT EQUIPMENT ELECTRONIC COMP 2024-376755<[01] REPLACED SUPPORT ANGLE LOCATED IN WEATHER RADAR TRASCEIVER MOUNT RH SIDE AT EQUIPMENT ELECTRONIC COMP IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 1
- [SDR SWAA2024071802245](https://openairdocs.org/sdr/SWAA2024071802245.md): Angle · cracked · Jun 16, 2024 · N7876A · Boeing 7377Q8 · Wing Miscellaneous Structure
  > CRACK ANGLE ACCESS PANEL 343AT AT RT WING 2024-376742<[01] REPLACED ANGLE ON ACCESS PANEL 343AT AT RT WING IAW B737-700 #DWG: 186A3005 SHEET:1 REV:B SRM 51-40-02 AND SRM 51-10-01 ITEM 9.;[02] REPLACED ANGLE ON ACCESS PANEL 343AT AT RT WING IAW B737-700 #DWG: 1
- [SDR SWAA2024071802112](https://openairdocs.org/sdr/SWAA2024071802112.md): Web · cracked · Jun 15, 2024 · N7876A · Boeing 7377Q8 · Fuselage Miscellaneous Structure
  > CRACK ON LOWER SNUBBER WEB AT FWD ENTRY DOOR 2024-376728<[01] REPLACED (ACESS PANEL) LOWER SNUBBER WEB AT FWD ENTRY DOOR IAW B737-700 SRM 51-10-02 ITEM 9 AND DRAWING 141A6260 REV. C. SEE INDIVIDUAL SIGN OFF BELLOW;[02] TASK COMPLETED<BR><BR>SEE INDIVIDUAL SIGN
- [SDR SWAA2024071801505](https://openairdocs.org/sdr/SWAA2024071801505.md): Angle · cracked · Jun 13, 2024 · N7876A · Boeing 7377Q8 · Fuselage Miscellaneous Structure
  > CRACK ANGLE LOCATED STA663.75 AND LBL8 AT CENTER WING BOX 2024-376712<[01] TOOL USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 23-JAN-25.;[02] ON STEPS 5 AND 6; TOOL USED P/N: NORTEC 500D; S/N: 500X1693P030457; CAL DUE: 15-OCT-24.;
- [SDR SWAA2024071801300](https://openairdocs.org/sdr/SWAA2024071801300.md): Frame · cracked · Jun 13, 2024 · N7876A · Boeing 7377Q8 · Fuselage Main, Frame
  > CRACK ON FRAME WEB LOCATED BS259.5 BTW STR9L AND STR10L AT PASSENGER CABIN 2024-376710<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600D; S/N: 60009161631; DUE DATE: 11-MAR-25;[02] REPAIRED FRAME WEB LOCATED BS259.5 BTW STR5L TO STR11L AT PASSENGER
- [SDR SWAA2024071801301](https://openairdocs.org/sdr/SWAA2024071801301.md): Web · cracked · Jun 13, 2024 · N7876A · Boeing 7377Q8 · Fuselage Miscellaneous Structure
  > CRACK ON FRAME WEB LOCATED BS259.5 BTW STR9R AND STR10R AT PASSENGER CABIN 2024-376711<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR P/N: NORTEC 600; S/N: 60007161486; DUE DATE: 28-JUL-24;[02] REPAIRED FRAME WEB LOCATED BS259.5 AT PASSENGER CABIN BETWEEN STR 5R T
- [SDR SWAA2024071801044](https://openairdocs.org/sdr/SWAA2024071801044.md): Fitting · deteriorated · Jun 13, 2024 · N7876A · Boeing 7377Q8 · Emergency Equipment
  > DETERIORATED GIRT BAR FITTING HARDWARE AT FWD SERVICE DOOR 2024-376689<[01] REPLACED GIRT BAR FITTING HARDWARE AT FWD SERVICE DOOR I.A.W B737-700 AMM 25-66-02-400-801 STEP 3.D(1) ITEM (E) THRU 3.D(1) ITEM (I);[02] CERTIFIED CORRECTIVE ACTION 1
- [SDR SWAA2024071801045](https://openairdocs.org/sdr/SWAA2024071801045.md): Fitting · deteriorated · Jun 13, 2024 · N7876A · Boeing 7377Q8 · Emergency Equipment
  > DETERIORATED GIRT BAR FITTING HARDWARE AT FWD ENTRY DOOR 2024-376690<[01] REPLACED GIRT BAR FITTING HARDWARE AT FWD ENTRY DOOR I.A.W B737-700 AMM 25-66-02-400-801 STEP 3.D(1) ITEM (E) THRU 3.D(1) ITEM (I);[02] CERTIFIED CORRECTIVE ACTION 1
- [SDR SWAA2024071801046](https://openairdocs.org/sdr/SWAA2024071801046.md): Plate · deteriorated · Jun 13, 2024 · N7876A · Boeing 7377Q8 · Emergency Equipment
  > DETERIORATED GIRT BAR FITTING ADAPTER PLATE AND SHIM AT FWD ENTRY DOOR 2024-376691<[01] REPLACED GIRT BAR FITTING ADAPTER PLATE AND SHIM AT FWD ENTRY DOOR I.A.W B737-700 AMM 25-66-02-400-801 STEP 3.D(1) ITEM (E) THRU 3.D(1) ITEM (J);[02] CERTIFIED CORRECTIVE A
- [SDR SWAA2024071813988](https://openairdocs.org/sdr/SWAA2024071813988.md): Shim · deteriorated · Jun 13, 2024 · N7876A · Boeing 7377Q8 · Emergency Equipment
  > DETERIORATED GIRT BAR FITTING ADAPTER PLATE AND SHIM AT FWD ENTRY DOOR 2024-376691<[01] REPLACED GIRT BAR FITTING ADAPTER PLATE AND SHIM AT FWD ENTRY DOOR I.A.W B737-700 AMM 25-66-02-400-801 STEP 3.D(1) ITEM (E) THRU 3.D(1) ITEM (J);[02] CERTIFIED CORRECTIVE A
- [SDR SWAA2024071801051](https://openairdocs.org/sdr/SWAA2024071801051.md): Plate · deteriorated · Jun 13, 2024 · N7876A · Boeing 7377Q8 · Emergency Equipment
  > DETERIORATED GIRT BAR FITTING ADAPTER PLATE AND SHIM AT FWD SERVICE DOOR 2024-376692<[01] REPLACED GIRT BAR FITTING ADAPTER PLATE AND SHIM AT FWD SERVICE DOOR I.A.W B737-700 AMM 25-66-02-400-801 STEP 3.D(1) ITEM (E) THRU 3.D(1) ITEM (J);[02] CERTIFIED CORRECTI
- [SDR SWAA2024071813989](https://openairdocs.org/sdr/SWAA2024071813989.md): Shim · deteriorated · Jun 13, 2024 · N7876A · Boeing 7377Q8 · Emergency Equipment
  > DETERIORATED GIRT BAR FITTING ADAPTER PLATE AND SHIM AT FWD SERVICE DOOR 2024-376692<[01] REPLACED GIRT BAR FITTING ADAPTER PLATE AND SHIM AT FWD SERVICE DOOR I.A.W B737-700 AMM 25-66-02-400-801 STEP 3.D(1) ITEM (E) THRU 3.D(1) ITEM (J);[02] CERTIFIED CORRECTI
- [SDR SWAA2024071701055](https://openairdocs.org/sdr/SWAA2024071701055.md): Fitting · deteriorated · Jun 13, 2024 · N7876A · Boeing 7377Q8 · Emergency Equipment
  > DETERIORATE HARDWARE OF GIRT BAR FITTING AT AFT ENTRY DOOR 2024-376706<[01] REPLACED HARDWARE OF GIRT BAR FITTING AT AFT ENTRY DOOR I.A.W B737-700 AMM 25-66-02-400-801 STEP 3.D(1) ITEM (G) THRU 3.D(1) ITEM (I);[02] REPLACED HARDWARE OF GIRT BAR FITTING AT AFT
- [SDR SWAA2024071701056](https://openairdocs.org/sdr/SWAA2024071701056.md): Fitting · deteriorated · Jun 13, 2024 · N7876A · Boeing 7377Q8 · Emergency Equipment
  > DETERIORATE ADAPTER PLATE (2EA) AND SHIM(2EA) OF GIRT BAR FITTING AT AFT SERVICE DOOR 2024-376705<[01] REPLACED ADAPTER PLATE (2EA) AND SHIM(2EA) OF GIRT BAR FITTING AT AFT SERVICE DOOR I.A.W B737-700 AMM 25-66-02-400-801 STEP 3.D(1) ITEM (F) THRU 3.D(1) ITEM
- [SDR SWAA2024071701057](https://openairdocs.org/sdr/SWAA2024071701057.md): Fitting · deteriorated · Jun 13, 2024 · N7876A · Boeing 7377Q8 · Emergency Equipment
  > DETERIORATE ADAPTER PLATE (2EA) AND SHIM (2EA) OF GIRT BAR FITTING AT AFT ENTRY DOOR 2024-376704<[01] REPLACED ADAPTER PLATE (2EA) AND SHIM (2EA) OF GIRT BAR FITTING AT AFT ENTRY DOOR I.A.W B737-700 AMM 25-66-02-400-801 STEP3.D(1) ITEM (F) THRU 3.D(1) ITEM (J)
- [SDR SWAA2024071800664](https://openairdocs.org/sdr/SWAA2024071800664.md): Scuff Plate · cracked · Jun 12, 2024 · N7876A · Boeing 7377Q8 · Fuselage Miscellaneous Structure
  > CRACK IN SCUFF PLATE OF SERVICE DOOR AT FWD GALLEY AREA 2024-376665<[01] TOOL USED DIGITAL CALIPER P/N: 500-196-30; S/N: B23399190; DUE DATE: 04 / MAR / 25.;[02] TOOL USED: RADIOMETER/PHOTOMETER KIT. P/N:XRP-3000. S/N:1859843. DUE DATE:24-JUL-24.;[03] REPAIRED
- [SDR SWAA2024071800665](https://openairdocs.org/sdr/SWAA2024071800665.md): Scuff Plate · cracked · Jun 12, 2024 · N7876A · Boeing 7377Q8 · Fuselage Miscellaneous Structure
  > CRACK CENTER SCUFF PLATE AT AFT CARGO COMPARTMENT 2024-376667<[01] TOOL USED DIGITAL CALIPER P/N: 500-196-30; S/N: B23399190; DUE DATE: 04 /MAR / 25.;[02] TOOL USED IN STEP 4: RADIOMETER/PHOTOMETER; P/N: XRP-3000; S/N: 1859843; DUE DATE: 24-JUL-24.;[03] REPAIR
- [SDR SWAA2024071800871](https://openairdocs.org/sdr/SWAA2024071800871.md): Doubler · unknown · Jun 12, 2024 · N7876A · Boeing 7377Q8 · Fuselage Main, Plate/Skin
  > REJECT - IMPROPERLY GROUND SERVICE DOOR 114AR FABRICATED REPAIR DOUBLER AT LOWER FUSELAGE (REPAIR DOBLER MADE THICK 0.040 INCHES INSTEAD 0.050 INCHES) 2024-376672<[01] MADE AND DRILLED REPAIR PARTS [2] DOUBLER WITH MATERIAL USED ALUMINUM SHEET P/N: 2024T3 0.05

Next page: https://openairdocs.org/aircraft/N7876A/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 = 'N7876A' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N7876A/reports

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